6 a27) · reference 7.2. the rendezvous navigation update schedule ... 4 122+55 csi targeting ip32...
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-F76 A27)
NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONMSC INTERNAL NOTE NO CF-R-69-23
LM RENDEZVOUS PROCEDURES
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0 MISSION
FINAL 189
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MANNED SPACECRAFT CENTER __-______ HOUSTONTEXAS
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by-_____
AARORMOANU-ERSNATIONAL (CATEGORY) INFORMATIONTECHNICALSERVICE S pn fi-d Va 22151 1
httpsntrsnasagovsearchjspR=19700025407 2020-01-29T010654+0000Z
LM
RENDEZVOUS PROCEDURES
G MISSION
AS-506CSM-107LM-5
May 16 1969
PREPARED BY=m StepWI P Gregaf Orbital Procedu~res Sectioed
APPROVED BY t ~ 62()Miflton C CoWrtella Chief Orbital Procedures Section
1rLiJC J4A-Paul C Kramer Chief Flight Procedures Branch
4- dames W Bilodeau Assistant Chief For Crew Integration Flight Crew Support Division
Chief Night Cfew Support Division
[onaid KSayton ]j- hairman Crew Procedies Control Board
-I-
TABLE OF CONTENTS
PAGE
10 PURPOSE 1-1
20 INTRODUCTION 2-I
30 DISCUSSION OF MAJOR EVENTS 3-1 31 Concentric Sequence Initiation 3-1 32 Constant Delta Height and Plane Change 3-1 33 Terminal Phase Initiation 3-2 34 Midcourse Corrections 3-2 3 5 Braking 3-2
40 NOMINAL PROCEDURES 4-1 41 Commander Tasks 4-1 4 2 LM Pilot Tasks 4-1 43 Abbreviations 4-1 44 Nominal PGNS Procedures 4-3
50 ABORT PROCEDURES 5-I 51 Nominal AGS Procedures 5-2
60 ONBOARD RENDEZVOUS CHARTS 6-1 61 Concentric Sequence Initiation 6-2 62 Constant Delta Height 6-4 63 Terminal Phase Initiation 6-6 64 First Midcourse Correction 6-7 6 5 Second Midcourse Correction 6-8 6 6 Relative Reference Trajectory 6-9
70 REFERENCES 7-1
=i1-
FIGURES
PAGE
Relative Motion Profile (2-1) 2-2
LUNAR ORBIT RENDEZVOUS ATTITUDE TIME HISTORY 2-3
Lift-off - CSI (2-2) 2-3
CDH-TPF (2-3) 2-4
LIST OF ACRONYMS AND ABBREVIATIONS ACQ ADJ AGS AOH AOS AOT APS ATT BU CALIB CB CDH CDR CM CMC CMD CMP COAS CSI CSM CT DAP DH DOI DPS DSKY DV DWN EMS ET FDAI FPS FWD GDC GET GETI GMBL GND HA HGA HOR HORIZ HP IMU INS IT LGC LM
Acquisition Adjust Abort Guidance System Apollo Operations Handbook Acquisition of Signal Alignment Optical Telescope Ascent Propulsion System Attitude Backup Calibration Circuit Breaker Constant Delta Height Commander Command Module Command Module Computer Command Module Commanders Position Command Module Pilot Crew Optical Alignment Sight Concentric Sequence Initiation Command and Service Module Cease Tracking Digital Autopilot Delta Height Descent Orbit Insertion Descent Propulsion System Display and KeyboardDelta Velocity Down Entry Monitor System Event Timer Flight Director Attitude Indicator Feet Per Second Forward Gyro Display Coupler Ground Elapsed Time Ground Elapsed Time of Ignition Gimbal Ground (Mission Control) Apogee Altitude High-Gain Antenna Horizon Horizontal Perigee Altitude Inertial Measurement Unit Insertion Initiate Tracking LM Guidance Computer Lunar Module
LV
-1v-
LMP LOI LOS
MNVR MCC MCCl MCC2 MCC-H MGA MSFN NAV ORDEAL PAD PB PC PDI PGNS PHS PIPA PLM PRO PROG PROP R RCS RDOT REFSMMAT RHC RR SHFT SC SEP SM SXT SYNC TFI THC THETA TIGN TLM TPF TPI TRUN TTCA VG VHF (XXXX) (XXXXX XX)
Lunar Module Pilot Lunar Orbit Injection Line Of Sight Launch Vehicle Maneuver Midcourse Correction First Midcourse Correction Second Midcourse Correction Mission Control Center - Houston Middle Gimbal Angle Manned Space Flight Network Navigation Orbital Rate Drive Earth and Lunar Data Voiced to Crew From Ground Pushbutton Plane Change Powered Descent Initiation Primary Guidance Navigation and Control System Phasing Pulse Integrating Pendulous Accelerometers LM Pitch Angle Proceed Program Propellant Range Reaction Control System Range Rate Reference Stable Member Matrix Rotation Hand Controller Rendezvous Radar Shaft Spacecraft Separation Service Module Sextant Synchronize Time From Ignition Translation Hand Controller Angle Between SC +X Axis and Local Horizontal Time of Ignition Telemetry Terminal Phase Finalization Terminal Phase Initiation Trunnion Translation Thrust Control Assembly Velocity to be Gained Very High Frequency Indicates GET From Liftoff in HoursMinutes Indicates GET From Liftoff in HoursMinutesSeconds
(XXXXXXXXXXXX) (OrdealInertial) Angles (Roll Pitch Yaw) (XXXXXX) Local Vertical DVs
Tracking Stations
ANG BDA CRO CYI GYM HSK HTV MAD MER MIL RED TEX VAN
-v-
Antigua Near Space Support Station Bermuda Near Space Support Station Carnarvon Near Space Support Station Canary Near Space Support Station Guaymas Near Space Support Station Honeysuckle Deep Space Support Station Huntsville Near Space Support Station Madrid Deep Space Support Station Mercury Near Space Support Ship MILA Near Space Support Station Redstone Near Space Support Ship Corpus Christi Near Space Support Station Vanguard Near Space Support Ship
10 PURPOSE
This document contains the primary procedures for the LM-5 active rendezvous with CSM-107 spacecraft in accordance with Detailed Test Objective Section 40 defined in Reference 71
The purpose of the LM Rendezvous Procedures document is to provide a single source of procedures information for use in flight planning in crew training and in preparing onboard data
This is a control document subject to review by all elements of the Apollo Program and to approval by the Procedures Conshyfiguration Control Board Comments should be directed to Mr Stephen P Grega Flight Procedures Branch Flight Crew Support Division Extension 5348
Beyond G mission planning no additional techniques and trajectory information specific to Mission H have been made available as of this date Therefore since Missions G and H are expected to be similar in the area of rendezvous guidance and navigation procedures the G mission final LM Rendezvous Procedures Document will serve -as an H mission preliminary LM Rendezvous and Procedures Document After reviewal by all elements of the Apollo Program and approval by the Procedures Configuration Control Board this document will then evolve into the control document for the Mission H crew procedures
2-1
20 INTRODUCTION
The LM-5CSM-l07 lunar orbit rendezvous exercise will beginduring the twenty-fourth CSM revolution with insertion at 122 35255 and end at approximately 1260000 with post rendezvous station keeping The LM procedures during this period are divided into segments of major activities which are discussed in detail in Section 30
A nominal LM-5CSM-107 mission profile is contained in Figshyure (2-1) This figure shows the locations in time and local horizontal position of the most significant nominal mission events Trajectory data used to generate the mission profile and timeline for procedures development was obtained from Reference 72 The rendezvous navigation update schedule assumed in the procedures is defined in Reference 73
A history of the LM body attitudes during the rendezvous accompanies the major events discussion and is also presented in Figures (2-2) and (2-3) Each figure illustrates the bodyattitudes with respect to the moon sun and earth and indicates FDAI roll pitch and yaw gimbal angles and the ordeal pitch angle for significant events during each lunar orbit
0RBI TR EL
TRAILINGDISPLACEMENT(N MI) 0 0 W60 20240 BE
33I I ] I I I
32 ltrMCCE 1125+-3 C CH (124t24) PLAN CHANGE023 TM)2
R~TC(222
40 1146235 A N MNTTIMETKS FROMISEDRT(GA122plusmn252
-- DAYLIGHT B shy
_ _ _ _ _ _ __E_ _ -- 7 LUNAR IARFAGELM MAJOR EVENTS
122+35 INSERTION 17 124+H7 AGE UPDATE AND ALIGN (R47) 2 122+40 IMU REFSMMAT ALIGN (P52) 1 124+24 CDH THRUSTING (P41) TRAILINGDISPLACEMETIN RI)
3 122+54 AGS UPDATE AND ALIGN (R471 19 124+26 TPI TARGETING IP34 amp AGS) 5 II 20 25 30 4 122+55 CSI TARGETING IP32 amp AGSI 20 124+26-124+51 RR NAVIGATION (P20 18 MARKS) - I I
5 122+54-123+14 RR NAVIGATION (P20 18 MARKS) 21 124+53 AGS UPDATE AND ALIGN (R47)I
6 123+18 COMPUTE CSI BACKUP 22 125+00 COMPUTE TPI BACKUP
7 123+19 AGS UPDATE AND ALIGN (R471 23 125+03 TPI THRUSTING (P411 c
8 123+26 CSI THRUSTING (P411 24 125+05 MCC1 TARGETING IP35) N - M ((25+232
9 123+30 SET W MATRIX 1200025) 25 125+05-125+16 RR NAVIGATION IP20 9 MARKS) 5
2 r INSERT A 10 123+31 CDH TARGETING IP33 amp AGS 26 125+16 COMPUTE MCCI THRUSTING IP41) 5 31 PHAE
11 123+31-123+46 RR NAVIGATION 1P20 14 MARKS) 27 125+18 MCC I THRUSTING (P41)
12 123+47 EXT AV FOR PLANE CHANGE (P20) 28 125+20 MCC2 TARGETING (P351 13 123+54 RCS PLANE CHANGE THRUSTING (P411 29 125+20-125+31 RR NAVIGATION (P20 9 MARKS) 14 123+56 CDH TARGETING (P33 amp AGS) 30 125+31 COMPUTE MCC 2 BACKUP Ideg
15 123+56-124+12 RR NAVIGATION (P20 13 MARKS) 31 125+33 MCC2 THRUSTING [P41)
16 124+15 COMPUTE CDH BACKUP 32 125+48 BRAKING (P47) 27 26TP25+03
33 126+00 STATION KEEPING LT
24
FIGURE 2-1 G MISSION RENDEZVOUS
(CSM-CENTERED RELATIVE MOTION) FOLDOUT FRAME
l D T R2A-e2 TALPFO EDUR ES EPREPAREDBY STEPHENP GRED501I DOUT FRAMW ORBI R B C 0
MISSION G LUNAR ORBIT RENDEZVOUS ATTITUDE TIME HISTORY
OFOR THE LM P33
P20 123+31) (021880)
LMI CSI NrxNMARKS i (123+26+27)
FINAL -
COMP(I123+1l6)
P32 LANDING SITEj P20 30ES (122+50) CSM AT (04650) PRIME MERIDIAN LIFT-OFF
P52 (122+28+11) (122+40)DIRECTION OF (03640)ORBITAL MOTION IS
CLOCKWISE
(18012150)I NERTIAL YAWKLINERTIAL PITCH
ORDEAL PITCH EARTHINERTIAL ROLL
FIGURE 2-2
MISSION G LUNAR ORBIT RENDEZVOUS ATTITUDE TIME HISTORY
FOR THE LM
LM TPF (126+00+00) (01302920)
LM LMC2PLANE CHANGELMPI+30) (123+54+25)
(TPI+30) (0560)(0782400) 7 SUN
P20
(TPI+15) P3
P33(0532480) COMP
---- _ (124+12--- ---
LM TPI (125+02+46) L D (026 627650) (124+24+25)
(0980)
FINAL
DIRECTION OF COMP ORBITAL MOTION IS (124+50)
CLOCKWISE
(18012150)
LL INERTIAL YAW NERTIAL PITCH
ORDEAL PITCH EARTH INERTIAL ROLL
FIGURE 2-3
3-1
30 DISCUSSION OF MAJOR EVENTS
31 Concentric Sequence Initiation
Immediately following Insertion the LM navigated vector will be downlinked to Mission Control Center-Houston this state vector is then uplinked to the CSM The LM commander will perform a Proqram 52 fine alignment to REFSMMAT at approxishymately 12240
The digital autopilot is configured to wide deadband Program P20 is called and an automatic pitch maneuver is initiated to the preferred track attitude At 122 55 CSI targeting parameters are loaded in the PGNS and AGS A period of rendezvous radar marking will then take place from 122-57 to 12315 Upon completion of tracking the LM will obtain an out-of-plane velocity from the CSM to be vectored with the in-plane component of the CSI delta V The CSMs estishymate of out-of-plane velocity is alleged to be better than the LMs estimate (Reference 74)
At approximately 123 20 the LM will voice its CSI solution to the CSM the AGS is updated aligned and targeted in external delta-V with the CDH solution to be excuted Program P41 will then be called and the automatic pitch maneuver bypassed since the burn isto be executed with Z-Axis thrusting The CSI burn occurs nominally at 123 26 27 After verification of the LM CSI burn the CSM will incorporate the LM burn parameters in its CMC LM state vector
32 Constant Delta Height and Plane Change
At 12330 approximately three minutes after the LM CSI burn the W matrix will be set to (200025) and the LM targeting paramters are loaded in both the PGNS and AGS for the CDH maneuver Out-of-plane velocity will then be computed and voiced to the LM from the CSM Program P30 is loaded with the targeting parameters for the LM Plane Change maneuver which will be accomplished in Program P41 30 minutes prior to the CDH maneuver Following the burn the target delta V parameters are voice to the CSM and incorporated into the CMC LM state vector At 12356 the CDH targeting parameters are loaded in both the PGNS and AGS for 1242425 A CDH chart solution is calculated 7 minutes prior to TIG The AGS is updated aligned and targeted in external delta V with the CDH solution to be executed The RCS Thrust Program P41 is called at 12418 and the burn attitude is bypassed since the LM executes CDH by thrusting out individual components of delta V while maintaining radar lock-on
3-2
3 3 Terminal Phase Initiation
Radar tracking is initiated after the CDH maneuver and updating of the LGC continued At 12426 approximately two minutes after the LM CDH burn targeting parameters are loaded in both the PGNS and AGS for the TPI maneuver which will be targeted for a node at intercept Backup measurements are made at the appropriate times The AGS is updated aligned and targeted in external delta V with the TPI solution to be executed The RCS Thrust Program P41 is called at 12456 and the burn attitude is bypassed since the LM is burning along the plus Z-axis with the thrust direction established with the COAS
3 4 Midcourse Corrections
Immediately after TPI the Midcourse Prethrust Program P35 will be called and radar tracking reinitiated Backup measshyurements are made and midcourse corrections chart solutions obtained The MCCl burn will nominally be performed at TPI plus 15 minutes (1251746) If MCCI is to be excuted Program P41 will be called and the burn attitude maneuver is bypassed since the plus Z-axis will remain boresighted at the CSM until docking
Following MCCI Program P35 will be called and targeted for MCC2 at TPI plus 30 minutes (1253246) and executed identishycally to MCCI
3 5 Braking
In preparation for braking the DAP is configured in narrow deadband Program P20 is terminated at 18000 feet but the radar is kept in auto track to provide radar range and range rate displayed on the tapemeter Average G is called by Program P47 prior to braking and attitude hold is selected The braking schedule is followed as contained in Section 4
4-1
40 NOMINAL MISSION PROCEDURES
The procedures included in this section do not specify which crewmember Commander or LM Pilot performs each task These need not be specified since the following basic rules define which crewmember performs each task
41 Commander Tasks
1 All attitude changes whether manual or automatic will be accomplished by the CDR
2 The operation of the DSKY during thrust programs (P40 P41 P42 P47) will be done by the CDR Actual manipulation of the TTCA need not be always done by the CDR but in most cases will be
3 Operation of the rendezvous and landing radar will be done by the CDR
4 The CDR will operate all other systems accessible to only his crew station
42 LM Pilot Tasks
1 AGS operation 2 DSKY operation will be done by the LMP except when keyboard
entries affect the control of spacecraft attitude or thrustshying
3 Backup data logging and chart calculations 4 All logging of maneuver solutions and systems performance 5 The LMP will operate all other systems accessible to only
his crew station
These general rules are guidelines only and may be deviated from by the LM crew if they develop more efficient Task assignments
43 ABBREVIATIONS
The abbreviations used herein are consistant with those in the AOH However in order to condense and simplify the procedures so that they are representative of onboard data a number of addshyitional shorthand conventions have been used To allow the unshyfamiliar reader to understand the procedures contained in this section the following explanations are included
1 AGS - A single asterisk is employed to denote those procedures involving operations to be performed on the DEDA The three number group following an asterisk specifies DEDA address An Rfollowing the address group indicates the address is to be read out A five digit group behind the Rindicates a nominal or expected display If the three number address group is followed by a plus or minus sign a data load is indicated When a single digit follows the plus addition of four zeros behind this digit is assumed Once used these conventions are easily handled and save considerable space
4-2
2 PGNS - The verb-noun addresses in the PGNS are indicated to the left of the procedures column An F is used to indicate a flashing display or absence of an F a static display To the right of the verb-noun on the same line are the contents of the three data registers If numeric quantities appear the DSKY should be correspondingly made to agree by executing a V21 V22 or V23 and performing a data load The procedure of blanking and loading registers is not included since it is repeated often and is highly familiar to the crews
EXAMPLE F 06 33 125-02 46 TIG OF TPI
Expanded this means Load flashing verb 06 noun 33 with the quantity 125 hours 2 minutes and 46 seconds the time of ignition of the RCS engine TPI maneuver Procedurally this is done by keying verb 25 enter loading +000125 in register 1 +00002 in register 2 and +04600 in register 3
If numberic quantities do not follow the verb-noun it is indicated that a computed or information quantity is being displayed via the DSKY If nominal values are listed for possible comparison they appear in parentheses
EXAMPLE- F 06 42 HA HP V
Expanded this means Flashing verb 06 noun 42 has computed height of apogee in register 1 height of perigee in regshyister 2 and velocity to be gained in register 3
3 TIME - The numbers in the left hand column preceded by a plus or minus indicate event timer time referenced to an event Minus indicates event timer counting down to a future event Periodically this same column contains the nominal mission ground elapsed times in parentheses Asterisks following the event time indicate a time critical event which should be accomplished to the nearest second
4-3
4 4 Nominal PGNS Procedures
ASSUMPTIONS
AFTER INSERTION
1 INSERTION COMPLETE (RESIOUALS NULLED) VERIFY V82E (ORBIT) 3 RNDZ RDR LOCKED ON IN MODE II 4 LGC AT FLASHING VERB 37 5 PROPER INITIAL W MATRIX LOADED IN LGC
GUID CONT-PGNS ATTITUDE MON-PGNS(CDR) RATE ERR MON-CMPTR(LMP) ATTITUDE MON-AGS(LMP) SHFTTRUN-+5 DEG X-POINTER-HI MULT RADAR TEST SW-OFF ENG ARM-OFF X-TRANSL-2JETS DEAD BAND-MIN PGNS MODE CONT-AUTO THROTJET-JET CBPGNS IMU OPR-CLOSE RR MODE-LGC TTCATRANSL-ENABLE(COR)
BAL CPL-ON MODE SEL-AGS
RNGALT MON-RNGRNGRT RATE ERR MON-RNDZ RORICOR) ATT CONT-PULSE(3)
AGS MODE CONT-ATT HOLD ACA4JET-DISABLE(CDRJ TTCATRANSL-DISABLE(LMP)
ACA4JET-DISABLE(LMPI
KEY ODE (PO0)
(DOWNLINK LM STATE VECTOR)
KEY V63E (RR SELF TEST)
4-4
F 04 12 00004 00001 PRO
F 16 72 TRUN SHFT PRO
F 16 78 R ROOT VERIFY TAPE METER WITH DSKY
+2 VERIFY INSERTION VELOCITY WITH RNDZ ROR WHERE RANGE = 2642 NM RANGE RATE = -4251 FPS
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
KEY V34E (TERMINATE) KEY V48E (LOAD DAP)
F 01 46 11002 PRO
F 06 47 LMWT CMWT PRO
KEY V56E (KILL AUTO TRACK ENABLE)
+3 KEY V41N72E (COARSE ALIGN RR) F 21 73 +000OOTRUN -077OOSHFT F 04 12 00006 00002 (CONTINUOUS DESIGNATE)
PRO 41 (COARSE ALIGN VERB)
KEY VI6N72E 16 72 MONITOR TRUNSHFT ANGLES
CB PGNS RNDZ RDR-OPEN CB AC BUS A RNDZ RDR-OPEN KEY V44E (TERMINATE RR DESIGNATE)
KEY V83E F 16 54 R ROOT THETA
SET ORDEAL PRO
CS HEATER AOT-CLOSE
CB AOT LAMP-CLOSE
+5 KEY V37E52E (IMU REALIGN)
4-5
410+1 CSI ROUTINE 373+02065 CS TIME 275+03028 TPI TIME
605400777 COTANGENT OF LOS TO-CSM 416+1 (ONE-HALF bRBITAL PERIOD) 411+0 RCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT 310R TIME TO CS
267R VELOCITY TO BE GAINED CSI
402R DELTA H
371R DELTA V CDH
372R _ DELTA T CSICDH
F 04 06 00001 00003 -(REFSMMAT) PRO -
F 50 25 00015 SELECT 1ST STAR ENTR
F 01 70 O02DE LOAD 1ST STAR PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FOAl ANGLES (AUTO MNVRI)
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVR)
F 01 71 002DE
KEY V76E PGNS MODE CONT-ATT HOLD
PRO +10 F 54 71 MARK 1ST STAR
PRO F 01 70 O02DE LOAD 2ND STAR
PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FDA ANGLES -(AUTO MNVRV
F 50 18 FDAI ANGLES (REQUEST PNVRt ENTR (BYPASS MNVR
F 01 71 002DE PGNS MODE CONT-ATT HOLD PRO
-35
4-6
+14 F 54 71 MARK 2ND STAR PRO
F 06 05 STAR ANGLE DIFFERENCE PRO
F 06 93 GYRO TORQUE ANGLES PRO
F 50 25 00014
PRO (CHECK ALIGNMENT IF TIME WILL PERMIT)
F 50 25 00015 SELECT 3RD STAR ENTR
F 01 70 OO2DE LOAD 3RD STAR PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FDAI ANGLES (AUTO MNVR)
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVR)
VERIFY ALIGNMENT VIA AOT
KEY V34E (TERMINATE) F 37 BB
V48E (LOAD DAP) F 01 46 11012
PRO F 06 47 LMWT CMWT
+17 PRO
CB AOT LAMP-OPEN
RESET ET (310R)
(12253) CB AC BUS A RNDZ RDR-CLOSE (WAIT 30 SEC) CB PGNS RNDZ RDR-CLOSE
RR MODE-LGC KEY V37E20E (ACQUIRE RADAR)
PGNS MODE CONT-AUTO F 50 18 FDA ANGLES (REQUEST MNVRJ
PRO (AUTO MNVR) 06 18 FDAI ANGLES (AUTO MNVR)
AGS MODE CONT-AUTO RATEERR MON-CMPTR (LMP)
F 50 18 FDAI ANGLES (REQUEST MNVR)
4-7
ENTR (BYPASS MNVR) NO TRK LT-OFF
F 50 72 RR TRUNSHFT VERIFY RR LOCK ON PRO
DSKY BLANKS
KEY V93E (BEFORE 1ST MARK REINIT W MATRIXI KEY V80E (UPDATE LM SV)
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (i20OOZOO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
400+3 AGS ALIGNshy400R (00000 COMPLETE) 507+0 Z-AXIS BORESIGHT 400+2 ACQUISITION STEERING
CS
(122amp55) KEY V37E32E (CSI)
F 06 11 1 S LOAD TIG CSI FROM DATA PAD (NOM 123S26- 271 PRO
F 06 55 +O000IN +02660E +13000 OMEGAT (CDH 180 DEG AFTER CSI PRO
F 06 37 LOAD TIG TPI FROM DATA PAD (NOM 1251021761 PRO
F 16 45 MKS TFI -00001
-30 COPY RDOT FOR 1ST CSI BU
31OR TIME TO CSI
267R VELOCITY TO BE GAINED CSI
402R DELTA H
371R DELTA V CDH
-22
4-8
372R _ DELTA T CSICDH
KEY V32E (MARKS=5
F 06 75 DELTA H DELTA T CSICDH DELTA T CDHTPI PRO
F 06 81 DELTA VOS-LV (CS) (NOM 501 DELTA VX)
CSI(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (CDH)
(NOM 60 DELTA VX) CDH(82)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
KEY V32E (MARKS=1C)
F 06 75 DELTA H DELTA TCSICDH DELTA TCDHTPI PRD
F 06 81 DELTA VS-LV (CSI) CSI(N811
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 82 DELTA VIS-LV(CDH)
CDH(82)
DELTA VX(LVI
DELTA VY(LV)
DELTA VZ(LV)
-12
4-9
-20 COPY RDOT FOR 2ND CSI BU
F 16 45
F 06 75
F 06 81
F 06 16
F 06 90
PRO MKS TFI -00001
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS NON SEL - PRPLNT A + B TEMP IND 40DEG TO lOODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + 8 PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4v 2 3 (120 - 190 DEG F
(LOS OF MSFN ) S-BAND - SLEW TO P = +90 Y a 0 S-BAND - FWD (OR AFT) S-BAND - DN VOICE BU BIOMED OFF
PRO (FINAL COMP)
267R - VELOCITY TO BE GAINED CSI
402R DELTA H
372R TIME CSICDHL
371R PREDICTED VEL TO BE GAINED CDH
263R OUT-OF-PLANE
DELTA H DELTA TCSICDH DELTA TCDHTPI PRO DELTA VS-LV (CSI)
KEY V9OE (OUT-OF-PLANED
0 LOAD TIG CSI FROM DATA PAD (NOM 12302627) PRO Y YDOT PSI
N90 CSM
YDOT
PRO
-7
4-10
F 06 81 DELTA VS-LV(CSI)
COPY YDOT FROM CSM AND LOAD NEGATIVE IN R2 CSIIN81I
DELTA VX(LV)
DELTA VYILV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (COH)
CDH(82)
DELTA VX(LV)
- DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RANGE AND RDOT FOR 3RD CS BU
COMPUTE CSI BU
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (i2000OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
(TRANSMIT CSI DATA TO CSMI VHF A XMTR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF TELEMETY PCM - LO
KEY VB3E F 16 54 R ROOT THETA
SET ORDEAL PRO
317R RANGE
440R RANGE RATE
4-11
400+3 AGS ALIGN t40OR (00000 COMPLETE)
277R THETA
PRO F 37 BB
-6 KEY 41E (RCS THRUSTING) F 50 18 FDAI-ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTAV 400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTAV 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA RF
TRANSMIT TGT DELTA VS TO CSM AND SYNC COUNTDOWN
16 85 DELTA VS-BODY
502R DELTA VZ (NOM 5Ql)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTAVS-BODY
(123t26t27) BURN +Z
NULL DELTA VS
4-12
VERIFY AGS RESIDUALS 50OR 501R 502R DELTA VX _ DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
CDH
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
KEY V67E (RESET W MATRIX) F 06 99 +0200E +O0020E +00005E
PRO
507+0 Z-AXIS BORESIGHT
(VHF RANGING WITH CSM) VHF A XMTR - VOICERNG VHF B XMTR - OFF VHF B RCVR - ON TELEMETRY PCM - HI
(12331) KEY V37E33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 a TIG CDH (NOM 1242425) -120 amp00 10 (AGS 0 TIME)
(CONVERT TO MINUTES)
411+0 THRUST ALONG Z-BODY AXIS ENTER IF YOU DONT TARGET CSI
373R (NOM 26443 310R TIME TO CDH
4-13
423R DESIRED ALT RATE AT CDH
402R DELTA Hshy
450R DELTA VX
452R DELTA VZ
623+0 Z-AXIS PARALLEL TO CSM PLANE
IPRO F 16 45 MKS TFI -00001
-52 RESET ET
KEY V93E (REINIT W MATRIX WHEN MARKS =4)
KEY V32E (MARKS = 3)
F 06 75 DELTA HCDH DELTA TCDHTPI DELTA TTPI PRO
F 06 81 DELTA VCDH-LV CDH(N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
-47 KEY VSOE (OUT-OF-PLANE)
_ TIG CDH (NOM 124t24t25) -3000 TIME FROM CDH
F 06 16 l1 LOAD TIG PLANE CHANGE (NOM 123amp54-253 PRO
F 06 90 Y YDOT PSI N90 CSM
VYDOT PRO
-42 KEY V32E (MARKS=1O)
F 06 75 DELTA HCDH DELTA TCDIHTPI DELTA TTPITPI PRO
F 06 81 DELTA VCDH-LV
4-14
CDH (NS1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -OO1
KEY V34E (TERMINATE) F 37 B8
PLANE CHANGE
KEY 30E (EXTERNAL DELTA V)
TIG CDH (NOM 124124t25) -3000 TIME FROM CDH
F 06 33 LOAD TIG PLANE CHANGE (NOM 123154T25) PRO
F 06 81 DELTA VS-LV (NOM 00)
-36 COPY RDOT FOR 1ST CDH BU
KEY V90E (OUT-OF-PLANE)
F 06 16 1 1 LOAD TIG PLANE CHANGE (NOM 1231543251 PRO
F 06 90 Y YOOT PSI N90 CSM
YDOT
PRO
F 06 81 DELTA VS-LV(NOM 00)
COPY YDOT AND LOAD NEGATIVE IN R2 PRO
F 06 42 HA HP DELTA V PRO
F 16 45 MKS TFI MGA
PRO
F 37 BB
KEY 41E (RCS THRUSTING)
-30
4-15
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVRI
410+5 EXTERNAL DELTA V 450+0 451-YDOT 452+0 (LOAD CSM -YDOT)
407+0 ROTATE EXTERNAL DELTA V RF
16 95 DELTA VS-BODY
-3035 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATTVHOLD 407+1 FREEZE EXTERNAL DELTAV
F 16 85 DELTA VS-BODY -
NULL DELTA VIS
PRO F 37BB
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
507+0 Z-AXIS BORESIGHT
(12356) KEY 33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 TIG CDH (NOM 124t24t25) -120 OO ZOO (AGS 0 TIME)
(CONVERT TO MINUTES)
373R _ (NOM 2644) 310R TIME TO CDH
423R DESIRED ALT RATE AT CDH
(ADS OF MSFN) S-BAND - SLEW TOP = ACQUIRE HGA LOCK ON VOICE - BUVOICE -- VOICE VERIFY VOICE TLM BIOMED - LEFT (OR RIGHT)
402R DELTAH
4-16
F 16 45
-25
-23
F 06 75
F 06 81
F 16 45
-12
F 06 75
F 06 81
450R DELTA VX
452R DELTA VZ
PRO MKS TFI -00001
KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
COPY ROOT FOR 2ND CDH BU
KEY v32E (MARKS = 5)
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40DEG TO 1OODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + B PRESS IND PSIA
A QUANTITY IND _ PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING a TEMP MON SEL RCS QUAD 1 4 2 3 (120 - 190 DEG F)i
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
CDH(NB1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO MKS TFI -00001
PRO (FINAL COMP)
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
KEY V9OE (OUT-OF-PLANE)
-7
4-17
F 06 16 jj LOAD TIG CDH FROM DATA PAD (NOM 12424251 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT PRO
COPY YOOT FROM CSM AND LOAD NEGATIVE IN R2
CDH(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RDOT FOR 3RD CDH BU
COMPUTE CDH BU
TRANSMIT TGT DELTA VOS TO CSM AND SYNC COUNTDOWN
KEY V47E (INITIALIZE AGS F 06 16 GET OF AGS 0 TIME 120O00OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
KEY V83E F 16 54 R RDOT THETA
SET ORDEAL PRO
317R _ RANGE
440R RANGE RATE 400+3 AGS ALIGN 40OR (00000 COMPLETE)
277R THETA
-6
4-18
PRO F 3 BB
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY V06N86E F 06 86 DELTA VIS-LV
AGS(N86) CHART
DELTA VX(LVD
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
16 85 DELTA VS-BODY
50OR DELTA VX (NOM -0O3)
502R DELTA VZ (NOM 60)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD 407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS BODY
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS 5OOR 50IR 502R DELTA VX -DELTA VY DELTA VZ-
VERIFY PGNS RESIDUALS N85
DELTA VX(LM)
4-19
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
TPI
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO 507+0 Z-AXIS BORESIGHT
(12426) KEY 34E (TPI)
-36 RESET ET
F 06 37 - amp LOAD TIG TPI FROM DATA PAD (NOM 1250246) PRO
F 06 55 +00000 +02660E +13000 OMEGAT PRO
F 16 45 MARKS TFI -00001
-32 KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
-29 KEY V32E (MARKS = 3)
F 06 37 __ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
RESET ET
410+3 TPI SEARCH ROUTINE 307+04300 DELTA T TRANSFER
4-20
-26 310+02600 TFI TPI
303R THETA AT TPI
267R DELTA VTPI
371R DELTA VTPI + DELTA VTPF
KEY V32E (MARKS = 10)
F 06 37 _ _ _ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VIS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
TEMPIPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40ODEG TO IGODEG F A + B PRESS IND 181 +-3 PSIA
TEMPIPRESS MON SEL - HEL
A + B PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD I 4 2 3 (120 - 190 DEG F)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
RESET ET
-13 310+01300 TFI TPI
303R THETA AT TPI
-12 PRO (FINAL COMP) F 06 37 Z TIG TPIj__
4-21
TRANSMIT TIG OF TPI TO CSM-
PRO F 06 58 HP DELTA VTPI DELTA VTRF
PRO F 06 81 DELTA VS-LV
KEY V9OE (OUT-OF-PLANE)
F 06 16 1 LOAD TIG TPI FROM DATA PAD (NOM 12502461 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT
PRO F 06 81 DELTA VS-LV
COPY CSM YDOT AND LOAD NEGATIVE IN R2 N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 59 DELTA VS LOS
N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI MGA
RESET ET
PRO F 37 BB
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (12000t600)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE)
-10
-6
4-22
F 50 16 DOWNLINK COMPLETE PRO (UPDATE COMPLETE)
400+3 AGS ALIGN 400R (00000 COMPLETE)
-9 277R COPY TGT LOS ANGLE
310+00800
303R THETA AT TPI 410+4 DIRECT TRANSFER AT ET=-8 404+0 405+0 406+0 (MONITOR 470 471 4721
373R TIG TPI
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
KEY 41E (RCS THRUSTING) F 50 18 FOAl ANGLES (REQUEST MNVRI
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
-5 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUS
400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
COMPUTE TPI BU
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
4-23
1685 DELTA VS-BODY
50OR DELTA VX(NOM -115)
502R DELTA VZ(NOM 229)
-Z35 OSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS-BODY
(1250246) BURN +Z
VERIFY AGS RESIDUALS 500R 501R 502R DELTAVX DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
MCC1
KEY V76E (PGNS PULSE) PGNSMODECONT-AUTO
KEY V93E (BEFORE 1ST MARK REINITW MATRIX)
+2 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
4-24
(LOS OF MSFN) S-BAND - SLEW TO P = 90 Y = 0 S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
404+0 405+0 406+0
(MONITOR 470 471 4721
+9 277R COPY TGT LOS ANGLE
+12 PRO (COMPUTE MCC FOR TPI+15I F 06 81 DELTA VS-LV
PRO F 06 59 DELTA VS-LOS
PRO F 16 45 MKS TFI MGA
+13 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUOS
COMPUTE MCC1 BU
PRO F 37 BB
+14 KEY 41E (RCS THRUSTING) F 50 18 FOAL ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+1425 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+15 F 16 85 NULL DELTA VS
PRO F 37 BB
MCC2
KEY V76E (PGNS PULSE)
4-25
PGNS MODE CONT-AUTO
KEY V93E (BEFORE 1ST MARK REINIT W MATRIX)
+16 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
404+0 405+0 406+0 (MONITOR 470 471 47)shy
+24 277R COPY TGT LOS ANGLE
+27 PRO (COMPUTE MCC FORTPI+30) F 06 81 DELTA VS-LV
PRO F 06 59 DELIA VPS-LOS
PRO F 16 45 MKS TFI MGA
+28 277R COPY TGT LOS ANGLE
COPY R RDOT FROM TAPEMETER FOR BUS
COMPUTE MCC2 BU
F 37 BB PRO
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+2925 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+30 F 16 85 NULL DELTA VS
PRO F 37 BB
KEY OOE (P001
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
4-26
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT KEY V34E (TERMINATE)
KEY V37E47E (AVE G) F 16 83 DELTA VIS
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT VERIFY TAPE METER WITH DSKY
BRAKING GATE 30 FPS - 6000 FT 20 FPS - 3000 FT 10 FPS - 1500 FT 5 FPS - 600 FT
RENDEZVOUS
STATION KEEPING
5-1
50 ABORT PROCEDURE
This is a specific AGS nominal abort procedure due to a PGNS failure between insertion and station keeping
51
5-2
Nominal AGS Procedures
ASSUMPTIONS
AFTER INSERTION
I INSERTION COMPLETE (RFSIDUALS NULLED) g PGNS FAILURE BEFORE INSERTION 3 RAUAR NOT LOCKED ON
(UI CoNT-AGS ATlI[uUE MON-AGS(CDR) RATE ERR MON-CNPTR(LMP) ATTITUDE MON-AGS(LMP) SHFITRUN-+5 DEG X-POINTER-HI MULT RADAR IEST Sw-OFF LNb GMbL-OFF ENG ARM-OFF X-IRANSL-2 JETS DEAD BAND-MAX PGNS MODE CONT-OFF THROTJET-JET CB IMU OIR-ON HH MOVE-AUTO rRACK TTCATNANSL-ENABLE(CDR)
AL CPL-ON MODE SL-AGS RNGAL1 MON-RNbRNGRT RAIE ERR MON-RNDZ HDR(CDR) AVl CoNT(3)-PULSE AGS MODE CONT-AUTO ACA4JET-DISABLE(CDR) TTCATRANSL-DISABLE(LMP) ACA4JET-DISABLE(LMP)
bO7+U Z-AXIS BOPESIGHT 400+2 Z-AXIS STEERING PULSE TO NULL AGS ERRORS POINT Z-AXIS IN DIRECTION OF CSM MODE CONT-ATT HOLD ATT CONT(3)-MODE CONTROL O unnr - ZirF
5-3
SLEW PATE - LO
SLEW RR ANT TO OqON FUAI VERIFY MAX SIGNAL STRENGTH RH MOOE-AUTO TRACK NO TRACK LIGHT OFF -
ATT CONT(3h-PULSE
CHECK INSERTION VELOCITY WITH TAPEMETER COMPARE EAPEMETER WITH AGS STATE VECTOR DATA I
17R RANGE(NOM 2642)
440R RANGE RATE(NOM -425l)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
cSI
+3 417+1 (RADAR FILTER INITIALIZED) 41b+l (NO BOHESIGHT) b03-XXXXX RANGE RATE
+5 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGF
41b+1 CSI ROUTINE 373+o2065 CSi TIME 275+03028 TPI TIME 605+0077 COTANGENT OF LOS TO CSM 41b+1 (ONE-HALF OFBITAL-PERIOD) 411+0 HCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT
610R TIME TO CST
43 RESET ET
267R VELOCITY TO BE GAINED CSI
402R FLTA H
371R DFLTA V CDH
5-4
372R DFLTA T CSICDH
-42 415+1 (No BORESIGHT) bO6-xXXXX RANGE RATE
-40 415+1 (NO BORESIGHT)503-XXXXX RANGE RATE dORESIGHT ON CSM
415+1 316+XXXXX RANGE
-37 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE
-15 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE UORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-2 415+1 (No BOHESIGHT) bO3-XXXXX RANGF RATE
i1uR TIME TO CS
RESEF ET
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-30 COPY ROOT FOR 1ST CSI 81J
BORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-t7 415+1 (NO BORFSIGHT) 50-XXxXx RANGF RATE
267R VELOCITY TO HE GAINED CSI
402R LELTA H
371R OFLTA V COH
372R OELTA T CSICDH
-5 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 blb+XXXXX RANGE
-i2 415+1 (No BORESIGHT) 5n3-XXXXX RANGE RATE
415+1 (NO BORESIGHT)
5-5
503-XXXXX RANGF RATE
COPY Roor FOR 2NO CSI BU
bORESIGHT ON CSM 415+1 316+XXXXX RANGE
TEMPPRESS MON SEL - FUEL MAN
A AND 8 PRESS 181 +-3 PIG TEMPPRESS MON SEL - PRPLNT
A AND B TEMP IND 4ODEG 0 IOODEG F A AND B PRFSS IND 181 +-3 PSIA
tEMPPRESS MON SEL - HEL
A AND 8 PRESS IND PSIA
A QUANTITY IND- -- PERCENT RFMAINING
8 QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4p 2 3 (120 - 190 DFG F)
415+1 (NO BORESIGHT)-17 503-XXXXX RANGE RATE
-15 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
(LOS OF MSFN) S-BAND - SLEW 10 P = +90t Y U S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
-12 415+1 (No 8ORESIGHT)
503-XXXXX RANGE RATE
267R VFLOCITY TU BE GAINED CSI
402R OFLTA H
372R TIME CSICH
371R PREDICTED VEL 10 RE GAINED COH
263R OLT-OF-PLANE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATL
-10 COPY RANGE AND ROOT FOR 3RD CSI 8U
SORESIGH ON CSM 41b+1
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
LM
RENDEZVOUS PROCEDURES
G MISSION
AS-506CSM-107LM-5
May 16 1969
PREPARED BY=m StepWI P Gregaf Orbital Procedu~res Sectioed
APPROVED BY t ~ 62()Miflton C CoWrtella Chief Orbital Procedures Section
1rLiJC J4A-Paul C Kramer Chief Flight Procedures Branch
4- dames W Bilodeau Assistant Chief For Crew Integration Flight Crew Support Division
Chief Night Cfew Support Division
[onaid KSayton ]j- hairman Crew Procedies Control Board
-I-
TABLE OF CONTENTS
PAGE
10 PURPOSE 1-1
20 INTRODUCTION 2-I
30 DISCUSSION OF MAJOR EVENTS 3-1 31 Concentric Sequence Initiation 3-1 32 Constant Delta Height and Plane Change 3-1 33 Terminal Phase Initiation 3-2 34 Midcourse Corrections 3-2 3 5 Braking 3-2
40 NOMINAL PROCEDURES 4-1 41 Commander Tasks 4-1 4 2 LM Pilot Tasks 4-1 43 Abbreviations 4-1 44 Nominal PGNS Procedures 4-3
50 ABORT PROCEDURES 5-I 51 Nominal AGS Procedures 5-2
60 ONBOARD RENDEZVOUS CHARTS 6-1 61 Concentric Sequence Initiation 6-2 62 Constant Delta Height 6-4 63 Terminal Phase Initiation 6-6 64 First Midcourse Correction 6-7 6 5 Second Midcourse Correction 6-8 6 6 Relative Reference Trajectory 6-9
70 REFERENCES 7-1
=i1-
FIGURES
PAGE
Relative Motion Profile (2-1) 2-2
LUNAR ORBIT RENDEZVOUS ATTITUDE TIME HISTORY 2-3
Lift-off - CSI (2-2) 2-3
CDH-TPF (2-3) 2-4
LIST OF ACRONYMS AND ABBREVIATIONS ACQ ADJ AGS AOH AOS AOT APS ATT BU CALIB CB CDH CDR CM CMC CMD CMP COAS CSI CSM CT DAP DH DOI DPS DSKY DV DWN EMS ET FDAI FPS FWD GDC GET GETI GMBL GND HA HGA HOR HORIZ HP IMU INS IT LGC LM
Acquisition Adjust Abort Guidance System Apollo Operations Handbook Acquisition of Signal Alignment Optical Telescope Ascent Propulsion System Attitude Backup Calibration Circuit Breaker Constant Delta Height Commander Command Module Command Module Computer Command Module Commanders Position Command Module Pilot Crew Optical Alignment Sight Concentric Sequence Initiation Command and Service Module Cease Tracking Digital Autopilot Delta Height Descent Orbit Insertion Descent Propulsion System Display and KeyboardDelta Velocity Down Entry Monitor System Event Timer Flight Director Attitude Indicator Feet Per Second Forward Gyro Display Coupler Ground Elapsed Time Ground Elapsed Time of Ignition Gimbal Ground (Mission Control) Apogee Altitude High-Gain Antenna Horizon Horizontal Perigee Altitude Inertial Measurement Unit Insertion Initiate Tracking LM Guidance Computer Lunar Module
LV
-1v-
LMP LOI LOS
MNVR MCC MCCl MCC2 MCC-H MGA MSFN NAV ORDEAL PAD PB PC PDI PGNS PHS PIPA PLM PRO PROG PROP R RCS RDOT REFSMMAT RHC RR SHFT SC SEP SM SXT SYNC TFI THC THETA TIGN TLM TPF TPI TRUN TTCA VG VHF (XXXX) (XXXXX XX)
Lunar Module Pilot Lunar Orbit Injection Line Of Sight Launch Vehicle Maneuver Midcourse Correction First Midcourse Correction Second Midcourse Correction Mission Control Center - Houston Middle Gimbal Angle Manned Space Flight Network Navigation Orbital Rate Drive Earth and Lunar Data Voiced to Crew From Ground Pushbutton Plane Change Powered Descent Initiation Primary Guidance Navigation and Control System Phasing Pulse Integrating Pendulous Accelerometers LM Pitch Angle Proceed Program Propellant Range Reaction Control System Range Rate Reference Stable Member Matrix Rotation Hand Controller Rendezvous Radar Shaft Spacecraft Separation Service Module Sextant Synchronize Time From Ignition Translation Hand Controller Angle Between SC +X Axis and Local Horizontal Time of Ignition Telemetry Terminal Phase Finalization Terminal Phase Initiation Trunnion Translation Thrust Control Assembly Velocity to be Gained Very High Frequency Indicates GET From Liftoff in HoursMinutes Indicates GET From Liftoff in HoursMinutesSeconds
(XXXXXXXXXXXX) (OrdealInertial) Angles (Roll Pitch Yaw) (XXXXXX) Local Vertical DVs
Tracking Stations
ANG BDA CRO CYI GYM HSK HTV MAD MER MIL RED TEX VAN
-v-
Antigua Near Space Support Station Bermuda Near Space Support Station Carnarvon Near Space Support Station Canary Near Space Support Station Guaymas Near Space Support Station Honeysuckle Deep Space Support Station Huntsville Near Space Support Station Madrid Deep Space Support Station Mercury Near Space Support Ship MILA Near Space Support Station Redstone Near Space Support Ship Corpus Christi Near Space Support Station Vanguard Near Space Support Ship
10 PURPOSE
This document contains the primary procedures for the LM-5 active rendezvous with CSM-107 spacecraft in accordance with Detailed Test Objective Section 40 defined in Reference 71
The purpose of the LM Rendezvous Procedures document is to provide a single source of procedures information for use in flight planning in crew training and in preparing onboard data
This is a control document subject to review by all elements of the Apollo Program and to approval by the Procedures Conshyfiguration Control Board Comments should be directed to Mr Stephen P Grega Flight Procedures Branch Flight Crew Support Division Extension 5348
Beyond G mission planning no additional techniques and trajectory information specific to Mission H have been made available as of this date Therefore since Missions G and H are expected to be similar in the area of rendezvous guidance and navigation procedures the G mission final LM Rendezvous Procedures Document will serve -as an H mission preliminary LM Rendezvous and Procedures Document After reviewal by all elements of the Apollo Program and approval by the Procedures Configuration Control Board this document will then evolve into the control document for the Mission H crew procedures
2-1
20 INTRODUCTION
The LM-5CSM-l07 lunar orbit rendezvous exercise will beginduring the twenty-fourth CSM revolution with insertion at 122 35255 and end at approximately 1260000 with post rendezvous station keeping The LM procedures during this period are divided into segments of major activities which are discussed in detail in Section 30
A nominal LM-5CSM-107 mission profile is contained in Figshyure (2-1) This figure shows the locations in time and local horizontal position of the most significant nominal mission events Trajectory data used to generate the mission profile and timeline for procedures development was obtained from Reference 72 The rendezvous navigation update schedule assumed in the procedures is defined in Reference 73
A history of the LM body attitudes during the rendezvous accompanies the major events discussion and is also presented in Figures (2-2) and (2-3) Each figure illustrates the bodyattitudes with respect to the moon sun and earth and indicates FDAI roll pitch and yaw gimbal angles and the ordeal pitch angle for significant events during each lunar orbit
0RBI TR EL
TRAILINGDISPLACEMENT(N MI) 0 0 W60 20240 BE
33I I ] I I I
32 ltrMCCE 1125+-3 C CH (124t24) PLAN CHANGE023 TM)2
R~TC(222
40 1146235 A N MNTTIMETKS FROMISEDRT(GA122plusmn252
-- DAYLIGHT B shy
_ _ _ _ _ _ __E_ _ -- 7 LUNAR IARFAGELM MAJOR EVENTS
122+35 INSERTION 17 124+H7 AGE UPDATE AND ALIGN (R47) 2 122+40 IMU REFSMMAT ALIGN (P52) 1 124+24 CDH THRUSTING (P41) TRAILINGDISPLACEMETIN RI)
3 122+54 AGS UPDATE AND ALIGN (R471 19 124+26 TPI TARGETING IP34 amp AGS) 5 II 20 25 30 4 122+55 CSI TARGETING IP32 amp AGSI 20 124+26-124+51 RR NAVIGATION (P20 18 MARKS) - I I
5 122+54-123+14 RR NAVIGATION (P20 18 MARKS) 21 124+53 AGS UPDATE AND ALIGN (R47)I
6 123+18 COMPUTE CSI BACKUP 22 125+00 COMPUTE TPI BACKUP
7 123+19 AGS UPDATE AND ALIGN (R471 23 125+03 TPI THRUSTING (P411 c
8 123+26 CSI THRUSTING (P411 24 125+05 MCC1 TARGETING IP35) N - M ((25+232
9 123+30 SET W MATRIX 1200025) 25 125+05-125+16 RR NAVIGATION IP20 9 MARKS) 5
2 r INSERT A 10 123+31 CDH TARGETING IP33 amp AGS 26 125+16 COMPUTE MCCI THRUSTING IP41) 5 31 PHAE
11 123+31-123+46 RR NAVIGATION 1P20 14 MARKS) 27 125+18 MCC I THRUSTING (P41)
12 123+47 EXT AV FOR PLANE CHANGE (P20) 28 125+20 MCC2 TARGETING (P351 13 123+54 RCS PLANE CHANGE THRUSTING (P411 29 125+20-125+31 RR NAVIGATION (P20 9 MARKS) 14 123+56 CDH TARGETING (P33 amp AGS) 30 125+31 COMPUTE MCC 2 BACKUP Ideg
15 123+56-124+12 RR NAVIGATION (P20 13 MARKS) 31 125+33 MCC2 THRUSTING [P41)
16 124+15 COMPUTE CDH BACKUP 32 125+48 BRAKING (P47) 27 26TP25+03
33 126+00 STATION KEEPING LT
24
FIGURE 2-1 G MISSION RENDEZVOUS
(CSM-CENTERED RELATIVE MOTION) FOLDOUT FRAME
l D T R2A-e2 TALPFO EDUR ES EPREPAREDBY STEPHENP GRED501I DOUT FRAMW ORBI R B C 0
MISSION G LUNAR ORBIT RENDEZVOUS ATTITUDE TIME HISTORY
OFOR THE LM P33
P20 123+31) (021880)
LMI CSI NrxNMARKS i (123+26+27)
FINAL -
COMP(I123+1l6)
P32 LANDING SITEj P20 30ES (122+50) CSM AT (04650) PRIME MERIDIAN LIFT-OFF
P52 (122+28+11) (122+40)DIRECTION OF (03640)ORBITAL MOTION IS
CLOCKWISE
(18012150)I NERTIAL YAWKLINERTIAL PITCH
ORDEAL PITCH EARTHINERTIAL ROLL
FIGURE 2-2
MISSION G LUNAR ORBIT RENDEZVOUS ATTITUDE TIME HISTORY
FOR THE LM
LM TPF (126+00+00) (01302920)
LM LMC2PLANE CHANGELMPI+30) (123+54+25)
(TPI+30) (0560)(0782400) 7 SUN
P20
(TPI+15) P3
P33(0532480) COMP
---- _ (124+12--- ---
LM TPI (125+02+46) L D (026 627650) (124+24+25)
(0980)
FINAL
DIRECTION OF COMP ORBITAL MOTION IS (124+50)
CLOCKWISE
(18012150)
LL INERTIAL YAW NERTIAL PITCH
ORDEAL PITCH EARTH INERTIAL ROLL
FIGURE 2-3
3-1
30 DISCUSSION OF MAJOR EVENTS
31 Concentric Sequence Initiation
Immediately following Insertion the LM navigated vector will be downlinked to Mission Control Center-Houston this state vector is then uplinked to the CSM The LM commander will perform a Proqram 52 fine alignment to REFSMMAT at approxishymately 12240
The digital autopilot is configured to wide deadband Program P20 is called and an automatic pitch maneuver is initiated to the preferred track attitude At 122 55 CSI targeting parameters are loaded in the PGNS and AGS A period of rendezvous radar marking will then take place from 122-57 to 12315 Upon completion of tracking the LM will obtain an out-of-plane velocity from the CSM to be vectored with the in-plane component of the CSI delta V The CSMs estishymate of out-of-plane velocity is alleged to be better than the LMs estimate (Reference 74)
At approximately 123 20 the LM will voice its CSI solution to the CSM the AGS is updated aligned and targeted in external delta-V with the CDH solution to be excuted Program P41 will then be called and the automatic pitch maneuver bypassed since the burn isto be executed with Z-Axis thrusting The CSI burn occurs nominally at 123 26 27 After verification of the LM CSI burn the CSM will incorporate the LM burn parameters in its CMC LM state vector
32 Constant Delta Height and Plane Change
At 12330 approximately three minutes after the LM CSI burn the W matrix will be set to (200025) and the LM targeting paramters are loaded in both the PGNS and AGS for the CDH maneuver Out-of-plane velocity will then be computed and voiced to the LM from the CSM Program P30 is loaded with the targeting parameters for the LM Plane Change maneuver which will be accomplished in Program P41 30 minutes prior to the CDH maneuver Following the burn the target delta V parameters are voice to the CSM and incorporated into the CMC LM state vector At 12356 the CDH targeting parameters are loaded in both the PGNS and AGS for 1242425 A CDH chart solution is calculated 7 minutes prior to TIG The AGS is updated aligned and targeted in external delta V with the CDH solution to be executed The RCS Thrust Program P41 is called at 12418 and the burn attitude is bypassed since the LM executes CDH by thrusting out individual components of delta V while maintaining radar lock-on
3-2
3 3 Terminal Phase Initiation
Radar tracking is initiated after the CDH maneuver and updating of the LGC continued At 12426 approximately two minutes after the LM CDH burn targeting parameters are loaded in both the PGNS and AGS for the TPI maneuver which will be targeted for a node at intercept Backup measurements are made at the appropriate times The AGS is updated aligned and targeted in external delta V with the TPI solution to be executed The RCS Thrust Program P41 is called at 12456 and the burn attitude is bypassed since the LM is burning along the plus Z-axis with the thrust direction established with the COAS
3 4 Midcourse Corrections
Immediately after TPI the Midcourse Prethrust Program P35 will be called and radar tracking reinitiated Backup measshyurements are made and midcourse corrections chart solutions obtained The MCCl burn will nominally be performed at TPI plus 15 minutes (1251746) If MCCI is to be excuted Program P41 will be called and the burn attitude maneuver is bypassed since the plus Z-axis will remain boresighted at the CSM until docking
Following MCCI Program P35 will be called and targeted for MCC2 at TPI plus 30 minutes (1253246) and executed identishycally to MCCI
3 5 Braking
In preparation for braking the DAP is configured in narrow deadband Program P20 is terminated at 18000 feet but the radar is kept in auto track to provide radar range and range rate displayed on the tapemeter Average G is called by Program P47 prior to braking and attitude hold is selected The braking schedule is followed as contained in Section 4
4-1
40 NOMINAL MISSION PROCEDURES
The procedures included in this section do not specify which crewmember Commander or LM Pilot performs each task These need not be specified since the following basic rules define which crewmember performs each task
41 Commander Tasks
1 All attitude changes whether manual or automatic will be accomplished by the CDR
2 The operation of the DSKY during thrust programs (P40 P41 P42 P47) will be done by the CDR Actual manipulation of the TTCA need not be always done by the CDR but in most cases will be
3 Operation of the rendezvous and landing radar will be done by the CDR
4 The CDR will operate all other systems accessible to only his crew station
42 LM Pilot Tasks
1 AGS operation 2 DSKY operation will be done by the LMP except when keyboard
entries affect the control of spacecraft attitude or thrustshying
3 Backup data logging and chart calculations 4 All logging of maneuver solutions and systems performance 5 The LMP will operate all other systems accessible to only
his crew station
These general rules are guidelines only and may be deviated from by the LM crew if they develop more efficient Task assignments
43 ABBREVIATIONS
The abbreviations used herein are consistant with those in the AOH However in order to condense and simplify the procedures so that they are representative of onboard data a number of addshyitional shorthand conventions have been used To allow the unshyfamiliar reader to understand the procedures contained in this section the following explanations are included
1 AGS - A single asterisk is employed to denote those procedures involving operations to be performed on the DEDA The three number group following an asterisk specifies DEDA address An Rfollowing the address group indicates the address is to be read out A five digit group behind the Rindicates a nominal or expected display If the three number address group is followed by a plus or minus sign a data load is indicated When a single digit follows the plus addition of four zeros behind this digit is assumed Once used these conventions are easily handled and save considerable space
4-2
2 PGNS - The verb-noun addresses in the PGNS are indicated to the left of the procedures column An F is used to indicate a flashing display or absence of an F a static display To the right of the verb-noun on the same line are the contents of the three data registers If numeric quantities appear the DSKY should be correspondingly made to agree by executing a V21 V22 or V23 and performing a data load The procedure of blanking and loading registers is not included since it is repeated often and is highly familiar to the crews
EXAMPLE F 06 33 125-02 46 TIG OF TPI
Expanded this means Load flashing verb 06 noun 33 with the quantity 125 hours 2 minutes and 46 seconds the time of ignition of the RCS engine TPI maneuver Procedurally this is done by keying verb 25 enter loading +000125 in register 1 +00002 in register 2 and +04600 in register 3
If numberic quantities do not follow the verb-noun it is indicated that a computed or information quantity is being displayed via the DSKY If nominal values are listed for possible comparison they appear in parentheses
EXAMPLE- F 06 42 HA HP V
Expanded this means Flashing verb 06 noun 42 has computed height of apogee in register 1 height of perigee in regshyister 2 and velocity to be gained in register 3
3 TIME - The numbers in the left hand column preceded by a plus or minus indicate event timer time referenced to an event Minus indicates event timer counting down to a future event Periodically this same column contains the nominal mission ground elapsed times in parentheses Asterisks following the event time indicate a time critical event which should be accomplished to the nearest second
4-3
4 4 Nominal PGNS Procedures
ASSUMPTIONS
AFTER INSERTION
1 INSERTION COMPLETE (RESIOUALS NULLED) VERIFY V82E (ORBIT) 3 RNDZ RDR LOCKED ON IN MODE II 4 LGC AT FLASHING VERB 37 5 PROPER INITIAL W MATRIX LOADED IN LGC
GUID CONT-PGNS ATTITUDE MON-PGNS(CDR) RATE ERR MON-CMPTR(LMP) ATTITUDE MON-AGS(LMP) SHFTTRUN-+5 DEG X-POINTER-HI MULT RADAR TEST SW-OFF ENG ARM-OFF X-TRANSL-2JETS DEAD BAND-MIN PGNS MODE CONT-AUTO THROTJET-JET CBPGNS IMU OPR-CLOSE RR MODE-LGC TTCATRANSL-ENABLE(COR)
BAL CPL-ON MODE SEL-AGS
RNGALT MON-RNGRNGRT RATE ERR MON-RNDZ RORICOR) ATT CONT-PULSE(3)
AGS MODE CONT-ATT HOLD ACA4JET-DISABLE(CDRJ TTCATRANSL-DISABLE(LMP)
ACA4JET-DISABLE(LMPI
KEY ODE (PO0)
(DOWNLINK LM STATE VECTOR)
KEY V63E (RR SELF TEST)
4-4
F 04 12 00004 00001 PRO
F 16 72 TRUN SHFT PRO
F 16 78 R ROOT VERIFY TAPE METER WITH DSKY
+2 VERIFY INSERTION VELOCITY WITH RNDZ ROR WHERE RANGE = 2642 NM RANGE RATE = -4251 FPS
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
KEY V34E (TERMINATE) KEY V48E (LOAD DAP)
F 01 46 11002 PRO
F 06 47 LMWT CMWT PRO
KEY V56E (KILL AUTO TRACK ENABLE)
+3 KEY V41N72E (COARSE ALIGN RR) F 21 73 +000OOTRUN -077OOSHFT F 04 12 00006 00002 (CONTINUOUS DESIGNATE)
PRO 41 (COARSE ALIGN VERB)
KEY VI6N72E 16 72 MONITOR TRUNSHFT ANGLES
CB PGNS RNDZ RDR-OPEN CB AC BUS A RNDZ RDR-OPEN KEY V44E (TERMINATE RR DESIGNATE)
KEY V83E F 16 54 R ROOT THETA
SET ORDEAL PRO
CS HEATER AOT-CLOSE
CB AOT LAMP-CLOSE
+5 KEY V37E52E (IMU REALIGN)
4-5
410+1 CSI ROUTINE 373+02065 CS TIME 275+03028 TPI TIME
605400777 COTANGENT OF LOS TO-CSM 416+1 (ONE-HALF bRBITAL PERIOD) 411+0 RCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT 310R TIME TO CS
267R VELOCITY TO BE GAINED CSI
402R DELTA H
371R DELTA V CDH
372R _ DELTA T CSICDH
F 04 06 00001 00003 -(REFSMMAT) PRO -
F 50 25 00015 SELECT 1ST STAR ENTR
F 01 70 O02DE LOAD 1ST STAR PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FOAl ANGLES (AUTO MNVRI)
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVR)
F 01 71 002DE
KEY V76E PGNS MODE CONT-ATT HOLD
PRO +10 F 54 71 MARK 1ST STAR
PRO F 01 70 O02DE LOAD 2ND STAR
PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FDA ANGLES -(AUTO MNVRV
F 50 18 FDAI ANGLES (REQUEST PNVRt ENTR (BYPASS MNVR
F 01 71 002DE PGNS MODE CONT-ATT HOLD PRO
-35
4-6
+14 F 54 71 MARK 2ND STAR PRO
F 06 05 STAR ANGLE DIFFERENCE PRO
F 06 93 GYRO TORQUE ANGLES PRO
F 50 25 00014
PRO (CHECK ALIGNMENT IF TIME WILL PERMIT)
F 50 25 00015 SELECT 3RD STAR ENTR
F 01 70 OO2DE LOAD 3RD STAR PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FDAI ANGLES (AUTO MNVR)
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVR)
VERIFY ALIGNMENT VIA AOT
KEY V34E (TERMINATE) F 37 BB
V48E (LOAD DAP) F 01 46 11012
PRO F 06 47 LMWT CMWT
+17 PRO
CB AOT LAMP-OPEN
RESET ET (310R)
(12253) CB AC BUS A RNDZ RDR-CLOSE (WAIT 30 SEC) CB PGNS RNDZ RDR-CLOSE
RR MODE-LGC KEY V37E20E (ACQUIRE RADAR)
PGNS MODE CONT-AUTO F 50 18 FDA ANGLES (REQUEST MNVRJ
PRO (AUTO MNVR) 06 18 FDAI ANGLES (AUTO MNVR)
AGS MODE CONT-AUTO RATEERR MON-CMPTR (LMP)
F 50 18 FDAI ANGLES (REQUEST MNVR)
4-7
ENTR (BYPASS MNVR) NO TRK LT-OFF
F 50 72 RR TRUNSHFT VERIFY RR LOCK ON PRO
DSKY BLANKS
KEY V93E (BEFORE 1ST MARK REINIT W MATRIXI KEY V80E (UPDATE LM SV)
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (i20OOZOO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
400+3 AGS ALIGNshy400R (00000 COMPLETE) 507+0 Z-AXIS BORESIGHT 400+2 ACQUISITION STEERING
CS
(122amp55) KEY V37E32E (CSI)
F 06 11 1 S LOAD TIG CSI FROM DATA PAD (NOM 123S26- 271 PRO
F 06 55 +O000IN +02660E +13000 OMEGAT (CDH 180 DEG AFTER CSI PRO
F 06 37 LOAD TIG TPI FROM DATA PAD (NOM 1251021761 PRO
F 16 45 MKS TFI -00001
-30 COPY RDOT FOR 1ST CSI BU
31OR TIME TO CSI
267R VELOCITY TO BE GAINED CSI
402R DELTA H
371R DELTA V CDH
-22
4-8
372R _ DELTA T CSICDH
KEY V32E (MARKS=5
F 06 75 DELTA H DELTA T CSICDH DELTA T CDHTPI PRO
F 06 81 DELTA VOS-LV (CS) (NOM 501 DELTA VX)
CSI(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (CDH)
(NOM 60 DELTA VX) CDH(82)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
KEY V32E (MARKS=1C)
F 06 75 DELTA H DELTA TCSICDH DELTA TCDHTPI PRD
F 06 81 DELTA VS-LV (CSI) CSI(N811
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 82 DELTA VIS-LV(CDH)
CDH(82)
DELTA VX(LVI
DELTA VY(LV)
DELTA VZ(LV)
-12
4-9
-20 COPY RDOT FOR 2ND CSI BU
F 16 45
F 06 75
F 06 81
F 06 16
F 06 90
PRO MKS TFI -00001
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS NON SEL - PRPLNT A + B TEMP IND 40DEG TO lOODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + 8 PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4v 2 3 (120 - 190 DEG F
(LOS OF MSFN ) S-BAND - SLEW TO P = +90 Y a 0 S-BAND - FWD (OR AFT) S-BAND - DN VOICE BU BIOMED OFF
PRO (FINAL COMP)
267R - VELOCITY TO BE GAINED CSI
402R DELTA H
372R TIME CSICDHL
371R PREDICTED VEL TO BE GAINED CDH
263R OUT-OF-PLANE
DELTA H DELTA TCSICDH DELTA TCDHTPI PRO DELTA VS-LV (CSI)
KEY V9OE (OUT-OF-PLANED
0 LOAD TIG CSI FROM DATA PAD (NOM 12302627) PRO Y YDOT PSI
N90 CSM
YDOT
PRO
-7
4-10
F 06 81 DELTA VS-LV(CSI)
COPY YDOT FROM CSM AND LOAD NEGATIVE IN R2 CSIIN81I
DELTA VX(LV)
DELTA VYILV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (COH)
CDH(82)
DELTA VX(LV)
- DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RANGE AND RDOT FOR 3RD CS BU
COMPUTE CSI BU
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (i2000OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
(TRANSMIT CSI DATA TO CSMI VHF A XMTR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF TELEMETY PCM - LO
KEY VB3E F 16 54 R ROOT THETA
SET ORDEAL PRO
317R RANGE
440R RANGE RATE
4-11
400+3 AGS ALIGN t40OR (00000 COMPLETE)
277R THETA
PRO F 37 BB
-6 KEY 41E (RCS THRUSTING) F 50 18 FDAI-ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTAV 400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTAV 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA RF
TRANSMIT TGT DELTA VS TO CSM AND SYNC COUNTDOWN
16 85 DELTA VS-BODY
502R DELTA VZ (NOM 5Ql)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTAVS-BODY
(123t26t27) BURN +Z
NULL DELTA VS
4-12
VERIFY AGS RESIDUALS 50OR 501R 502R DELTA VX _ DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
CDH
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
KEY V67E (RESET W MATRIX) F 06 99 +0200E +O0020E +00005E
PRO
507+0 Z-AXIS BORESIGHT
(VHF RANGING WITH CSM) VHF A XMTR - VOICERNG VHF B XMTR - OFF VHF B RCVR - ON TELEMETRY PCM - HI
(12331) KEY V37E33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 a TIG CDH (NOM 1242425) -120 amp00 10 (AGS 0 TIME)
(CONVERT TO MINUTES)
411+0 THRUST ALONG Z-BODY AXIS ENTER IF YOU DONT TARGET CSI
373R (NOM 26443 310R TIME TO CDH
4-13
423R DESIRED ALT RATE AT CDH
402R DELTA Hshy
450R DELTA VX
452R DELTA VZ
623+0 Z-AXIS PARALLEL TO CSM PLANE
IPRO F 16 45 MKS TFI -00001
-52 RESET ET
KEY V93E (REINIT W MATRIX WHEN MARKS =4)
KEY V32E (MARKS = 3)
F 06 75 DELTA HCDH DELTA TCDHTPI DELTA TTPI PRO
F 06 81 DELTA VCDH-LV CDH(N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
-47 KEY VSOE (OUT-OF-PLANE)
_ TIG CDH (NOM 124t24t25) -3000 TIME FROM CDH
F 06 16 l1 LOAD TIG PLANE CHANGE (NOM 123amp54-253 PRO
F 06 90 Y YDOT PSI N90 CSM
VYDOT PRO
-42 KEY V32E (MARKS=1O)
F 06 75 DELTA HCDH DELTA TCDIHTPI DELTA TTPITPI PRO
F 06 81 DELTA VCDH-LV
4-14
CDH (NS1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -OO1
KEY V34E (TERMINATE) F 37 B8
PLANE CHANGE
KEY 30E (EXTERNAL DELTA V)
TIG CDH (NOM 124124t25) -3000 TIME FROM CDH
F 06 33 LOAD TIG PLANE CHANGE (NOM 123154T25) PRO
F 06 81 DELTA VS-LV (NOM 00)
-36 COPY RDOT FOR 1ST CDH BU
KEY V90E (OUT-OF-PLANE)
F 06 16 1 1 LOAD TIG PLANE CHANGE (NOM 1231543251 PRO
F 06 90 Y YOOT PSI N90 CSM
YDOT
PRO
F 06 81 DELTA VS-LV(NOM 00)
COPY YDOT AND LOAD NEGATIVE IN R2 PRO
F 06 42 HA HP DELTA V PRO
F 16 45 MKS TFI MGA
PRO
F 37 BB
KEY 41E (RCS THRUSTING)
-30
4-15
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVRI
410+5 EXTERNAL DELTA V 450+0 451-YDOT 452+0 (LOAD CSM -YDOT)
407+0 ROTATE EXTERNAL DELTA V RF
16 95 DELTA VS-BODY
-3035 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATTVHOLD 407+1 FREEZE EXTERNAL DELTAV
F 16 85 DELTA VS-BODY -
NULL DELTA VIS
PRO F 37BB
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
507+0 Z-AXIS BORESIGHT
(12356) KEY 33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 TIG CDH (NOM 124t24t25) -120 OO ZOO (AGS 0 TIME)
(CONVERT TO MINUTES)
373R _ (NOM 2644) 310R TIME TO CDH
423R DESIRED ALT RATE AT CDH
(ADS OF MSFN) S-BAND - SLEW TOP = ACQUIRE HGA LOCK ON VOICE - BUVOICE -- VOICE VERIFY VOICE TLM BIOMED - LEFT (OR RIGHT)
402R DELTAH
4-16
F 16 45
-25
-23
F 06 75
F 06 81
F 16 45
-12
F 06 75
F 06 81
450R DELTA VX
452R DELTA VZ
PRO MKS TFI -00001
KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
COPY ROOT FOR 2ND CDH BU
KEY v32E (MARKS = 5)
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40DEG TO 1OODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + B PRESS IND PSIA
A QUANTITY IND _ PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING a TEMP MON SEL RCS QUAD 1 4 2 3 (120 - 190 DEG F)i
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
CDH(NB1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO MKS TFI -00001
PRO (FINAL COMP)
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
KEY V9OE (OUT-OF-PLANE)
-7
4-17
F 06 16 jj LOAD TIG CDH FROM DATA PAD (NOM 12424251 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT PRO
COPY YOOT FROM CSM AND LOAD NEGATIVE IN R2
CDH(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RDOT FOR 3RD CDH BU
COMPUTE CDH BU
TRANSMIT TGT DELTA VOS TO CSM AND SYNC COUNTDOWN
KEY V47E (INITIALIZE AGS F 06 16 GET OF AGS 0 TIME 120O00OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
KEY V83E F 16 54 R RDOT THETA
SET ORDEAL PRO
317R _ RANGE
440R RANGE RATE 400+3 AGS ALIGN 40OR (00000 COMPLETE)
277R THETA
-6
4-18
PRO F 3 BB
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY V06N86E F 06 86 DELTA VIS-LV
AGS(N86) CHART
DELTA VX(LVD
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
16 85 DELTA VS-BODY
50OR DELTA VX (NOM -0O3)
502R DELTA VZ (NOM 60)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD 407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS BODY
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS 5OOR 50IR 502R DELTA VX -DELTA VY DELTA VZ-
VERIFY PGNS RESIDUALS N85
DELTA VX(LM)
4-19
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
TPI
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO 507+0 Z-AXIS BORESIGHT
(12426) KEY 34E (TPI)
-36 RESET ET
F 06 37 - amp LOAD TIG TPI FROM DATA PAD (NOM 1250246) PRO
F 06 55 +00000 +02660E +13000 OMEGAT PRO
F 16 45 MARKS TFI -00001
-32 KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
-29 KEY V32E (MARKS = 3)
F 06 37 __ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
RESET ET
410+3 TPI SEARCH ROUTINE 307+04300 DELTA T TRANSFER
4-20
-26 310+02600 TFI TPI
303R THETA AT TPI
267R DELTA VTPI
371R DELTA VTPI + DELTA VTPF
KEY V32E (MARKS = 10)
F 06 37 _ _ _ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VIS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
TEMPIPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40ODEG TO IGODEG F A + B PRESS IND 181 +-3 PSIA
TEMPIPRESS MON SEL - HEL
A + B PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD I 4 2 3 (120 - 190 DEG F)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
RESET ET
-13 310+01300 TFI TPI
303R THETA AT TPI
-12 PRO (FINAL COMP) F 06 37 Z TIG TPIj__
4-21
TRANSMIT TIG OF TPI TO CSM-
PRO F 06 58 HP DELTA VTPI DELTA VTRF
PRO F 06 81 DELTA VS-LV
KEY V9OE (OUT-OF-PLANE)
F 06 16 1 LOAD TIG TPI FROM DATA PAD (NOM 12502461 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT
PRO F 06 81 DELTA VS-LV
COPY CSM YDOT AND LOAD NEGATIVE IN R2 N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 59 DELTA VS LOS
N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI MGA
RESET ET
PRO F 37 BB
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (12000t600)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE)
-10
-6
4-22
F 50 16 DOWNLINK COMPLETE PRO (UPDATE COMPLETE)
400+3 AGS ALIGN 400R (00000 COMPLETE)
-9 277R COPY TGT LOS ANGLE
310+00800
303R THETA AT TPI 410+4 DIRECT TRANSFER AT ET=-8 404+0 405+0 406+0 (MONITOR 470 471 4721
373R TIG TPI
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
KEY 41E (RCS THRUSTING) F 50 18 FOAl ANGLES (REQUEST MNVRI
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
-5 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUS
400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
COMPUTE TPI BU
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
4-23
1685 DELTA VS-BODY
50OR DELTA VX(NOM -115)
502R DELTA VZ(NOM 229)
-Z35 OSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS-BODY
(1250246) BURN +Z
VERIFY AGS RESIDUALS 500R 501R 502R DELTAVX DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
MCC1
KEY V76E (PGNS PULSE) PGNSMODECONT-AUTO
KEY V93E (BEFORE 1ST MARK REINITW MATRIX)
+2 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
4-24
(LOS OF MSFN) S-BAND - SLEW TO P = 90 Y = 0 S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
404+0 405+0 406+0
(MONITOR 470 471 4721
+9 277R COPY TGT LOS ANGLE
+12 PRO (COMPUTE MCC FOR TPI+15I F 06 81 DELTA VS-LV
PRO F 06 59 DELTA VS-LOS
PRO F 16 45 MKS TFI MGA
+13 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUOS
COMPUTE MCC1 BU
PRO F 37 BB
+14 KEY 41E (RCS THRUSTING) F 50 18 FOAL ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+1425 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+15 F 16 85 NULL DELTA VS
PRO F 37 BB
MCC2
KEY V76E (PGNS PULSE)
4-25
PGNS MODE CONT-AUTO
KEY V93E (BEFORE 1ST MARK REINIT W MATRIX)
+16 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
404+0 405+0 406+0 (MONITOR 470 471 47)shy
+24 277R COPY TGT LOS ANGLE
+27 PRO (COMPUTE MCC FORTPI+30) F 06 81 DELTA VS-LV
PRO F 06 59 DELIA VPS-LOS
PRO F 16 45 MKS TFI MGA
+28 277R COPY TGT LOS ANGLE
COPY R RDOT FROM TAPEMETER FOR BUS
COMPUTE MCC2 BU
F 37 BB PRO
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+2925 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+30 F 16 85 NULL DELTA VS
PRO F 37 BB
KEY OOE (P001
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
4-26
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT KEY V34E (TERMINATE)
KEY V37E47E (AVE G) F 16 83 DELTA VIS
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT VERIFY TAPE METER WITH DSKY
BRAKING GATE 30 FPS - 6000 FT 20 FPS - 3000 FT 10 FPS - 1500 FT 5 FPS - 600 FT
RENDEZVOUS
STATION KEEPING
5-1
50 ABORT PROCEDURE
This is a specific AGS nominal abort procedure due to a PGNS failure between insertion and station keeping
51
5-2
Nominal AGS Procedures
ASSUMPTIONS
AFTER INSERTION
I INSERTION COMPLETE (RFSIDUALS NULLED) g PGNS FAILURE BEFORE INSERTION 3 RAUAR NOT LOCKED ON
(UI CoNT-AGS ATlI[uUE MON-AGS(CDR) RATE ERR MON-CNPTR(LMP) ATTITUDE MON-AGS(LMP) SHFITRUN-+5 DEG X-POINTER-HI MULT RADAR IEST Sw-OFF LNb GMbL-OFF ENG ARM-OFF X-IRANSL-2 JETS DEAD BAND-MAX PGNS MODE CONT-OFF THROTJET-JET CB IMU OIR-ON HH MOVE-AUTO rRACK TTCATNANSL-ENABLE(CDR)
AL CPL-ON MODE SL-AGS RNGAL1 MON-RNbRNGRT RAIE ERR MON-RNDZ HDR(CDR) AVl CoNT(3)-PULSE AGS MODE CONT-AUTO ACA4JET-DISABLE(CDR) TTCATRANSL-DISABLE(LMP) ACA4JET-DISABLE(LMP)
bO7+U Z-AXIS BOPESIGHT 400+2 Z-AXIS STEERING PULSE TO NULL AGS ERRORS POINT Z-AXIS IN DIRECTION OF CSM MODE CONT-ATT HOLD ATT CONT(3)-MODE CONTROL O unnr - ZirF
5-3
SLEW PATE - LO
SLEW RR ANT TO OqON FUAI VERIFY MAX SIGNAL STRENGTH RH MOOE-AUTO TRACK NO TRACK LIGHT OFF -
ATT CONT(3h-PULSE
CHECK INSERTION VELOCITY WITH TAPEMETER COMPARE EAPEMETER WITH AGS STATE VECTOR DATA I
17R RANGE(NOM 2642)
440R RANGE RATE(NOM -425l)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
cSI
+3 417+1 (RADAR FILTER INITIALIZED) 41b+l (NO BOHESIGHT) b03-XXXXX RANGE RATE
+5 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGF
41b+1 CSI ROUTINE 373+o2065 CSi TIME 275+03028 TPI TIME 605+0077 COTANGENT OF LOS TO CSM 41b+1 (ONE-HALF OFBITAL-PERIOD) 411+0 HCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT
610R TIME TO CST
43 RESET ET
267R VELOCITY TO BE GAINED CSI
402R FLTA H
371R DFLTA V CDH
5-4
372R DFLTA T CSICDH
-42 415+1 (No BORESIGHT) bO6-xXXXX RANGE RATE
-40 415+1 (NO BORESIGHT)503-XXXXX RANGE RATE dORESIGHT ON CSM
415+1 316+XXXXX RANGE
-37 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE
-15 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE UORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-2 415+1 (No BOHESIGHT) bO3-XXXXX RANGF RATE
i1uR TIME TO CS
RESEF ET
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-30 COPY ROOT FOR 1ST CSI 81J
BORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-t7 415+1 (NO BORFSIGHT) 50-XXxXx RANGF RATE
267R VELOCITY TO HE GAINED CSI
402R LELTA H
371R OFLTA V COH
372R OELTA T CSICDH
-5 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 blb+XXXXX RANGE
-i2 415+1 (No BORESIGHT) 5n3-XXXXX RANGE RATE
415+1 (NO BORESIGHT)
5-5
503-XXXXX RANGF RATE
COPY Roor FOR 2NO CSI BU
bORESIGHT ON CSM 415+1 316+XXXXX RANGE
TEMPPRESS MON SEL - FUEL MAN
A AND 8 PRESS 181 +-3 PIG TEMPPRESS MON SEL - PRPLNT
A AND B TEMP IND 4ODEG 0 IOODEG F A AND B PRFSS IND 181 +-3 PSIA
tEMPPRESS MON SEL - HEL
A AND 8 PRESS IND PSIA
A QUANTITY IND- -- PERCENT RFMAINING
8 QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4p 2 3 (120 - 190 DFG F)
415+1 (NO BORESIGHT)-17 503-XXXXX RANGE RATE
-15 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
(LOS OF MSFN) S-BAND - SLEW 10 P = +90t Y U S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
-12 415+1 (No 8ORESIGHT)
503-XXXXX RANGE RATE
267R VFLOCITY TU BE GAINED CSI
402R OFLTA H
372R TIME CSICH
371R PREDICTED VEL 10 RE GAINED COH
263R OLT-OF-PLANE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATL
-10 COPY RANGE AND ROOT FOR 3RD CSI 8U
SORESIGH ON CSM 41b+1
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
-I-
TABLE OF CONTENTS
PAGE
10 PURPOSE 1-1
20 INTRODUCTION 2-I
30 DISCUSSION OF MAJOR EVENTS 3-1 31 Concentric Sequence Initiation 3-1 32 Constant Delta Height and Plane Change 3-1 33 Terminal Phase Initiation 3-2 34 Midcourse Corrections 3-2 3 5 Braking 3-2
40 NOMINAL PROCEDURES 4-1 41 Commander Tasks 4-1 4 2 LM Pilot Tasks 4-1 43 Abbreviations 4-1 44 Nominal PGNS Procedures 4-3
50 ABORT PROCEDURES 5-I 51 Nominal AGS Procedures 5-2
60 ONBOARD RENDEZVOUS CHARTS 6-1 61 Concentric Sequence Initiation 6-2 62 Constant Delta Height 6-4 63 Terminal Phase Initiation 6-6 64 First Midcourse Correction 6-7 6 5 Second Midcourse Correction 6-8 6 6 Relative Reference Trajectory 6-9
70 REFERENCES 7-1
=i1-
FIGURES
PAGE
Relative Motion Profile (2-1) 2-2
LUNAR ORBIT RENDEZVOUS ATTITUDE TIME HISTORY 2-3
Lift-off - CSI (2-2) 2-3
CDH-TPF (2-3) 2-4
LIST OF ACRONYMS AND ABBREVIATIONS ACQ ADJ AGS AOH AOS AOT APS ATT BU CALIB CB CDH CDR CM CMC CMD CMP COAS CSI CSM CT DAP DH DOI DPS DSKY DV DWN EMS ET FDAI FPS FWD GDC GET GETI GMBL GND HA HGA HOR HORIZ HP IMU INS IT LGC LM
Acquisition Adjust Abort Guidance System Apollo Operations Handbook Acquisition of Signal Alignment Optical Telescope Ascent Propulsion System Attitude Backup Calibration Circuit Breaker Constant Delta Height Commander Command Module Command Module Computer Command Module Commanders Position Command Module Pilot Crew Optical Alignment Sight Concentric Sequence Initiation Command and Service Module Cease Tracking Digital Autopilot Delta Height Descent Orbit Insertion Descent Propulsion System Display and KeyboardDelta Velocity Down Entry Monitor System Event Timer Flight Director Attitude Indicator Feet Per Second Forward Gyro Display Coupler Ground Elapsed Time Ground Elapsed Time of Ignition Gimbal Ground (Mission Control) Apogee Altitude High-Gain Antenna Horizon Horizontal Perigee Altitude Inertial Measurement Unit Insertion Initiate Tracking LM Guidance Computer Lunar Module
LV
-1v-
LMP LOI LOS
MNVR MCC MCCl MCC2 MCC-H MGA MSFN NAV ORDEAL PAD PB PC PDI PGNS PHS PIPA PLM PRO PROG PROP R RCS RDOT REFSMMAT RHC RR SHFT SC SEP SM SXT SYNC TFI THC THETA TIGN TLM TPF TPI TRUN TTCA VG VHF (XXXX) (XXXXX XX)
Lunar Module Pilot Lunar Orbit Injection Line Of Sight Launch Vehicle Maneuver Midcourse Correction First Midcourse Correction Second Midcourse Correction Mission Control Center - Houston Middle Gimbal Angle Manned Space Flight Network Navigation Orbital Rate Drive Earth and Lunar Data Voiced to Crew From Ground Pushbutton Plane Change Powered Descent Initiation Primary Guidance Navigation and Control System Phasing Pulse Integrating Pendulous Accelerometers LM Pitch Angle Proceed Program Propellant Range Reaction Control System Range Rate Reference Stable Member Matrix Rotation Hand Controller Rendezvous Radar Shaft Spacecraft Separation Service Module Sextant Synchronize Time From Ignition Translation Hand Controller Angle Between SC +X Axis and Local Horizontal Time of Ignition Telemetry Terminal Phase Finalization Terminal Phase Initiation Trunnion Translation Thrust Control Assembly Velocity to be Gained Very High Frequency Indicates GET From Liftoff in HoursMinutes Indicates GET From Liftoff in HoursMinutesSeconds
(XXXXXXXXXXXX) (OrdealInertial) Angles (Roll Pitch Yaw) (XXXXXX) Local Vertical DVs
Tracking Stations
ANG BDA CRO CYI GYM HSK HTV MAD MER MIL RED TEX VAN
-v-
Antigua Near Space Support Station Bermuda Near Space Support Station Carnarvon Near Space Support Station Canary Near Space Support Station Guaymas Near Space Support Station Honeysuckle Deep Space Support Station Huntsville Near Space Support Station Madrid Deep Space Support Station Mercury Near Space Support Ship MILA Near Space Support Station Redstone Near Space Support Ship Corpus Christi Near Space Support Station Vanguard Near Space Support Ship
10 PURPOSE
This document contains the primary procedures for the LM-5 active rendezvous with CSM-107 spacecraft in accordance with Detailed Test Objective Section 40 defined in Reference 71
The purpose of the LM Rendezvous Procedures document is to provide a single source of procedures information for use in flight planning in crew training and in preparing onboard data
This is a control document subject to review by all elements of the Apollo Program and to approval by the Procedures Conshyfiguration Control Board Comments should be directed to Mr Stephen P Grega Flight Procedures Branch Flight Crew Support Division Extension 5348
Beyond G mission planning no additional techniques and trajectory information specific to Mission H have been made available as of this date Therefore since Missions G and H are expected to be similar in the area of rendezvous guidance and navigation procedures the G mission final LM Rendezvous Procedures Document will serve -as an H mission preliminary LM Rendezvous and Procedures Document After reviewal by all elements of the Apollo Program and approval by the Procedures Configuration Control Board this document will then evolve into the control document for the Mission H crew procedures
2-1
20 INTRODUCTION
The LM-5CSM-l07 lunar orbit rendezvous exercise will beginduring the twenty-fourth CSM revolution with insertion at 122 35255 and end at approximately 1260000 with post rendezvous station keeping The LM procedures during this period are divided into segments of major activities which are discussed in detail in Section 30
A nominal LM-5CSM-107 mission profile is contained in Figshyure (2-1) This figure shows the locations in time and local horizontal position of the most significant nominal mission events Trajectory data used to generate the mission profile and timeline for procedures development was obtained from Reference 72 The rendezvous navigation update schedule assumed in the procedures is defined in Reference 73
A history of the LM body attitudes during the rendezvous accompanies the major events discussion and is also presented in Figures (2-2) and (2-3) Each figure illustrates the bodyattitudes with respect to the moon sun and earth and indicates FDAI roll pitch and yaw gimbal angles and the ordeal pitch angle for significant events during each lunar orbit
0RBI TR EL
TRAILINGDISPLACEMENT(N MI) 0 0 W60 20240 BE
33I I ] I I I
32 ltrMCCE 1125+-3 C CH (124t24) PLAN CHANGE023 TM)2
R~TC(222
40 1146235 A N MNTTIMETKS FROMISEDRT(GA122plusmn252
-- DAYLIGHT B shy
_ _ _ _ _ _ __E_ _ -- 7 LUNAR IARFAGELM MAJOR EVENTS
122+35 INSERTION 17 124+H7 AGE UPDATE AND ALIGN (R47) 2 122+40 IMU REFSMMAT ALIGN (P52) 1 124+24 CDH THRUSTING (P41) TRAILINGDISPLACEMETIN RI)
3 122+54 AGS UPDATE AND ALIGN (R471 19 124+26 TPI TARGETING IP34 amp AGS) 5 II 20 25 30 4 122+55 CSI TARGETING IP32 amp AGSI 20 124+26-124+51 RR NAVIGATION (P20 18 MARKS) - I I
5 122+54-123+14 RR NAVIGATION (P20 18 MARKS) 21 124+53 AGS UPDATE AND ALIGN (R47)I
6 123+18 COMPUTE CSI BACKUP 22 125+00 COMPUTE TPI BACKUP
7 123+19 AGS UPDATE AND ALIGN (R471 23 125+03 TPI THRUSTING (P411 c
8 123+26 CSI THRUSTING (P411 24 125+05 MCC1 TARGETING IP35) N - M ((25+232
9 123+30 SET W MATRIX 1200025) 25 125+05-125+16 RR NAVIGATION IP20 9 MARKS) 5
2 r INSERT A 10 123+31 CDH TARGETING IP33 amp AGS 26 125+16 COMPUTE MCCI THRUSTING IP41) 5 31 PHAE
11 123+31-123+46 RR NAVIGATION 1P20 14 MARKS) 27 125+18 MCC I THRUSTING (P41)
12 123+47 EXT AV FOR PLANE CHANGE (P20) 28 125+20 MCC2 TARGETING (P351 13 123+54 RCS PLANE CHANGE THRUSTING (P411 29 125+20-125+31 RR NAVIGATION (P20 9 MARKS) 14 123+56 CDH TARGETING (P33 amp AGS) 30 125+31 COMPUTE MCC 2 BACKUP Ideg
15 123+56-124+12 RR NAVIGATION (P20 13 MARKS) 31 125+33 MCC2 THRUSTING [P41)
16 124+15 COMPUTE CDH BACKUP 32 125+48 BRAKING (P47) 27 26TP25+03
33 126+00 STATION KEEPING LT
24
FIGURE 2-1 G MISSION RENDEZVOUS
(CSM-CENTERED RELATIVE MOTION) FOLDOUT FRAME
l D T R2A-e2 TALPFO EDUR ES EPREPAREDBY STEPHENP GRED501I DOUT FRAMW ORBI R B C 0
MISSION G LUNAR ORBIT RENDEZVOUS ATTITUDE TIME HISTORY
OFOR THE LM P33
P20 123+31) (021880)
LMI CSI NrxNMARKS i (123+26+27)
FINAL -
COMP(I123+1l6)
P32 LANDING SITEj P20 30ES (122+50) CSM AT (04650) PRIME MERIDIAN LIFT-OFF
P52 (122+28+11) (122+40)DIRECTION OF (03640)ORBITAL MOTION IS
CLOCKWISE
(18012150)I NERTIAL YAWKLINERTIAL PITCH
ORDEAL PITCH EARTHINERTIAL ROLL
FIGURE 2-2
MISSION G LUNAR ORBIT RENDEZVOUS ATTITUDE TIME HISTORY
FOR THE LM
LM TPF (126+00+00) (01302920)
LM LMC2PLANE CHANGELMPI+30) (123+54+25)
(TPI+30) (0560)(0782400) 7 SUN
P20
(TPI+15) P3
P33(0532480) COMP
---- _ (124+12--- ---
LM TPI (125+02+46) L D (026 627650) (124+24+25)
(0980)
FINAL
DIRECTION OF COMP ORBITAL MOTION IS (124+50)
CLOCKWISE
(18012150)
LL INERTIAL YAW NERTIAL PITCH
ORDEAL PITCH EARTH INERTIAL ROLL
FIGURE 2-3
3-1
30 DISCUSSION OF MAJOR EVENTS
31 Concentric Sequence Initiation
Immediately following Insertion the LM navigated vector will be downlinked to Mission Control Center-Houston this state vector is then uplinked to the CSM The LM commander will perform a Proqram 52 fine alignment to REFSMMAT at approxishymately 12240
The digital autopilot is configured to wide deadband Program P20 is called and an automatic pitch maneuver is initiated to the preferred track attitude At 122 55 CSI targeting parameters are loaded in the PGNS and AGS A period of rendezvous radar marking will then take place from 122-57 to 12315 Upon completion of tracking the LM will obtain an out-of-plane velocity from the CSM to be vectored with the in-plane component of the CSI delta V The CSMs estishymate of out-of-plane velocity is alleged to be better than the LMs estimate (Reference 74)
At approximately 123 20 the LM will voice its CSI solution to the CSM the AGS is updated aligned and targeted in external delta-V with the CDH solution to be excuted Program P41 will then be called and the automatic pitch maneuver bypassed since the burn isto be executed with Z-Axis thrusting The CSI burn occurs nominally at 123 26 27 After verification of the LM CSI burn the CSM will incorporate the LM burn parameters in its CMC LM state vector
32 Constant Delta Height and Plane Change
At 12330 approximately three minutes after the LM CSI burn the W matrix will be set to (200025) and the LM targeting paramters are loaded in both the PGNS and AGS for the CDH maneuver Out-of-plane velocity will then be computed and voiced to the LM from the CSM Program P30 is loaded with the targeting parameters for the LM Plane Change maneuver which will be accomplished in Program P41 30 minutes prior to the CDH maneuver Following the burn the target delta V parameters are voice to the CSM and incorporated into the CMC LM state vector At 12356 the CDH targeting parameters are loaded in both the PGNS and AGS for 1242425 A CDH chart solution is calculated 7 minutes prior to TIG The AGS is updated aligned and targeted in external delta V with the CDH solution to be executed The RCS Thrust Program P41 is called at 12418 and the burn attitude is bypassed since the LM executes CDH by thrusting out individual components of delta V while maintaining radar lock-on
3-2
3 3 Terminal Phase Initiation
Radar tracking is initiated after the CDH maneuver and updating of the LGC continued At 12426 approximately two minutes after the LM CDH burn targeting parameters are loaded in both the PGNS and AGS for the TPI maneuver which will be targeted for a node at intercept Backup measurements are made at the appropriate times The AGS is updated aligned and targeted in external delta V with the TPI solution to be executed The RCS Thrust Program P41 is called at 12456 and the burn attitude is bypassed since the LM is burning along the plus Z-axis with the thrust direction established with the COAS
3 4 Midcourse Corrections
Immediately after TPI the Midcourse Prethrust Program P35 will be called and radar tracking reinitiated Backup measshyurements are made and midcourse corrections chart solutions obtained The MCCl burn will nominally be performed at TPI plus 15 minutes (1251746) If MCCI is to be excuted Program P41 will be called and the burn attitude maneuver is bypassed since the plus Z-axis will remain boresighted at the CSM until docking
Following MCCI Program P35 will be called and targeted for MCC2 at TPI plus 30 minutes (1253246) and executed identishycally to MCCI
3 5 Braking
In preparation for braking the DAP is configured in narrow deadband Program P20 is terminated at 18000 feet but the radar is kept in auto track to provide radar range and range rate displayed on the tapemeter Average G is called by Program P47 prior to braking and attitude hold is selected The braking schedule is followed as contained in Section 4
4-1
40 NOMINAL MISSION PROCEDURES
The procedures included in this section do not specify which crewmember Commander or LM Pilot performs each task These need not be specified since the following basic rules define which crewmember performs each task
41 Commander Tasks
1 All attitude changes whether manual or automatic will be accomplished by the CDR
2 The operation of the DSKY during thrust programs (P40 P41 P42 P47) will be done by the CDR Actual manipulation of the TTCA need not be always done by the CDR but in most cases will be
3 Operation of the rendezvous and landing radar will be done by the CDR
4 The CDR will operate all other systems accessible to only his crew station
42 LM Pilot Tasks
1 AGS operation 2 DSKY operation will be done by the LMP except when keyboard
entries affect the control of spacecraft attitude or thrustshying
3 Backup data logging and chart calculations 4 All logging of maneuver solutions and systems performance 5 The LMP will operate all other systems accessible to only
his crew station
These general rules are guidelines only and may be deviated from by the LM crew if they develop more efficient Task assignments
43 ABBREVIATIONS
The abbreviations used herein are consistant with those in the AOH However in order to condense and simplify the procedures so that they are representative of onboard data a number of addshyitional shorthand conventions have been used To allow the unshyfamiliar reader to understand the procedures contained in this section the following explanations are included
1 AGS - A single asterisk is employed to denote those procedures involving operations to be performed on the DEDA The three number group following an asterisk specifies DEDA address An Rfollowing the address group indicates the address is to be read out A five digit group behind the Rindicates a nominal or expected display If the three number address group is followed by a plus or minus sign a data load is indicated When a single digit follows the plus addition of four zeros behind this digit is assumed Once used these conventions are easily handled and save considerable space
4-2
2 PGNS - The verb-noun addresses in the PGNS are indicated to the left of the procedures column An F is used to indicate a flashing display or absence of an F a static display To the right of the verb-noun on the same line are the contents of the three data registers If numeric quantities appear the DSKY should be correspondingly made to agree by executing a V21 V22 or V23 and performing a data load The procedure of blanking and loading registers is not included since it is repeated often and is highly familiar to the crews
EXAMPLE F 06 33 125-02 46 TIG OF TPI
Expanded this means Load flashing verb 06 noun 33 with the quantity 125 hours 2 minutes and 46 seconds the time of ignition of the RCS engine TPI maneuver Procedurally this is done by keying verb 25 enter loading +000125 in register 1 +00002 in register 2 and +04600 in register 3
If numberic quantities do not follow the verb-noun it is indicated that a computed or information quantity is being displayed via the DSKY If nominal values are listed for possible comparison they appear in parentheses
EXAMPLE- F 06 42 HA HP V
Expanded this means Flashing verb 06 noun 42 has computed height of apogee in register 1 height of perigee in regshyister 2 and velocity to be gained in register 3
3 TIME - The numbers in the left hand column preceded by a plus or minus indicate event timer time referenced to an event Minus indicates event timer counting down to a future event Periodically this same column contains the nominal mission ground elapsed times in parentheses Asterisks following the event time indicate a time critical event which should be accomplished to the nearest second
4-3
4 4 Nominal PGNS Procedures
ASSUMPTIONS
AFTER INSERTION
1 INSERTION COMPLETE (RESIOUALS NULLED) VERIFY V82E (ORBIT) 3 RNDZ RDR LOCKED ON IN MODE II 4 LGC AT FLASHING VERB 37 5 PROPER INITIAL W MATRIX LOADED IN LGC
GUID CONT-PGNS ATTITUDE MON-PGNS(CDR) RATE ERR MON-CMPTR(LMP) ATTITUDE MON-AGS(LMP) SHFTTRUN-+5 DEG X-POINTER-HI MULT RADAR TEST SW-OFF ENG ARM-OFF X-TRANSL-2JETS DEAD BAND-MIN PGNS MODE CONT-AUTO THROTJET-JET CBPGNS IMU OPR-CLOSE RR MODE-LGC TTCATRANSL-ENABLE(COR)
BAL CPL-ON MODE SEL-AGS
RNGALT MON-RNGRNGRT RATE ERR MON-RNDZ RORICOR) ATT CONT-PULSE(3)
AGS MODE CONT-ATT HOLD ACA4JET-DISABLE(CDRJ TTCATRANSL-DISABLE(LMP)
ACA4JET-DISABLE(LMPI
KEY ODE (PO0)
(DOWNLINK LM STATE VECTOR)
KEY V63E (RR SELF TEST)
4-4
F 04 12 00004 00001 PRO
F 16 72 TRUN SHFT PRO
F 16 78 R ROOT VERIFY TAPE METER WITH DSKY
+2 VERIFY INSERTION VELOCITY WITH RNDZ ROR WHERE RANGE = 2642 NM RANGE RATE = -4251 FPS
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
KEY V34E (TERMINATE) KEY V48E (LOAD DAP)
F 01 46 11002 PRO
F 06 47 LMWT CMWT PRO
KEY V56E (KILL AUTO TRACK ENABLE)
+3 KEY V41N72E (COARSE ALIGN RR) F 21 73 +000OOTRUN -077OOSHFT F 04 12 00006 00002 (CONTINUOUS DESIGNATE)
PRO 41 (COARSE ALIGN VERB)
KEY VI6N72E 16 72 MONITOR TRUNSHFT ANGLES
CB PGNS RNDZ RDR-OPEN CB AC BUS A RNDZ RDR-OPEN KEY V44E (TERMINATE RR DESIGNATE)
KEY V83E F 16 54 R ROOT THETA
SET ORDEAL PRO
CS HEATER AOT-CLOSE
CB AOT LAMP-CLOSE
+5 KEY V37E52E (IMU REALIGN)
4-5
410+1 CSI ROUTINE 373+02065 CS TIME 275+03028 TPI TIME
605400777 COTANGENT OF LOS TO-CSM 416+1 (ONE-HALF bRBITAL PERIOD) 411+0 RCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT 310R TIME TO CS
267R VELOCITY TO BE GAINED CSI
402R DELTA H
371R DELTA V CDH
372R _ DELTA T CSICDH
F 04 06 00001 00003 -(REFSMMAT) PRO -
F 50 25 00015 SELECT 1ST STAR ENTR
F 01 70 O02DE LOAD 1ST STAR PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FOAl ANGLES (AUTO MNVRI)
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVR)
F 01 71 002DE
KEY V76E PGNS MODE CONT-ATT HOLD
PRO +10 F 54 71 MARK 1ST STAR
PRO F 01 70 O02DE LOAD 2ND STAR
PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FDA ANGLES -(AUTO MNVRV
F 50 18 FDAI ANGLES (REQUEST PNVRt ENTR (BYPASS MNVR
F 01 71 002DE PGNS MODE CONT-ATT HOLD PRO
-35
4-6
+14 F 54 71 MARK 2ND STAR PRO
F 06 05 STAR ANGLE DIFFERENCE PRO
F 06 93 GYRO TORQUE ANGLES PRO
F 50 25 00014
PRO (CHECK ALIGNMENT IF TIME WILL PERMIT)
F 50 25 00015 SELECT 3RD STAR ENTR
F 01 70 OO2DE LOAD 3RD STAR PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FDAI ANGLES (AUTO MNVR)
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVR)
VERIFY ALIGNMENT VIA AOT
KEY V34E (TERMINATE) F 37 BB
V48E (LOAD DAP) F 01 46 11012
PRO F 06 47 LMWT CMWT
+17 PRO
CB AOT LAMP-OPEN
RESET ET (310R)
(12253) CB AC BUS A RNDZ RDR-CLOSE (WAIT 30 SEC) CB PGNS RNDZ RDR-CLOSE
RR MODE-LGC KEY V37E20E (ACQUIRE RADAR)
PGNS MODE CONT-AUTO F 50 18 FDA ANGLES (REQUEST MNVRJ
PRO (AUTO MNVR) 06 18 FDAI ANGLES (AUTO MNVR)
AGS MODE CONT-AUTO RATEERR MON-CMPTR (LMP)
F 50 18 FDAI ANGLES (REQUEST MNVR)
4-7
ENTR (BYPASS MNVR) NO TRK LT-OFF
F 50 72 RR TRUNSHFT VERIFY RR LOCK ON PRO
DSKY BLANKS
KEY V93E (BEFORE 1ST MARK REINIT W MATRIXI KEY V80E (UPDATE LM SV)
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (i20OOZOO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
400+3 AGS ALIGNshy400R (00000 COMPLETE) 507+0 Z-AXIS BORESIGHT 400+2 ACQUISITION STEERING
CS
(122amp55) KEY V37E32E (CSI)
F 06 11 1 S LOAD TIG CSI FROM DATA PAD (NOM 123S26- 271 PRO
F 06 55 +O000IN +02660E +13000 OMEGAT (CDH 180 DEG AFTER CSI PRO
F 06 37 LOAD TIG TPI FROM DATA PAD (NOM 1251021761 PRO
F 16 45 MKS TFI -00001
-30 COPY RDOT FOR 1ST CSI BU
31OR TIME TO CSI
267R VELOCITY TO BE GAINED CSI
402R DELTA H
371R DELTA V CDH
-22
4-8
372R _ DELTA T CSICDH
KEY V32E (MARKS=5
F 06 75 DELTA H DELTA T CSICDH DELTA T CDHTPI PRO
F 06 81 DELTA VOS-LV (CS) (NOM 501 DELTA VX)
CSI(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (CDH)
(NOM 60 DELTA VX) CDH(82)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
KEY V32E (MARKS=1C)
F 06 75 DELTA H DELTA TCSICDH DELTA TCDHTPI PRD
F 06 81 DELTA VS-LV (CSI) CSI(N811
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 82 DELTA VIS-LV(CDH)
CDH(82)
DELTA VX(LVI
DELTA VY(LV)
DELTA VZ(LV)
-12
4-9
-20 COPY RDOT FOR 2ND CSI BU
F 16 45
F 06 75
F 06 81
F 06 16
F 06 90
PRO MKS TFI -00001
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS NON SEL - PRPLNT A + B TEMP IND 40DEG TO lOODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + 8 PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4v 2 3 (120 - 190 DEG F
(LOS OF MSFN ) S-BAND - SLEW TO P = +90 Y a 0 S-BAND - FWD (OR AFT) S-BAND - DN VOICE BU BIOMED OFF
PRO (FINAL COMP)
267R - VELOCITY TO BE GAINED CSI
402R DELTA H
372R TIME CSICDHL
371R PREDICTED VEL TO BE GAINED CDH
263R OUT-OF-PLANE
DELTA H DELTA TCSICDH DELTA TCDHTPI PRO DELTA VS-LV (CSI)
KEY V9OE (OUT-OF-PLANED
0 LOAD TIG CSI FROM DATA PAD (NOM 12302627) PRO Y YDOT PSI
N90 CSM
YDOT
PRO
-7
4-10
F 06 81 DELTA VS-LV(CSI)
COPY YDOT FROM CSM AND LOAD NEGATIVE IN R2 CSIIN81I
DELTA VX(LV)
DELTA VYILV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (COH)
CDH(82)
DELTA VX(LV)
- DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RANGE AND RDOT FOR 3RD CS BU
COMPUTE CSI BU
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (i2000OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
(TRANSMIT CSI DATA TO CSMI VHF A XMTR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF TELEMETY PCM - LO
KEY VB3E F 16 54 R ROOT THETA
SET ORDEAL PRO
317R RANGE
440R RANGE RATE
4-11
400+3 AGS ALIGN t40OR (00000 COMPLETE)
277R THETA
PRO F 37 BB
-6 KEY 41E (RCS THRUSTING) F 50 18 FDAI-ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTAV 400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTAV 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA RF
TRANSMIT TGT DELTA VS TO CSM AND SYNC COUNTDOWN
16 85 DELTA VS-BODY
502R DELTA VZ (NOM 5Ql)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTAVS-BODY
(123t26t27) BURN +Z
NULL DELTA VS
4-12
VERIFY AGS RESIDUALS 50OR 501R 502R DELTA VX _ DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
CDH
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
KEY V67E (RESET W MATRIX) F 06 99 +0200E +O0020E +00005E
PRO
507+0 Z-AXIS BORESIGHT
(VHF RANGING WITH CSM) VHF A XMTR - VOICERNG VHF B XMTR - OFF VHF B RCVR - ON TELEMETRY PCM - HI
(12331) KEY V37E33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 a TIG CDH (NOM 1242425) -120 amp00 10 (AGS 0 TIME)
(CONVERT TO MINUTES)
411+0 THRUST ALONG Z-BODY AXIS ENTER IF YOU DONT TARGET CSI
373R (NOM 26443 310R TIME TO CDH
4-13
423R DESIRED ALT RATE AT CDH
402R DELTA Hshy
450R DELTA VX
452R DELTA VZ
623+0 Z-AXIS PARALLEL TO CSM PLANE
IPRO F 16 45 MKS TFI -00001
-52 RESET ET
KEY V93E (REINIT W MATRIX WHEN MARKS =4)
KEY V32E (MARKS = 3)
F 06 75 DELTA HCDH DELTA TCDHTPI DELTA TTPI PRO
F 06 81 DELTA VCDH-LV CDH(N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
-47 KEY VSOE (OUT-OF-PLANE)
_ TIG CDH (NOM 124t24t25) -3000 TIME FROM CDH
F 06 16 l1 LOAD TIG PLANE CHANGE (NOM 123amp54-253 PRO
F 06 90 Y YDOT PSI N90 CSM
VYDOT PRO
-42 KEY V32E (MARKS=1O)
F 06 75 DELTA HCDH DELTA TCDIHTPI DELTA TTPITPI PRO
F 06 81 DELTA VCDH-LV
4-14
CDH (NS1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -OO1
KEY V34E (TERMINATE) F 37 B8
PLANE CHANGE
KEY 30E (EXTERNAL DELTA V)
TIG CDH (NOM 124124t25) -3000 TIME FROM CDH
F 06 33 LOAD TIG PLANE CHANGE (NOM 123154T25) PRO
F 06 81 DELTA VS-LV (NOM 00)
-36 COPY RDOT FOR 1ST CDH BU
KEY V90E (OUT-OF-PLANE)
F 06 16 1 1 LOAD TIG PLANE CHANGE (NOM 1231543251 PRO
F 06 90 Y YOOT PSI N90 CSM
YDOT
PRO
F 06 81 DELTA VS-LV(NOM 00)
COPY YDOT AND LOAD NEGATIVE IN R2 PRO
F 06 42 HA HP DELTA V PRO
F 16 45 MKS TFI MGA
PRO
F 37 BB
KEY 41E (RCS THRUSTING)
-30
4-15
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVRI
410+5 EXTERNAL DELTA V 450+0 451-YDOT 452+0 (LOAD CSM -YDOT)
407+0 ROTATE EXTERNAL DELTA V RF
16 95 DELTA VS-BODY
-3035 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATTVHOLD 407+1 FREEZE EXTERNAL DELTAV
F 16 85 DELTA VS-BODY -
NULL DELTA VIS
PRO F 37BB
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
507+0 Z-AXIS BORESIGHT
(12356) KEY 33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 TIG CDH (NOM 124t24t25) -120 OO ZOO (AGS 0 TIME)
(CONVERT TO MINUTES)
373R _ (NOM 2644) 310R TIME TO CDH
423R DESIRED ALT RATE AT CDH
(ADS OF MSFN) S-BAND - SLEW TOP = ACQUIRE HGA LOCK ON VOICE - BUVOICE -- VOICE VERIFY VOICE TLM BIOMED - LEFT (OR RIGHT)
402R DELTAH
4-16
F 16 45
-25
-23
F 06 75
F 06 81
F 16 45
-12
F 06 75
F 06 81
450R DELTA VX
452R DELTA VZ
PRO MKS TFI -00001
KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
COPY ROOT FOR 2ND CDH BU
KEY v32E (MARKS = 5)
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40DEG TO 1OODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + B PRESS IND PSIA
A QUANTITY IND _ PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING a TEMP MON SEL RCS QUAD 1 4 2 3 (120 - 190 DEG F)i
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
CDH(NB1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO MKS TFI -00001
PRO (FINAL COMP)
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
KEY V9OE (OUT-OF-PLANE)
-7
4-17
F 06 16 jj LOAD TIG CDH FROM DATA PAD (NOM 12424251 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT PRO
COPY YOOT FROM CSM AND LOAD NEGATIVE IN R2
CDH(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RDOT FOR 3RD CDH BU
COMPUTE CDH BU
TRANSMIT TGT DELTA VOS TO CSM AND SYNC COUNTDOWN
KEY V47E (INITIALIZE AGS F 06 16 GET OF AGS 0 TIME 120O00OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
KEY V83E F 16 54 R RDOT THETA
SET ORDEAL PRO
317R _ RANGE
440R RANGE RATE 400+3 AGS ALIGN 40OR (00000 COMPLETE)
277R THETA
-6
4-18
PRO F 3 BB
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY V06N86E F 06 86 DELTA VIS-LV
AGS(N86) CHART
DELTA VX(LVD
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
16 85 DELTA VS-BODY
50OR DELTA VX (NOM -0O3)
502R DELTA VZ (NOM 60)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD 407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS BODY
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS 5OOR 50IR 502R DELTA VX -DELTA VY DELTA VZ-
VERIFY PGNS RESIDUALS N85
DELTA VX(LM)
4-19
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
TPI
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO 507+0 Z-AXIS BORESIGHT
(12426) KEY 34E (TPI)
-36 RESET ET
F 06 37 - amp LOAD TIG TPI FROM DATA PAD (NOM 1250246) PRO
F 06 55 +00000 +02660E +13000 OMEGAT PRO
F 16 45 MARKS TFI -00001
-32 KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
-29 KEY V32E (MARKS = 3)
F 06 37 __ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
RESET ET
410+3 TPI SEARCH ROUTINE 307+04300 DELTA T TRANSFER
4-20
-26 310+02600 TFI TPI
303R THETA AT TPI
267R DELTA VTPI
371R DELTA VTPI + DELTA VTPF
KEY V32E (MARKS = 10)
F 06 37 _ _ _ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VIS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
TEMPIPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40ODEG TO IGODEG F A + B PRESS IND 181 +-3 PSIA
TEMPIPRESS MON SEL - HEL
A + B PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD I 4 2 3 (120 - 190 DEG F)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
RESET ET
-13 310+01300 TFI TPI
303R THETA AT TPI
-12 PRO (FINAL COMP) F 06 37 Z TIG TPIj__
4-21
TRANSMIT TIG OF TPI TO CSM-
PRO F 06 58 HP DELTA VTPI DELTA VTRF
PRO F 06 81 DELTA VS-LV
KEY V9OE (OUT-OF-PLANE)
F 06 16 1 LOAD TIG TPI FROM DATA PAD (NOM 12502461 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT
PRO F 06 81 DELTA VS-LV
COPY CSM YDOT AND LOAD NEGATIVE IN R2 N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 59 DELTA VS LOS
N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI MGA
RESET ET
PRO F 37 BB
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (12000t600)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE)
-10
-6
4-22
F 50 16 DOWNLINK COMPLETE PRO (UPDATE COMPLETE)
400+3 AGS ALIGN 400R (00000 COMPLETE)
-9 277R COPY TGT LOS ANGLE
310+00800
303R THETA AT TPI 410+4 DIRECT TRANSFER AT ET=-8 404+0 405+0 406+0 (MONITOR 470 471 4721
373R TIG TPI
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
KEY 41E (RCS THRUSTING) F 50 18 FOAl ANGLES (REQUEST MNVRI
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
-5 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUS
400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
COMPUTE TPI BU
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
4-23
1685 DELTA VS-BODY
50OR DELTA VX(NOM -115)
502R DELTA VZ(NOM 229)
-Z35 OSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS-BODY
(1250246) BURN +Z
VERIFY AGS RESIDUALS 500R 501R 502R DELTAVX DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
MCC1
KEY V76E (PGNS PULSE) PGNSMODECONT-AUTO
KEY V93E (BEFORE 1ST MARK REINITW MATRIX)
+2 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
4-24
(LOS OF MSFN) S-BAND - SLEW TO P = 90 Y = 0 S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
404+0 405+0 406+0
(MONITOR 470 471 4721
+9 277R COPY TGT LOS ANGLE
+12 PRO (COMPUTE MCC FOR TPI+15I F 06 81 DELTA VS-LV
PRO F 06 59 DELTA VS-LOS
PRO F 16 45 MKS TFI MGA
+13 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUOS
COMPUTE MCC1 BU
PRO F 37 BB
+14 KEY 41E (RCS THRUSTING) F 50 18 FOAL ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+1425 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+15 F 16 85 NULL DELTA VS
PRO F 37 BB
MCC2
KEY V76E (PGNS PULSE)
4-25
PGNS MODE CONT-AUTO
KEY V93E (BEFORE 1ST MARK REINIT W MATRIX)
+16 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
404+0 405+0 406+0 (MONITOR 470 471 47)shy
+24 277R COPY TGT LOS ANGLE
+27 PRO (COMPUTE MCC FORTPI+30) F 06 81 DELTA VS-LV
PRO F 06 59 DELIA VPS-LOS
PRO F 16 45 MKS TFI MGA
+28 277R COPY TGT LOS ANGLE
COPY R RDOT FROM TAPEMETER FOR BUS
COMPUTE MCC2 BU
F 37 BB PRO
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+2925 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+30 F 16 85 NULL DELTA VS
PRO F 37 BB
KEY OOE (P001
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
4-26
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT KEY V34E (TERMINATE)
KEY V37E47E (AVE G) F 16 83 DELTA VIS
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT VERIFY TAPE METER WITH DSKY
BRAKING GATE 30 FPS - 6000 FT 20 FPS - 3000 FT 10 FPS - 1500 FT 5 FPS - 600 FT
RENDEZVOUS
STATION KEEPING
5-1
50 ABORT PROCEDURE
This is a specific AGS nominal abort procedure due to a PGNS failure between insertion and station keeping
51
5-2
Nominal AGS Procedures
ASSUMPTIONS
AFTER INSERTION
I INSERTION COMPLETE (RFSIDUALS NULLED) g PGNS FAILURE BEFORE INSERTION 3 RAUAR NOT LOCKED ON
(UI CoNT-AGS ATlI[uUE MON-AGS(CDR) RATE ERR MON-CNPTR(LMP) ATTITUDE MON-AGS(LMP) SHFITRUN-+5 DEG X-POINTER-HI MULT RADAR IEST Sw-OFF LNb GMbL-OFF ENG ARM-OFF X-IRANSL-2 JETS DEAD BAND-MAX PGNS MODE CONT-OFF THROTJET-JET CB IMU OIR-ON HH MOVE-AUTO rRACK TTCATNANSL-ENABLE(CDR)
AL CPL-ON MODE SL-AGS RNGAL1 MON-RNbRNGRT RAIE ERR MON-RNDZ HDR(CDR) AVl CoNT(3)-PULSE AGS MODE CONT-AUTO ACA4JET-DISABLE(CDR) TTCATRANSL-DISABLE(LMP) ACA4JET-DISABLE(LMP)
bO7+U Z-AXIS BOPESIGHT 400+2 Z-AXIS STEERING PULSE TO NULL AGS ERRORS POINT Z-AXIS IN DIRECTION OF CSM MODE CONT-ATT HOLD ATT CONT(3)-MODE CONTROL O unnr - ZirF
5-3
SLEW PATE - LO
SLEW RR ANT TO OqON FUAI VERIFY MAX SIGNAL STRENGTH RH MOOE-AUTO TRACK NO TRACK LIGHT OFF -
ATT CONT(3h-PULSE
CHECK INSERTION VELOCITY WITH TAPEMETER COMPARE EAPEMETER WITH AGS STATE VECTOR DATA I
17R RANGE(NOM 2642)
440R RANGE RATE(NOM -425l)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
cSI
+3 417+1 (RADAR FILTER INITIALIZED) 41b+l (NO BOHESIGHT) b03-XXXXX RANGE RATE
+5 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGF
41b+1 CSI ROUTINE 373+o2065 CSi TIME 275+03028 TPI TIME 605+0077 COTANGENT OF LOS TO CSM 41b+1 (ONE-HALF OFBITAL-PERIOD) 411+0 HCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT
610R TIME TO CST
43 RESET ET
267R VELOCITY TO BE GAINED CSI
402R FLTA H
371R DFLTA V CDH
5-4
372R DFLTA T CSICDH
-42 415+1 (No BORESIGHT) bO6-xXXXX RANGE RATE
-40 415+1 (NO BORESIGHT)503-XXXXX RANGE RATE dORESIGHT ON CSM
415+1 316+XXXXX RANGE
-37 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE
-15 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE UORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-2 415+1 (No BOHESIGHT) bO3-XXXXX RANGF RATE
i1uR TIME TO CS
RESEF ET
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-30 COPY ROOT FOR 1ST CSI 81J
BORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-t7 415+1 (NO BORFSIGHT) 50-XXxXx RANGF RATE
267R VELOCITY TO HE GAINED CSI
402R LELTA H
371R OFLTA V COH
372R OELTA T CSICDH
-5 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 blb+XXXXX RANGE
-i2 415+1 (No BORESIGHT) 5n3-XXXXX RANGE RATE
415+1 (NO BORESIGHT)
5-5
503-XXXXX RANGF RATE
COPY Roor FOR 2NO CSI BU
bORESIGHT ON CSM 415+1 316+XXXXX RANGE
TEMPPRESS MON SEL - FUEL MAN
A AND 8 PRESS 181 +-3 PIG TEMPPRESS MON SEL - PRPLNT
A AND B TEMP IND 4ODEG 0 IOODEG F A AND B PRFSS IND 181 +-3 PSIA
tEMPPRESS MON SEL - HEL
A AND 8 PRESS IND PSIA
A QUANTITY IND- -- PERCENT RFMAINING
8 QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4p 2 3 (120 - 190 DFG F)
415+1 (NO BORESIGHT)-17 503-XXXXX RANGE RATE
-15 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
(LOS OF MSFN) S-BAND - SLEW 10 P = +90t Y U S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
-12 415+1 (No 8ORESIGHT)
503-XXXXX RANGE RATE
267R VFLOCITY TU BE GAINED CSI
402R OFLTA H
372R TIME CSICH
371R PREDICTED VEL 10 RE GAINED COH
263R OLT-OF-PLANE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATL
-10 COPY RANGE AND ROOT FOR 3RD CSI 8U
SORESIGH ON CSM 41b+1
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
=i1-
FIGURES
PAGE
Relative Motion Profile (2-1) 2-2
LUNAR ORBIT RENDEZVOUS ATTITUDE TIME HISTORY 2-3
Lift-off - CSI (2-2) 2-3
CDH-TPF (2-3) 2-4
LIST OF ACRONYMS AND ABBREVIATIONS ACQ ADJ AGS AOH AOS AOT APS ATT BU CALIB CB CDH CDR CM CMC CMD CMP COAS CSI CSM CT DAP DH DOI DPS DSKY DV DWN EMS ET FDAI FPS FWD GDC GET GETI GMBL GND HA HGA HOR HORIZ HP IMU INS IT LGC LM
Acquisition Adjust Abort Guidance System Apollo Operations Handbook Acquisition of Signal Alignment Optical Telescope Ascent Propulsion System Attitude Backup Calibration Circuit Breaker Constant Delta Height Commander Command Module Command Module Computer Command Module Commanders Position Command Module Pilot Crew Optical Alignment Sight Concentric Sequence Initiation Command and Service Module Cease Tracking Digital Autopilot Delta Height Descent Orbit Insertion Descent Propulsion System Display and KeyboardDelta Velocity Down Entry Monitor System Event Timer Flight Director Attitude Indicator Feet Per Second Forward Gyro Display Coupler Ground Elapsed Time Ground Elapsed Time of Ignition Gimbal Ground (Mission Control) Apogee Altitude High-Gain Antenna Horizon Horizontal Perigee Altitude Inertial Measurement Unit Insertion Initiate Tracking LM Guidance Computer Lunar Module
LV
-1v-
LMP LOI LOS
MNVR MCC MCCl MCC2 MCC-H MGA MSFN NAV ORDEAL PAD PB PC PDI PGNS PHS PIPA PLM PRO PROG PROP R RCS RDOT REFSMMAT RHC RR SHFT SC SEP SM SXT SYNC TFI THC THETA TIGN TLM TPF TPI TRUN TTCA VG VHF (XXXX) (XXXXX XX)
Lunar Module Pilot Lunar Orbit Injection Line Of Sight Launch Vehicle Maneuver Midcourse Correction First Midcourse Correction Second Midcourse Correction Mission Control Center - Houston Middle Gimbal Angle Manned Space Flight Network Navigation Orbital Rate Drive Earth and Lunar Data Voiced to Crew From Ground Pushbutton Plane Change Powered Descent Initiation Primary Guidance Navigation and Control System Phasing Pulse Integrating Pendulous Accelerometers LM Pitch Angle Proceed Program Propellant Range Reaction Control System Range Rate Reference Stable Member Matrix Rotation Hand Controller Rendezvous Radar Shaft Spacecraft Separation Service Module Sextant Synchronize Time From Ignition Translation Hand Controller Angle Between SC +X Axis and Local Horizontal Time of Ignition Telemetry Terminal Phase Finalization Terminal Phase Initiation Trunnion Translation Thrust Control Assembly Velocity to be Gained Very High Frequency Indicates GET From Liftoff in HoursMinutes Indicates GET From Liftoff in HoursMinutesSeconds
(XXXXXXXXXXXX) (OrdealInertial) Angles (Roll Pitch Yaw) (XXXXXX) Local Vertical DVs
Tracking Stations
ANG BDA CRO CYI GYM HSK HTV MAD MER MIL RED TEX VAN
-v-
Antigua Near Space Support Station Bermuda Near Space Support Station Carnarvon Near Space Support Station Canary Near Space Support Station Guaymas Near Space Support Station Honeysuckle Deep Space Support Station Huntsville Near Space Support Station Madrid Deep Space Support Station Mercury Near Space Support Ship MILA Near Space Support Station Redstone Near Space Support Ship Corpus Christi Near Space Support Station Vanguard Near Space Support Ship
10 PURPOSE
This document contains the primary procedures for the LM-5 active rendezvous with CSM-107 spacecraft in accordance with Detailed Test Objective Section 40 defined in Reference 71
The purpose of the LM Rendezvous Procedures document is to provide a single source of procedures information for use in flight planning in crew training and in preparing onboard data
This is a control document subject to review by all elements of the Apollo Program and to approval by the Procedures Conshyfiguration Control Board Comments should be directed to Mr Stephen P Grega Flight Procedures Branch Flight Crew Support Division Extension 5348
Beyond G mission planning no additional techniques and trajectory information specific to Mission H have been made available as of this date Therefore since Missions G and H are expected to be similar in the area of rendezvous guidance and navigation procedures the G mission final LM Rendezvous Procedures Document will serve -as an H mission preliminary LM Rendezvous and Procedures Document After reviewal by all elements of the Apollo Program and approval by the Procedures Configuration Control Board this document will then evolve into the control document for the Mission H crew procedures
2-1
20 INTRODUCTION
The LM-5CSM-l07 lunar orbit rendezvous exercise will beginduring the twenty-fourth CSM revolution with insertion at 122 35255 and end at approximately 1260000 with post rendezvous station keeping The LM procedures during this period are divided into segments of major activities which are discussed in detail in Section 30
A nominal LM-5CSM-107 mission profile is contained in Figshyure (2-1) This figure shows the locations in time and local horizontal position of the most significant nominal mission events Trajectory data used to generate the mission profile and timeline for procedures development was obtained from Reference 72 The rendezvous navigation update schedule assumed in the procedures is defined in Reference 73
A history of the LM body attitudes during the rendezvous accompanies the major events discussion and is also presented in Figures (2-2) and (2-3) Each figure illustrates the bodyattitudes with respect to the moon sun and earth and indicates FDAI roll pitch and yaw gimbal angles and the ordeal pitch angle for significant events during each lunar orbit
0RBI TR EL
TRAILINGDISPLACEMENT(N MI) 0 0 W60 20240 BE
33I I ] I I I
32 ltrMCCE 1125+-3 C CH (124t24) PLAN CHANGE023 TM)2
R~TC(222
40 1146235 A N MNTTIMETKS FROMISEDRT(GA122plusmn252
-- DAYLIGHT B shy
_ _ _ _ _ _ __E_ _ -- 7 LUNAR IARFAGELM MAJOR EVENTS
122+35 INSERTION 17 124+H7 AGE UPDATE AND ALIGN (R47) 2 122+40 IMU REFSMMAT ALIGN (P52) 1 124+24 CDH THRUSTING (P41) TRAILINGDISPLACEMETIN RI)
3 122+54 AGS UPDATE AND ALIGN (R471 19 124+26 TPI TARGETING IP34 amp AGS) 5 II 20 25 30 4 122+55 CSI TARGETING IP32 amp AGSI 20 124+26-124+51 RR NAVIGATION (P20 18 MARKS) - I I
5 122+54-123+14 RR NAVIGATION (P20 18 MARKS) 21 124+53 AGS UPDATE AND ALIGN (R47)I
6 123+18 COMPUTE CSI BACKUP 22 125+00 COMPUTE TPI BACKUP
7 123+19 AGS UPDATE AND ALIGN (R471 23 125+03 TPI THRUSTING (P411 c
8 123+26 CSI THRUSTING (P411 24 125+05 MCC1 TARGETING IP35) N - M ((25+232
9 123+30 SET W MATRIX 1200025) 25 125+05-125+16 RR NAVIGATION IP20 9 MARKS) 5
2 r INSERT A 10 123+31 CDH TARGETING IP33 amp AGS 26 125+16 COMPUTE MCCI THRUSTING IP41) 5 31 PHAE
11 123+31-123+46 RR NAVIGATION 1P20 14 MARKS) 27 125+18 MCC I THRUSTING (P41)
12 123+47 EXT AV FOR PLANE CHANGE (P20) 28 125+20 MCC2 TARGETING (P351 13 123+54 RCS PLANE CHANGE THRUSTING (P411 29 125+20-125+31 RR NAVIGATION (P20 9 MARKS) 14 123+56 CDH TARGETING (P33 amp AGS) 30 125+31 COMPUTE MCC 2 BACKUP Ideg
15 123+56-124+12 RR NAVIGATION (P20 13 MARKS) 31 125+33 MCC2 THRUSTING [P41)
16 124+15 COMPUTE CDH BACKUP 32 125+48 BRAKING (P47) 27 26TP25+03
33 126+00 STATION KEEPING LT
24
FIGURE 2-1 G MISSION RENDEZVOUS
(CSM-CENTERED RELATIVE MOTION) FOLDOUT FRAME
l D T R2A-e2 TALPFO EDUR ES EPREPAREDBY STEPHENP GRED501I DOUT FRAMW ORBI R B C 0
MISSION G LUNAR ORBIT RENDEZVOUS ATTITUDE TIME HISTORY
OFOR THE LM P33
P20 123+31) (021880)
LMI CSI NrxNMARKS i (123+26+27)
FINAL -
COMP(I123+1l6)
P32 LANDING SITEj P20 30ES (122+50) CSM AT (04650) PRIME MERIDIAN LIFT-OFF
P52 (122+28+11) (122+40)DIRECTION OF (03640)ORBITAL MOTION IS
CLOCKWISE
(18012150)I NERTIAL YAWKLINERTIAL PITCH
ORDEAL PITCH EARTHINERTIAL ROLL
FIGURE 2-2
MISSION G LUNAR ORBIT RENDEZVOUS ATTITUDE TIME HISTORY
FOR THE LM
LM TPF (126+00+00) (01302920)
LM LMC2PLANE CHANGELMPI+30) (123+54+25)
(TPI+30) (0560)(0782400) 7 SUN
P20
(TPI+15) P3
P33(0532480) COMP
---- _ (124+12--- ---
LM TPI (125+02+46) L D (026 627650) (124+24+25)
(0980)
FINAL
DIRECTION OF COMP ORBITAL MOTION IS (124+50)
CLOCKWISE
(18012150)
LL INERTIAL YAW NERTIAL PITCH
ORDEAL PITCH EARTH INERTIAL ROLL
FIGURE 2-3
3-1
30 DISCUSSION OF MAJOR EVENTS
31 Concentric Sequence Initiation
Immediately following Insertion the LM navigated vector will be downlinked to Mission Control Center-Houston this state vector is then uplinked to the CSM The LM commander will perform a Proqram 52 fine alignment to REFSMMAT at approxishymately 12240
The digital autopilot is configured to wide deadband Program P20 is called and an automatic pitch maneuver is initiated to the preferred track attitude At 122 55 CSI targeting parameters are loaded in the PGNS and AGS A period of rendezvous radar marking will then take place from 122-57 to 12315 Upon completion of tracking the LM will obtain an out-of-plane velocity from the CSM to be vectored with the in-plane component of the CSI delta V The CSMs estishymate of out-of-plane velocity is alleged to be better than the LMs estimate (Reference 74)
At approximately 123 20 the LM will voice its CSI solution to the CSM the AGS is updated aligned and targeted in external delta-V with the CDH solution to be excuted Program P41 will then be called and the automatic pitch maneuver bypassed since the burn isto be executed with Z-Axis thrusting The CSI burn occurs nominally at 123 26 27 After verification of the LM CSI burn the CSM will incorporate the LM burn parameters in its CMC LM state vector
32 Constant Delta Height and Plane Change
At 12330 approximately three minutes after the LM CSI burn the W matrix will be set to (200025) and the LM targeting paramters are loaded in both the PGNS and AGS for the CDH maneuver Out-of-plane velocity will then be computed and voiced to the LM from the CSM Program P30 is loaded with the targeting parameters for the LM Plane Change maneuver which will be accomplished in Program P41 30 minutes prior to the CDH maneuver Following the burn the target delta V parameters are voice to the CSM and incorporated into the CMC LM state vector At 12356 the CDH targeting parameters are loaded in both the PGNS and AGS for 1242425 A CDH chart solution is calculated 7 minutes prior to TIG The AGS is updated aligned and targeted in external delta V with the CDH solution to be executed The RCS Thrust Program P41 is called at 12418 and the burn attitude is bypassed since the LM executes CDH by thrusting out individual components of delta V while maintaining radar lock-on
3-2
3 3 Terminal Phase Initiation
Radar tracking is initiated after the CDH maneuver and updating of the LGC continued At 12426 approximately two minutes after the LM CDH burn targeting parameters are loaded in both the PGNS and AGS for the TPI maneuver which will be targeted for a node at intercept Backup measurements are made at the appropriate times The AGS is updated aligned and targeted in external delta V with the TPI solution to be executed The RCS Thrust Program P41 is called at 12456 and the burn attitude is bypassed since the LM is burning along the plus Z-axis with the thrust direction established with the COAS
3 4 Midcourse Corrections
Immediately after TPI the Midcourse Prethrust Program P35 will be called and radar tracking reinitiated Backup measshyurements are made and midcourse corrections chart solutions obtained The MCCl burn will nominally be performed at TPI plus 15 minutes (1251746) If MCCI is to be excuted Program P41 will be called and the burn attitude maneuver is bypassed since the plus Z-axis will remain boresighted at the CSM until docking
Following MCCI Program P35 will be called and targeted for MCC2 at TPI plus 30 minutes (1253246) and executed identishycally to MCCI
3 5 Braking
In preparation for braking the DAP is configured in narrow deadband Program P20 is terminated at 18000 feet but the radar is kept in auto track to provide radar range and range rate displayed on the tapemeter Average G is called by Program P47 prior to braking and attitude hold is selected The braking schedule is followed as contained in Section 4
4-1
40 NOMINAL MISSION PROCEDURES
The procedures included in this section do not specify which crewmember Commander or LM Pilot performs each task These need not be specified since the following basic rules define which crewmember performs each task
41 Commander Tasks
1 All attitude changes whether manual or automatic will be accomplished by the CDR
2 The operation of the DSKY during thrust programs (P40 P41 P42 P47) will be done by the CDR Actual manipulation of the TTCA need not be always done by the CDR but in most cases will be
3 Operation of the rendezvous and landing radar will be done by the CDR
4 The CDR will operate all other systems accessible to only his crew station
42 LM Pilot Tasks
1 AGS operation 2 DSKY operation will be done by the LMP except when keyboard
entries affect the control of spacecraft attitude or thrustshying
3 Backup data logging and chart calculations 4 All logging of maneuver solutions and systems performance 5 The LMP will operate all other systems accessible to only
his crew station
These general rules are guidelines only and may be deviated from by the LM crew if they develop more efficient Task assignments
43 ABBREVIATIONS
The abbreviations used herein are consistant with those in the AOH However in order to condense and simplify the procedures so that they are representative of onboard data a number of addshyitional shorthand conventions have been used To allow the unshyfamiliar reader to understand the procedures contained in this section the following explanations are included
1 AGS - A single asterisk is employed to denote those procedures involving operations to be performed on the DEDA The three number group following an asterisk specifies DEDA address An Rfollowing the address group indicates the address is to be read out A five digit group behind the Rindicates a nominal or expected display If the three number address group is followed by a plus or minus sign a data load is indicated When a single digit follows the plus addition of four zeros behind this digit is assumed Once used these conventions are easily handled and save considerable space
4-2
2 PGNS - The verb-noun addresses in the PGNS are indicated to the left of the procedures column An F is used to indicate a flashing display or absence of an F a static display To the right of the verb-noun on the same line are the contents of the three data registers If numeric quantities appear the DSKY should be correspondingly made to agree by executing a V21 V22 or V23 and performing a data load The procedure of blanking and loading registers is not included since it is repeated often and is highly familiar to the crews
EXAMPLE F 06 33 125-02 46 TIG OF TPI
Expanded this means Load flashing verb 06 noun 33 with the quantity 125 hours 2 minutes and 46 seconds the time of ignition of the RCS engine TPI maneuver Procedurally this is done by keying verb 25 enter loading +000125 in register 1 +00002 in register 2 and +04600 in register 3
If numberic quantities do not follow the verb-noun it is indicated that a computed or information quantity is being displayed via the DSKY If nominal values are listed for possible comparison they appear in parentheses
EXAMPLE- F 06 42 HA HP V
Expanded this means Flashing verb 06 noun 42 has computed height of apogee in register 1 height of perigee in regshyister 2 and velocity to be gained in register 3
3 TIME - The numbers in the left hand column preceded by a plus or minus indicate event timer time referenced to an event Minus indicates event timer counting down to a future event Periodically this same column contains the nominal mission ground elapsed times in parentheses Asterisks following the event time indicate a time critical event which should be accomplished to the nearest second
4-3
4 4 Nominal PGNS Procedures
ASSUMPTIONS
AFTER INSERTION
1 INSERTION COMPLETE (RESIOUALS NULLED) VERIFY V82E (ORBIT) 3 RNDZ RDR LOCKED ON IN MODE II 4 LGC AT FLASHING VERB 37 5 PROPER INITIAL W MATRIX LOADED IN LGC
GUID CONT-PGNS ATTITUDE MON-PGNS(CDR) RATE ERR MON-CMPTR(LMP) ATTITUDE MON-AGS(LMP) SHFTTRUN-+5 DEG X-POINTER-HI MULT RADAR TEST SW-OFF ENG ARM-OFF X-TRANSL-2JETS DEAD BAND-MIN PGNS MODE CONT-AUTO THROTJET-JET CBPGNS IMU OPR-CLOSE RR MODE-LGC TTCATRANSL-ENABLE(COR)
BAL CPL-ON MODE SEL-AGS
RNGALT MON-RNGRNGRT RATE ERR MON-RNDZ RORICOR) ATT CONT-PULSE(3)
AGS MODE CONT-ATT HOLD ACA4JET-DISABLE(CDRJ TTCATRANSL-DISABLE(LMP)
ACA4JET-DISABLE(LMPI
KEY ODE (PO0)
(DOWNLINK LM STATE VECTOR)
KEY V63E (RR SELF TEST)
4-4
F 04 12 00004 00001 PRO
F 16 72 TRUN SHFT PRO
F 16 78 R ROOT VERIFY TAPE METER WITH DSKY
+2 VERIFY INSERTION VELOCITY WITH RNDZ ROR WHERE RANGE = 2642 NM RANGE RATE = -4251 FPS
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
KEY V34E (TERMINATE) KEY V48E (LOAD DAP)
F 01 46 11002 PRO
F 06 47 LMWT CMWT PRO
KEY V56E (KILL AUTO TRACK ENABLE)
+3 KEY V41N72E (COARSE ALIGN RR) F 21 73 +000OOTRUN -077OOSHFT F 04 12 00006 00002 (CONTINUOUS DESIGNATE)
PRO 41 (COARSE ALIGN VERB)
KEY VI6N72E 16 72 MONITOR TRUNSHFT ANGLES
CB PGNS RNDZ RDR-OPEN CB AC BUS A RNDZ RDR-OPEN KEY V44E (TERMINATE RR DESIGNATE)
KEY V83E F 16 54 R ROOT THETA
SET ORDEAL PRO
CS HEATER AOT-CLOSE
CB AOT LAMP-CLOSE
+5 KEY V37E52E (IMU REALIGN)
4-5
410+1 CSI ROUTINE 373+02065 CS TIME 275+03028 TPI TIME
605400777 COTANGENT OF LOS TO-CSM 416+1 (ONE-HALF bRBITAL PERIOD) 411+0 RCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT 310R TIME TO CS
267R VELOCITY TO BE GAINED CSI
402R DELTA H
371R DELTA V CDH
372R _ DELTA T CSICDH
F 04 06 00001 00003 -(REFSMMAT) PRO -
F 50 25 00015 SELECT 1ST STAR ENTR
F 01 70 O02DE LOAD 1ST STAR PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FOAl ANGLES (AUTO MNVRI)
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVR)
F 01 71 002DE
KEY V76E PGNS MODE CONT-ATT HOLD
PRO +10 F 54 71 MARK 1ST STAR
PRO F 01 70 O02DE LOAD 2ND STAR
PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FDA ANGLES -(AUTO MNVRV
F 50 18 FDAI ANGLES (REQUEST PNVRt ENTR (BYPASS MNVR
F 01 71 002DE PGNS MODE CONT-ATT HOLD PRO
-35
4-6
+14 F 54 71 MARK 2ND STAR PRO
F 06 05 STAR ANGLE DIFFERENCE PRO
F 06 93 GYRO TORQUE ANGLES PRO
F 50 25 00014
PRO (CHECK ALIGNMENT IF TIME WILL PERMIT)
F 50 25 00015 SELECT 3RD STAR ENTR
F 01 70 OO2DE LOAD 3RD STAR PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FDAI ANGLES (AUTO MNVR)
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVR)
VERIFY ALIGNMENT VIA AOT
KEY V34E (TERMINATE) F 37 BB
V48E (LOAD DAP) F 01 46 11012
PRO F 06 47 LMWT CMWT
+17 PRO
CB AOT LAMP-OPEN
RESET ET (310R)
(12253) CB AC BUS A RNDZ RDR-CLOSE (WAIT 30 SEC) CB PGNS RNDZ RDR-CLOSE
RR MODE-LGC KEY V37E20E (ACQUIRE RADAR)
PGNS MODE CONT-AUTO F 50 18 FDA ANGLES (REQUEST MNVRJ
PRO (AUTO MNVR) 06 18 FDAI ANGLES (AUTO MNVR)
AGS MODE CONT-AUTO RATEERR MON-CMPTR (LMP)
F 50 18 FDAI ANGLES (REQUEST MNVR)
4-7
ENTR (BYPASS MNVR) NO TRK LT-OFF
F 50 72 RR TRUNSHFT VERIFY RR LOCK ON PRO
DSKY BLANKS
KEY V93E (BEFORE 1ST MARK REINIT W MATRIXI KEY V80E (UPDATE LM SV)
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (i20OOZOO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
400+3 AGS ALIGNshy400R (00000 COMPLETE) 507+0 Z-AXIS BORESIGHT 400+2 ACQUISITION STEERING
CS
(122amp55) KEY V37E32E (CSI)
F 06 11 1 S LOAD TIG CSI FROM DATA PAD (NOM 123S26- 271 PRO
F 06 55 +O000IN +02660E +13000 OMEGAT (CDH 180 DEG AFTER CSI PRO
F 06 37 LOAD TIG TPI FROM DATA PAD (NOM 1251021761 PRO
F 16 45 MKS TFI -00001
-30 COPY RDOT FOR 1ST CSI BU
31OR TIME TO CSI
267R VELOCITY TO BE GAINED CSI
402R DELTA H
371R DELTA V CDH
-22
4-8
372R _ DELTA T CSICDH
KEY V32E (MARKS=5
F 06 75 DELTA H DELTA T CSICDH DELTA T CDHTPI PRO
F 06 81 DELTA VOS-LV (CS) (NOM 501 DELTA VX)
CSI(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (CDH)
(NOM 60 DELTA VX) CDH(82)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
KEY V32E (MARKS=1C)
F 06 75 DELTA H DELTA TCSICDH DELTA TCDHTPI PRD
F 06 81 DELTA VS-LV (CSI) CSI(N811
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 82 DELTA VIS-LV(CDH)
CDH(82)
DELTA VX(LVI
DELTA VY(LV)
DELTA VZ(LV)
-12
4-9
-20 COPY RDOT FOR 2ND CSI BU
F 16 45
F 06 75
F 06 81
F 06 16
F 06 90
PRO MKS TFI -00001
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS NON SEL - PRPLNT A + B TEMP IND 40DEG TO lOODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + 8 PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4v 2 3 (120 - 190 DEG F
(LOS OF MSFN ) S-BAND - SLEW TO P = +90 Y a 0 S-BAND - FWD (OR AFT) S-BAND - DN VOICE BU BIOMED OFF
PRO (FINAL COMP)
267R - VELOCITY TO BE GAINED CSI
402R DELTA H
372R TIME CSICDHL
371R PREDICTED VEL TO BE GAINED CDH
263R OUT-OF-PLANE
DELTA H DELTA TCSICDH DELTA TCDHTPI PRO DELTA VS-LV (CSI)
KEY V9OE (OUT-OF-PLANED
0 LOAD TIG CSI FROM DATA PAD (NOM 12302627) PRO Y YDOT PSI
N90 CSM
YDOT
PRO
-7
4-10
F 06 81 DELTA VS-LV(CSI)
COPY YDOT FROM CSM AND LOAD NEGATIVE IN R2 CSIIN81I
DELTA VX(LV)
DELTA VYILV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (COH)
CDH(82)
DELTA VX(LV)
- DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RANGE AND RDOT FOR 3RD CS BU
COMPUTE CSI BU
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (i2000OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
(TRANSMIT CSI DATA TO CSMI VHF A XMTR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF TELEMETY PCM - LO
KEY VB3E F 16 54 R ROOT THETA
SET ORDEAL PRO
317R RANGE
440R RANGE RATE
4-11
400+3 AGS ALIGN t40OR (00000 COMPLETE)
277R THETA
PRO F 37 BB
-6 KEY 41E (RCS THRUSTING) F 50 18 FDAI-ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTAV 400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTAV 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA RF
TRANSMIT TGT DELTA VS TO CSM AND SYNC COUNTDOWN
16 85 DELTA VS-BODY
502R DELTA VZ (NOM 5Ql)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTAVS-BODY
(123t26t27) BURN +Z
NULL DELTA VS
4-12
VERIFY AGS RESIDUALS 50OR 501R 502R DELTA VX _ DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
CDH
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
KEY V67E (RESET W MATRIX) F 06 99 +0200E +O0020E +00005E
PRO
507+0 Z-AXIS BORESIGHT
(VHF RANGING WITH CSM) VHF A XMTR - VOICERNG VHF B XMTR - OFF VHF B RCVR - ON TELEMETRY PCM - HI
(12331) KEY V37E33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 a TIG CDH (NOM 1242425) -120 amp00 10 (AGS 0 TIME)
(CONVERT TO MINUTES)
411+0 THRUST ALONG Z-BODY AXIS ENTER IF YOU DONT TARGET CSI
373R (NOM 26443 310R TIME TO CDH
4-13
423R DESIRED ALT RATE AT CDH
402R DELTA Hshy
450R DELTA VX
452R DELTA VZ
623+0 Z-AXIS PARALLEL TO CSM PLANE
IPRO F 16 45 MKS TFI -00001
-52 RESET ET
KEY V93E (REINIT W MATRIX WHEN MARKS =4)
KEY V32E (MARKS = 3)
F 06 75 DELTA HCDH DELTA TCDHTPI DELTA TTPI PRO
F 06 81 DELTA VCDH-LV CDH(N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
-47 KEY VSOE (OUT-OF-PLANE)
_ TIG CDH (NOM 124t24t25) -3000 TIME FROM CDH
F 06 16 l1 LOAD TIG PLANE CHANGE (NOM 123amp54-253 PRO
F 06 90 Y YDOT PSI N90 CSM
VYDOT PRO
-42 KEY V32E (MARKS=1O)
F 06 75 DELTA HCDH DELTA TCDIHTPI DELTA TTPITPI PRO
F 06 81 DELTA VCDH-LV
4-14
CDH (NS1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -OO1
KEY V34E (TERMINATE) F 37 B8
PLANE CHANGE
KEY 30E (EXTERNAL DELTA V)
TIG CDH (NOM 124124t25) -3000 TIME FROM CDH
F 06 33 LOAD TIG PLANE CHANGE (NOM 123154T25) PRO
F 06 81 DELTA VS-LV (NOM 00)
-36 COPY RDOT FOR 1ST CDH BU
KEY V90E (OUT-OF-PLANE)
F 06 16 1 1 LOAD TIG PLANE CHANGE (NOM 1231543251 PRO
F 06 90 Y YOOT PSI N90 CSM
YDOT
PRO
F 06 81 DELTA VS-LV(NOM 00)
COPY YDOT AND LOAD NEGATIVE IN R2 PRO
F 06 42 HA HP DELTA V PRO
F 16 45 MKS TFI MGA
PRO
F 37 BB
KEY 41E (RCS THRUSTING)
-30
4-15
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVRI
410+5 EXTERNAL DELTA V 450+0 451-YDOT 452+0 (LOAD CSM -YDOT)
407+0 ROTATE EXTERNAL DELTA V RF
16 95 DELTA VS-BODY
-3035 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATTVHOLD 407+1 FREEZE EXTERNAL DELTAV
F 16 85 DELTA VS-BODY -
NULL DELTA VIS
PRO F 37BB
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
507+0 Z-AXIS BORESIGHT
(12356) KEY 33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 TIG CDH (NOM 124t24t25) -120 OO ZOO (AGS 0 TIME)
(CONVERT TO MINUTES)
373R _ (NOM 2644) 310R TIME TO CDH
423R DESIRED ALT RATE AT CDH
(ADS OF MSFN) S-BAND - SLEW TOP = ACQUIRE HGA LOCK ON VOICE - BUVOICE -- VOICE VERIFY VOICE TLM BIOMED - LEFT (OR RIGHT)
402R DELTAH
4-16
F 16 45
-25
-23
F 06 75
F 06 81
F 16 45
-12
F 06 75
F 06 81
450R DELTA VX
452R DELTA VZ
PRO MKS TFI -00001
KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
COPY ROOT FOR 2ND CDH BU
KEY v32E (MARKS = 5)
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40DEG TO 1OODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + B PRESS IND PSIA
A QUANTITY IND _ PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING a TEMP MON SEL RCS QUAD 1 4 2 3 (120 - 190 DEG F)i
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
CDH(NB1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO MKS TFI -00001
PRO (FINAL COMP)
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
KEY V9OE (OUT-OF-PLANE)
-7
4-17
F 06 16 jj LOAD TIG CDH FROM DATA PAD (NOM 12424251 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT PRO
COPY YOOT FROM CSM AND LOAD NEGATIVE IN R2
CDH(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RDOT FOR 3RD CDH BU
COMPUTE CDH BU
TRANSMIT TGT DELTA VOS TO CSM AND SYNC COUNTDOWN
KEY V47E (INITIALIZE AGS F 06 16 GET OF AGS 0 TIME 120O00OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
KEY V83E F 16 54 R RDOT THETA
SET ORDEAL PRO
317R _ RANGE
440R RANGE RATE 400+3 AGS ALIGN 40OR (00000 COMPLETE)
277R THETA
-6
4-18
PRO F 3 BB
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY V06N86E F 06 86 DELTA VIS-LV
AGS(N86) CHART
DELTA VX(LVD
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
16 85 DELTA VS-BODY
50OR DELTA VX (NOM -0O3)
502R DELTA VZ (NOM 60)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD 407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS BODY
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS 5OOR 50IR 502R DELTA VX -DELTA VY DELTA VZ-
VERIFY PGNS RESIDUALS N85
DELTA VX(LM)
4-19
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
TPI
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO 507+0 Z-AXIS BORESIGHT
(12426) KEY 34E (TPI)
-36 RESET ET
F 06 37 - amp LOAD TIG TPI FROM DATA PAD (NOM 1250246) PRO
F 06 55 +00000 +02660E +13000 OMEGAT PRO
F 16 45 MARKS TFI -00001
-32 KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
-29 KEY V32E (MARKS = 3)
F 06 37 __ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
RESET ET
410+3 TPI SEARCH ROUTINE 307+04300 DELTA T TRANSFER
4-20
-26 310+02600 TFI TPI
303R THETA AT TPI
267R DELTA VTPI
371R DELTA VTPI + DELTA VTPF
KEY V32E (MARKS = 10)
F 06 37 _ _ _ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VIS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
TEMPIPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40ODEG TO IGODEG F A + B PRESS IND 181 +-3 PSIA
TEMPIPRESS MON SEL - HEL
A + B PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD I 4 2 3 (120 - 190 DEG F)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
RESET ET
-13 310+01300 TFI TPI
303R THETA AT TPI
-12 PRO (FINAL COMP) F 06 37 Z TIG TPIj__
4-21
TRANSMIT TIG OF TPI TO CSM-
PRO F 06 58 HP DELTA VTPI DELTA VTRF
PRO F 06 81 DELTA VS-LV
KEY V9OE (OUT-OF-PLANE)
F 06 16 1 LOAD TIG TPI FROM DATA PAD (NOM 12502461 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT
PRO F 06 81 DELTA VS-LV
COPY CSM YDOT AND LOAD NEGATIVE IN R2 N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 59 DELTA VS LOS
N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI MGA
RESET ET
PRO F 37 BB
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (12000t600)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE)
-10
-6
4-22
F 50 16 DOWNLINK COMPLETE PRO (UPDATE COMPLETE)
400+3 AGS ALIGN 400R (00000 COMPLETE)
-9 277R COPY TGT LOS ANGLE
310+00800
303R THETA AT TPI 410+4 DIRECT TRANSFER AT ET=-8 404+0 405+0 406+0 (MONITOR 470 471 4721
373R TIG TPI
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
KEY 41E (RCS THRUSTING) F 50 18 FOAl ANGLES (REQUEST MNVRI
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
-5 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUS
400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
COMPUTE TPI BU
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
4-23
1685 DELTA VS-BODY
50OR DELTA VX(NOM -115)
502R DELTA VZ(NOM 229)
-Z35 OSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS-BODY
(1250246) BURN +Z
VERIFY AGS RESIDUALS 500R 501R 502R DELTAVX DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
MCC1
KEY V76E (PGNS PULSE) PGNSMODECONT-AUTO
KEY V93E (BEFORE 1ST MARK REINITW MATRIX)
+2 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
4-24
(LOS OF MSFN) S-BAND - SLEW TO P = 90 Y = 0 S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
404+0 405+0 406+0
(MONITOR 470 471 4721
+9 277R COPY TGT LOS ANGLE
+12 PRO (COMPUTE MCC FOR TPI+15I F 06 81 DELTA VS-LV
PRO F 06 59 DELTA VS-LOS
PRO F 16 45 MKS TFI MGA
+13 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUOS
COMPUTE MCC1 BU
PRO F 37 BB
+14 KEY 41E (RCS THRUSTING) F 50 18 FOAL ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+1425 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+15 F 16 85 NULL DELTA VS
PRO F 37 BB
MCC2
KEY V76E (PGNS PULSE)
4-25
PGNS MODE CONT-AUTO
KEY V93E (BEFORE 1ST MARK REINIT W MATRIX)
+16 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
404+0 405+0 406+0 (MONITOR 470 471 47)shy
+24 277R COPY TGT LOS ANGLE
+27 PRO (COMPUTE MCC FORTPI+30) F 06 81 DELTA VS-LV
PRO F 06 59 DELIA VPS-LOS
PRO F 16 45 MKS TFI MGA
+28 277R COPY TGT LOS ANGLE
COPY R RDOT FROM TAPEMETER FOR BUS
COMPUTE MCC2 BU
F 37 BB PRO
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+2925 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+30 F 16 85 NULL DELTA VS
PRO F 37 BB
KEY OOE (P001
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
4-26
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT KEY V34E (TERMINATE)
KEY V37E47E (AVE G) F 16 83 DELTA VIS
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT VERIFY TAPE METER WITH DSKY
BRAKING GATE 30 FPS - 6000 FT 20 FPS - 3000 FT 10 FPS - 1500 FT 5 FPS - 600 FT
RENDEZVOUS
STATION KEEPING
5-1
50 ABORT PROCEDURE
This is a specific AGS nominal abort procedure due to a PGNS failure between insertion and station keeping
51
5-2
Nominal AGS Procedures
ASSUMPTIONS
AFTER INSERTION
I INSERTION COMPLETE (RFSIDUALS NULLED) g PGNS FAILURE BEFORE INSERTION 3 RAUAR NOT LOCKED ON
(UI CoNT-AGS ATlI[uUE MON-AGS(CDR) RATE ERR MON-CNPTR(LMP) ATTITUDE MON-AGS(LMP) SHFITRUN-+5 DEG X-POINTER-HI MULT RADAR IEST Sw-OFF LNb GMbL-OFF ENG ARM-OFF X-IRANSL-2 JETS DEAD BAND-MAX PGNS MODE CONT-OFF THROTJET-JET CB IMU OIR-ON HH MOVE-AUTO rRACK TTCATNANSL-ENABLE(CDR)
AL CPL-ON MODE SL-AGS RNGAL1 MON-RNbRNGRT RAIE ERR MON-RNDZ HDR(CDR) AVl CoNT(3)-PULSE AGS MODE CONT-AUTO ACA4JET-DISABLE(CDR) TTCATRANSL-DISABLE(LMP) ACA4JET-DISABLE(LMP)
bO7+U Z-AXIS BOPESIGHT 400+2 Z-AXIS STEERING PULSE TO NULL AGS ERRORS POINT Z-AXIS IN DIRECTION OF CSM MODE CONT-ATT HOLD ATT CONT(3)-MODE CONTROL O unnr - ZirF
5-3
SLEW PATE - LO
SLEW RR ANT TO OqON FUAI VERIFY MAX SIGNAL STRENGTH RH MOOE-AUTO TRACK NO TRACK LIGHT OFF -
ATT CONT(3h-PULSE
CHECK INSERTION VELOCITY WITH TAPEMETER COMPARE EAPEMETER WITH AGS STATE VECTOR DATA I
17R RANGE(NOM 2642)
440R RANGE RATE(NOM -425l)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
cSI
+3 417+1 (RADAR FILTER INITIALIZED) 41b+l (NO BOHESIGHT) b03-XXXXX RANGE RATE
+5 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGF
41b+1 CSI ROUTINE 373+o2065 CSi TIME 275+03028 TPI TIME 605+0077 COTANGENT OF LOS TO CSM 41b+1 (ONE-HALF OFBITAL-PERIOD) 411+0 HCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT
610R TIME TO CST
43 RESET ET
267R VELOCITY TO BE GAINED CSI
402R FLTA H
371R DFLTA V CDH
5-4
372R DFLTA T CSICDH
-42 415+1 (No BORESIGHT) bO6-xXXXX RANGE RATE
-40 415+1 (NO BORESIGHT)503-XXXXX RANGE RATE dORESIGHT ON CSM
415+1 316+XXXXX RANGE
-37 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE
-15 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE UORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-2 415+1 (No BOHESIGHT) bO3-XXXXX RANGF RATE
i1uR TIME TO CS
RESEF ET
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-30 COPY ROOT FOR 1ST CSI 81J
BORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-t7 415+1 (NO BORFSIGHT) 50-XXxXx RANGF RATE
267R VELOCITY TO HE GAINED CSI
402R LELTA H
371R OFLTA V COH
372R OELTA T CSICDH
-5 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 blb+XXXXX RANGE
-i2 415+1 (No BORESIGHT) 5n3-XXXXX RANGE RATE
415+1 (NO BORESIGHT)
5-5
503-XXXXX RANGF RATE
COPY Roor FOR 2NO CSI BU
bORESIGHT ON CSM 415+1 316+XXXXX RANGE
TEMPPRESS MON SEL - FUEL MAN
A AND 8 PRESS 181 +-3 PIG TEMPPRESS MON SEL - PRPLNT
A AND B TEMP IND 4ODEG 0 IOODEG F A AND B PRFSS IND 181 +-3 PSIA
tEMPPRESS MON SEL - HEL
A AND 8 PRESS IND PSIA
A QUANTITY IND- -- PERCENT RFMAINING
8 QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4p 2 3 (120 - 190 DFG F)
415+1 (NO BORESIGHT)-17 503-XXXXX RANGE RATE
-15 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
(LOS OF MSFN) S-BAND - SLEW 10 P = +90t Y U S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
-12 415+1 (No 8ORESIGHT)
503-XXXXX RANGE RATE
267R VFLOCITY TU BE GAINED CSI
402R OFLTA H
372R TIME CSICH
371R PREDICTED VEL 10 RE GAINED COH
263R OLT-OF-PLANE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATL
-10 COPY RANGE AND ROOT FOR 3RD CSI 8U
SORESIGH ON CSM 41b+1
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
LIST OF ACRONYMS AND ABBREVIATIONS ACQ ADJ AGS AOH AOS AOT APS ATT BU CALIB CB CDH CDR CM CMC CMD CMP COAS CSI CSM CT DAP DH DOI DPS DSKY DV DWN EMS ET FDAI FPS FWD GDC GET GETI GMBL GND HA HGA HOR HORIZ HP IMU INS IT LGC LM
Acquisition Adjust Abort Guidance System Apollo Operations Handbook Acquisition of Signal Alignment Optical Telescope Ascent Propulsion System Attitude Backup Calibration Circuit Breaker Constant Delta Height Commander Command Module Command Module Computer Command Module Commanders Position Command Module Pilot Crew Optical Alignment Sight Concentric Sequence Initiation Command and Service Module Cease Tracking Digital Autopilot Delta Height Descent Orbit Insertion Descent Propulsion System Display and KeyboardDelta Velocity Down Entry Monitor System Event Timer Flight Director Attitude Indicator Feet Per Second Forward Gyro Display Coupler Ground Elapsed Time Ground Elapsed Time of Ignition Gimbal Ground (Mission Control) Apogee Altitude High-Gain Antenna Horizon Horizontal Perigee Altitude Inertial Measurement Unit Insertion Initiate Tracking LM Guidance Computer Lunar Module
LV
-1v-
LMP LOI LOS
MNVR MCC MCCl MCC2 MCC-H MGA MSFN NAV ORDEAL PAD PB PC PDI PGNS PHS PIPA PLM PRO PROG PROP R RCS RDOT REFSMMAT RHC RR SHFT SC SEP SM SXT SYNC TFI THC THETA TIGN TLM TPF TPI TRUN TTCA VG VHF (XXXX) (XXXXX XX)
Lunar Module Pilot Lunar Orbit Injection Line Of Sight Launch Vehicle Maneuver Midcourse Correction First Midcourse Correction Second Midcourse Correction Mission Control Center - Houston Middle Gimbal Angle Manned Space Flight Network Navigation Orbital Rate Drive Earth and Lunar Data Voiced to Crew From Ground Pushbutton Plane Change Powered Descent Initiation Primary Guidance Navigation and Control System Phasing Pulse Integrating Pendulous Accelerometers LM Pitch Angle Proceed Program Propellant Range Reaction Control System Range Rate Reference Stable Member Matrix Rotation Hand Controller Rendezvous Radar Shaft Spacecraft Separation Service Module Sextant Synchronize Time From Ignition Translation Hand Controller Angle Between SC +X Axis and Local Horizontal Time of Ignition Telemetry Terminal Phase Finalization Terminal Phase Initiation Trunnion Translation Thrust Control Assembly Velocity to be Gained Very High Frequency Indicates GET From Liftoff in HoursMinutes Indicates GET From Liftoff in HoursMinutesSeconds
(XXXXXXXXXXXX) (OrdealInertial) Angles (Roll Pitch Yaw) (XXXXXX) Local Vertical DVs
Tracking Stations
ANG BDA CRO CYI GYM HSK HTV MAD MER MIL RED TEX VAN
-v-
Antigua Near Space Support Station Bermuda Near Space Support Station Carnarvon Near Space Support Station Canary Near Space Support Station Guaymas Near Space Support Station Honeysuckle Deep Space Support Station Huntsville Near Space Support Station Madrid Deep Space Support Station Mercury Near Space Support Ship MILA Near Space Support Station Redstone Near Space Support Ship Corpus Christi Near Space Support Station Vanguard Near Space Support Ship
10 PURPOSE
This document contains the primary procedures for the LM-5 active rendezvous with CSM-107 spacecraft in accordance with Detailed Test Objective Section 40 defined in Reference 71
The purpose of the LM Rendezvous Procedures document is to provide a single source of procedures information for use in flight planning in crew training and in preparing onboard data
This is a control document subject to review by all elements of the Apollo Program and to approval by the Procedures Conshyfiguration Control Board Comments should be directed to Mr Stephen P Grega Flight Procedures Branch Flight Crew Support Division Extension 5348
Beyond G mission planning no additional techniques and trajectory information specific to Mission H have been made available as of this date Therefore since Missions G and H are expected to be similar in the area of rendezvous guidance and navigation procedures the G mission final LM Rendezvous Procedures Document will serve -as an H mission preliminary LM Rendezvous and Procedures Document After reviewal by all elements of the Apollo Program and approval by the Procedures Configuration Control Board this document will then evolve into the control document for the Mission H crew procedures
2-1
20 INTRODUCTION
The LM-5CSM-l07 lunar orbit rendezvous exercise will beginduring the twenty-fourth CSM revolution with insertion at 122 35255 and end at approximately 1260000 with post rendezvous station keeping The LM procedures during this period are divided into segments of major activities which are discussed in detail in Section 30
A nominal LM-5CSM-107 mission profile is contained in Figshyure (2-1) This figure shows the locations in time and local horizontal position of the most significant nominal mission events Trajectory data used to generate the mission profile and timeline for procedures development was obtained from Reference 72 The rendezvous navigation update schedule assumed in the procedures is defined in Reference 73
A history of the LM body attitudes during the rendezvous accompanies the major events discussion and is also presented in Figures (2-2) and (2-3) Each figure illustrates the bodyattitudes with respect to the moon sun and earth and indicates FDAI roll pitch and yaw gimbal angles and the ordeal pitch angle for significant events during each lunar orbit
0RBI TR EL
TRAILINGDISPLACEMENT(N MI) 0 0 W60 20240 BE
33I I ] I I I
32 ltrMCCE 1125+-3 C CH (124t24) PLAN CHANGE023 TM)2
R~TC(222
40 1146235 A N MNTTIMETKS FROMISEDRT(GA122plusmn252
-- DAYLIGHT B shy
_ _ _ _ _ _ __E_ _ -- 7 LUNAR IARFAGELM MAJOR EVENTS
122+35 INSERTION 17 124+H7 AGE UPDATE AND ALIGN (R47) 2 122+40 IMU REFSMMAT ALIGN (P52) 1 124+24 CDH THRUSTING (P41) TRAILINGDISPLACEMETIN RI)
3 122+54 AGS UPDATE AND ALIGN (R471 19 124+26 TPI TARGETING IP34 amp AGS) 5 II 20 25 30 4 122+55 CSI TARGETING IP32 amp AGSI 20 124+26-124+51 RR NAVIGATION (P20 18 MARKS) - I I
5 122+54-123+14 RR NAVIGATION (P20 18 MARKS) 21 124+53 AGS UPDATE AND ALIGN (R47)I
6 123+18 COMPUTE CSI BACKUP 22 125+00 COMPUTE TPI BACKUP
7 123+19 AGS UPDATE AND ALIGN (R471 23 125+03 TPI THRUSTING (P411 c
8 123+26 CSI THRUSTING (P411 24 125+05 MCC1 TARGETING IP35) N - M ((25+232
9 123+30 SET W MATRIX 1200025) 25 125+05-125+16 RR NAVIGATION IP20 9 MARKS) 5
2 r INSERT A 10 123+31 CDH TARGETING IP33 amp AGS 26 125+16 COMPUTE MCCI THRUSTING IP41) 5 31 PHAE
11 123+31-123+46 RR NAVIGATION 1P20 14 MARKS) 27 125+18 MCC I THRUSTING (P41)
12 123+47 EXT AV FOR PLANE CHANGE (P20) 28 125+20 MCC2 TARGETING (P351 13 123+54 RCS PLANE CHANGE THRUSTING (P411 29 125+20-125+31 RR NAVIGATION (P20 9 MARKS) 14 123+56 CDH TARGETING (P33 amp AGS) 30 125+31 COMPUTE MCC 2 BACKUP Ideg
15 123+56-124+12 RR NAVIGATION (P20 13 MARKS) 31 125+33 MCC2 THRUSTING [P41)
16 124+15 COMPUTE CDH BACKUP 32 125+48 BRAKING (P47) 27 26TP25+03
33 126+00 STATION KEEPING LT
24
FIGURE 2-1 G MISSION RENDEZVOUS
(CSM-CENTERED RELATIVE MOTION) FOLDOUT FRAME
l D T R2A-e2 TALPFO EDUR ES EPREPAREDBY STEPHENP GRED501I DOUT FRAMW ORBI R B C 0
MISSION G LUNAR ORBIT RENDEZVOUS ATTITUDE TIME HISTORY
OFOR THE LM P33
P20 123+31) (021880)
LMI CSI NrxNMARKS i (123+26+27)
FINAL -
COMP(I123+1l6)
P32 LANDING SITEj P20 30ES (122+50) CSM AT (04650) PRIME MERIDIAN LIFT-OFF
P52 (122+28+11) (122+40)DIRECTION OF (03640)ORBITAL MOTION IS
CLOCKWISE
(18012150)I NERTIAL YAWKLINERTIAL PITCH
ORDEAL PITCH EARTHINERTIAL ROLL
FIGURE 2-2
MISSION G LUNAR ORBIT RENDEZVOUS ATTITUDE TIME HISTORY
FOR THE LM
LM TPF (126+00+00) (01302920)
LM LMC2PLANE CHANGELMPI+30) (123+54+25)
(TPI+30) (0560)(0782400) 7 SUN
P20
(TPI+15) P3
P33(0532480) COMP
---- _ (124+12--- ---
LM TPI (125+02+46) L D (026 627650) (124+24+25)
(0980)
FINAL
DIRECTION OF COMP ORBITAL MOTION IS (124+50)
CLOCKWISE
(18012150)
LL INERTIAL YAW NERTIAL PITCH
ORDEAL PITCH EARTH INERTIAL ROLL
FIGURE 2-3
3-1
30 DISCUSSION OF MAJOR EVENTS
31 Concentric Sequence Initiation
Immediately following Insertion the LM navigated vector will be downlinked to Mission Control Center-Houston this state vector is then uplinked to the CSM The LM commander will perform a Proqram 52 fine alignment to REFSMMAT at approxishymately 12240
The digital autopilot is configured to wide deadband Program P20 is called and an automatic pitch maneuver is initiated to the preferred track attitude At 122 55 CSI targeting parameters are loaded in the PGNS and AGS A period of rendezvous radar marking will then take place from 122-57 to 12315 Upon completion of tracking the LM will obtain an out-of-plane velocity from the CSM to be vectored with the in-plane component of the CSI delta V The CSMs estishymate of out-of-plane velocity is alleged to be better than the LMs estimate (Reference 74)
At approximately 123 20 the LM will voice its CSI solution to the CSM the AGS is updated aligned and targeted in external delta-V with the CDH solution to be excuted Program P41 will then be called and the automatic pitch maneuver bypassed since the burn isto be executed with Z-Axis thrusting The CSI burn occurs nominally at 123 26 27 After verification of the LM CSI burn the CSM will incorporate the LM burn parameters in its CMC LM state vector
32 Constant Delta Height and Plane Change
At 12330 approximately three minutes after the LM CSI burn the W matrix will be set to (200025) and the LM targeting paramters are loaded in both the PGNS and AGS for the CDH maneuver Out-of-plane velocity will then be computed and voiced to the LM from the CSM Program P30 is loaded with the targeting parameters for the LM Plane Change maneuver which will be accomplished in Program P41 30 minutes prior to the CDH maneuver Following the burn the target delta V parameters are voice to the CSM and incorporated into the CMC LM state vector At 12356 the CDH targeting parameters are loaded in both the PGNS and AGS for 1242425 A CDH chart solution is calculated 7 minutes prior to TIG The AGS is updated aligned and targeted in external delta V with the CDH solution to be executed The RCS Thrust Program P41 is called at 12418 and the burn attitude is bypassed since the LM executes CDH by thrusting out individual components of delta V while maintaining radar lock-on
3-2
3 3 Terminal Phase Initiation
Radar tracking is initiated after the CDH maneuver and updating of the LGC continued At 12426 approximately two minutes after the LM CDH burn targeting parameters are loaded in both the PGNS and AGS for the TPI maneuver which will be targeted for a node at intercept Backup measurements are made at the appropriate times The AGS is updated aligned and targeted in external delta V with the TPI solution to be executed The RCS Thrust Program P41 is called at 12456 and the burn attitude is bypassed since the LM is burning along the plus Z-axis with the thrust direction established with the COAS
3 4 Midcourse Corrections
Immediately after TPI the Midcourse Prethrust Program P35 will be called and radar tracking reinitiated Backup measshyurements are made and midcourse corrections chart solutions obtained The MCCl burn will nominally be performed at TPI plus 15 minutes (1251746) If MCCI is to be excuted Program P41 will be called and the burn attitude maneuver is bypassed since the plus Z-axis will remain boresighted at the CSM until docking
Following MCCI Program P35 will be called and targeted for MCC2 at TPI plus 30 minutes (1253246) and executed identishycally to MCCI
3 5 Braking
In preparation for braking the DAP is configured in narrow deadband Program P20 is terminated at 18000 feet but the radar is kept in auto track to provide radar range and range rate displayed on the tapemeter Average G is called by Program P47 prior to braking and attitude hold is selected The braking schedule is followed as contained in Section 4
4-1
40 NOMINAL MISSION PROCEDURES
The procedures included in this section do not specify which crewmember Commander or LM Pilot performs each task These need not be specified since the following basic rules define which crewmember performs each task
41 Commander Tasks
1 All attitude changes whether manual or automatic will be accomplished by the CDR
2 The operation of the DSKY during thrust programs (P40 P41 P42 P47) will be done by the CDR Actual manipulation of the TTCA need not be always done by the CDR but in most cases will be
3 Operation of the rendezvous and landing radar will be done by the CDR
4 The CDR will operate all other systems accessible to only his crew station
42 LM Pilot Tasks
1 AGS operation 2 DSKY operation will be done by the LMP except when keyboard
entries affect the control of spacecraft attitude or thrustshying
3 Backup data logging and chart calculations 4 All logging of maneuver solutions and systems performance 5 The LMP will operate all other systems accessible to only
his crew station
These general rules are guidelines only and may be deviated from by the LM crew if they develop more efficient Task assignments
43 ABBREVIATIONS
The abbreviations used herein are consistant with those in the AOH However in order to condense and simplify the procedures so that they are representative of onboard data a number of addshyitional shorthand conventions have been used To allow the unshyfamiliar reader to understand the procedures contained in this section the following explanations are included
1 AGS - A single asterisk is employed to denote those procedures involving operations to be performed on the DEDA The three number group following an asterisk specifies DEDA address An Rfollowing the address group indicates the address is to be read out A five digit group behind the Rindicates a nominal or expected display If the three number address group is followed by a plus or minus sign a data load is indicated When a single digit follows the plus addition of four zeros behind this digit is assumed Once used these conventions are easily handled and save considerable space
4-2
2 PGNS - The verb-noun addresses in the PGNS are indicated to the left of the procedures column An F is used to indicate a flashing display or absence of an F a static display To the right of the verb-noun on the same line are the contents of the three data registers If numeric quantities appear the DSKY should be correspondingly made to agree by executing a V21 V22 or V23 and performing a data load The procedure of blanking and loading registers is not included since it is repeated often and is highly familiar to the crews
EXAMPLE F 06 33 125-02 46 TIG OF TPI
Expanded this means Load flashing verb 06 noun 33 with the quantity 125 hours 2 minutes and 46 seconds the time of ignition of the RCS engine TPI maneuver Procedurally this is done by keying verb 25 enter loading +000125 in register 1 +00002 in register 2 and +04600 in register 3
If numberic quantities do not follow the verb-noun it is indicated that a computed or information quantity is being displayed via the DSKY If nominal values are listed for possible comparison they appear in parentheses
EXAMPLE- F 06 42 HA HP V
Expanded this means Flashing verb 06 noun 42 has computed height of apogee in register 1 height of perigee in regshyister 2 and velocity to be gained in register 3
3 TIME - The numbers in the left hand column preceded by a plus or minus indicate event timer time referenced to an event Minus indicates event timer counting down to a future event Periodically this same column contains the nominal mission ground elapsed times in parentheses Asterisks following the event time indicate a time critical event which should be accomplished to the nearest second
4-3
4 4 Nominal PGNS Procedures
ASSUMPTIONS
AFTER INSERTION
1 INSERTION COMPLETE (RESIOUALS NULLED) VERIFY V82E (ORBIT) 3 RNDZ RDR LOCKED ON IN MODE II 4 LGC AT FLASHING VERB 37 5 PROPER INITIAL W MATRIX LOADED IN LGC
GUID CONT-PGNS ATTITUDE MON-PGNS(CDR) RATE ERR MON-CMPTR(LMP) ATTITUDE MON-AGS(LMP) SHFTTRUN-+5 DEG X-POINTER-HI MULT RADAR TEST SW-OFF ENG ARM-OFF X-TRANSL-2JETS DEAD BAND-MIN PGNS MODE CONT-AUTO THROTJET-JET CBPGNS IMU OPR-CLOSE RR MODE-LGC TTCATRANSL-ENABLE(COR)
BAL CPL-ON MODE SEL-AGS
RNGALT MON-RNGRNGRT RATE ERR MON-RNDZ RORICOR) ATT CONT-PULSE(3)
AGS MODE CONT-ATT HOLD ACA4JET-DISABLE(CDRJ TTCATRANSL-DISABLE(LMP)
ACA4JET-DISABLE(LMPI
KEY ODE (PO0)
(DOWNLINK LM STATE VECTOR)
KEY V63E (RR SELF TEST)
4-4
F 04 12 00004 00001 PRO
F 16 72 TRUN SHFT PRO
F 16 78 R ROOT VERIFY TAPE METER WITH DSKY
+2 VERIFY INSERTION VELOCITY WITH RNDZ ROR WHERE RANGE = 2642 NM RANGE RATE = -4251 FPS
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
KEY V34E (TERMINATE) KEY V48E (LOAD DAP)
F 01 46 11002 PRO
F 06 47 LMWT CMWT PRO
KEY V56E (KILL AUTO TRACK ENABLE)
+3 KEY V41N72E (COARSE ALIGN RR) F 21 73 +000OOTRUN -077OOSHFT F 04 12 00006 00002 (CONTINUOUS DESIGNATE)
PRO 41 (COARSE ALIGN VERB)
KEY VI6N72E 16 72 MONITOR TRUNSHFT ANGLES
CB PGNS RNDZ RDR-OPEN CB AC BUS A RNDZ RDR-OPEN KEY V44E (TERMINATE RR DESIGNATE)
KEY V83E F 16 54 R ROOT THETA
SET ORDEAL PRO
CS HEATER AOT-CLOSE
CB AOT LAMP-CLOSE
+5 KEY V37E52E (IMU REALIGN)
4-5
410+1 CSI ROUTINE 373+02065 CS TIME 275+03028 TPI TIME
605400777 COTANGENT OF LOS TO-CSM 416+1 (ONE-HALF bRBITAL PERIOD) 411+0 RCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT 310R TIME TO CS
267R VELOCITY TO BE GAINED CSI
402R DELTA H
371R DELTA V CDH
372R _ DELTA T CSICDH
F 04 06 00001 00003 -(REFSMMAT) PRO -
F 50 25 00015 SELECT 1ST STAR ENTR
F 01 70 O02DE LOAD 1ST STAR PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FOAl ANGLES (AUTO MNVRI)
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVR)
F 01 71 002DE
KEY V76E PGNS MODE CONT-ATT HOLD
PRO +10 F 54 71 MARK 1ST STAR
PRO F 01 70 O02DE LOAD 2ND STAR
PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FDA ANGLES -(AUTO MNVRV
F 50 18 FDAI ANGLES (REQUEST PNVRt ENTR (BYPASS MNVR
F 01 71 002DE PGNS MODE CONT-ATT HOLD PRO
-35
4-6
+14 F 54 71 MARK 2ND STAR PRO
F 06 05 STAR ANGLE DIFFERENCE PRO
F 06 93 GYRO TORQUE ANGLES PRO
F 50 25 00014
PRO (CHECK ALIGNMENT IF TIME WILL PERMIT)
F 50 25 00015 SELECT 3RD STAR ENTR
F 01 70 OO2DE LOAD 3RD STAR PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FDAI ANGLES (AUTO MNVR)
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVR)
VERIFY ALIGNMENT VIA AOT
KEY V34E (TERMINATE) F 37 BB
V48E (LOAD DAP) F 01 46 11012
PRO F 06 47 LMWT CMWT
+17 PRO
CB AOT LAMP-OPEN
RESET ET (310R)
(12253) CB AC BUS A RNDZ RDR-CLOSE (WAIT 30 SEC) CB PGNS RNDZ RDR-CLOSE
RR MODE-LGC KEY V37E20E (ACQUIRE RADAR)
PGNS MODE CONT-AUTO F 50 18 FDA ANGLES (REQUEST MNVRJ
PRO (AUTO MNVR) 06 18 FDAI ANGLES (AUTO MNVR)
AGS MODE CONT-AUTO RATEERR MON-CMPTR (LMP)
F 50 18 FDAI ANGLES (REQUEST MNVR)
4-7
ENTR (BYPASS MNVR) NO TRK LT-OFF
F 50 72 RR TRUNSHFT VERIFY RR LOCK ON PRO
DSKY BLANKS
KEY V93E (BEFORE 1ST MARK REINIT W MATRIXI KEY V80E (UPDATE LM SV)
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (i20OOZOO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
400+3 AGS ALIGNshy400R (00000 COMPLETE) 507+0 Z-AXIS BORESIGHT 400+2 ACQUISITION STEERING
CS
(122amp55) KEY V37E32E (CSI)
F 06 11 1 S LOAD TIG CSI FROM DATA PAD (NOM 123S26- 271 PRO
F 06 55 +O000IN +02660E +13000 OMEGAT (CDH 180 DEG AFTER CSI PRO
F 06 37 LOAD TIG TPI FROM DATA PAD (NOM 1251021761 PRO
F 16 45 MKS TFI -00001
-30 COPY RDOT FOR 1ST CSI BU
31OR TIME TO CSI
267R VELOCITY TO BE GAINED CSI
402R DELTA H
371R DELTA V CDH
-22
4-8
372R _ DELTA T CSICDH
KEY V32E (MARKS=5
F 06 75 DELTA H DELTA T CSICDH DELTA T CDHTPI PRO
F 06 81 DELTA VOS-LV (CS) (NOM 501 DELTA VX)
CSI(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (CDH)
(NOM 60 DELTA VX) CDH(82)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
KEY V32E (MARKS=1C)
F 06 75 DELTA H DELTA TCSICDH DELTA TCDHTPI PRD
F 06 81 DELTA VS-LV (CSI) CSI(N811
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 82 DELTA VIS-LV(CDH)
CDH(82)
DELTA VX(LVI
DELTA VY(LV)
DELTA VZ(LV)
-12
4-9
-20 COPY RDOT FOR 2ND CSI BU
F 16 45
F 06 75
F 06 81
F 06 16
F 06 90
PRO MKS TFI -00001
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS NON SEL - PRPLNT A + B TEMP IND 40DEG TO lOODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + 8 PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4v 2 3 (120 - 190 DEG F
(LOS OF MSFN ) S-BAND - SLEW TO P = +90 Y a 0 S-BAND - FWD (OR AFT) S-BAND - DN VOICE BU BIOMED OFF
PRO (FINAL COMP)
267R - VELOCITY TO BE GAINED CSI
402R DELTA H
372R TIME CSICDHL
371R PREDICTED VEL TO BE GAINED CDH
263R OUT-OF-PLANE
DELTA H DELTA TCSICDH DELTA TCDHTPI PRO DELTA VS-LV (CSI)
KEY V9OE (OUT-OF-PLANED
0 LOAD TIG CSI FROM DATA PAD (NOM 12302627) PRO Y YDOT PSI
N90 CSM
YDOT
PRO
-7
4-10
F 06 81 DELTA VS-LV(CSI)
COPY YDOT FROM CSM AND LOAD NEGATIVE IN R2 CSIIN81I
DELTA VX(LV)
DELTA VYILV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (COH)
CDH(82)
DELTA VX(LV)
- DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RANGE AND RDOT FOR 3RD CS BU
COMPUTE CSI BU
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (i2000OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
(TRANSMIT CSI DATA TO CSMI VHF A XMTR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF TELEMETY PCM - LO
KEY VB3E F 16 54 R ROOT THETA
SET ORDEAL PRO
317R RANGE
440R RANGE RATE
4-11
400+3 AGS ALIGN t40OR (00000 COMPLETE)
277R THETA
PRO F 37 BB
-6 KEY 41E (RCS THRUSTING) F 50 18 FDAI-ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTAV 400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTAV 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA RF
TRANSMIT TGT DELTA VS TO CSM AND SYNC COUNTDOWN
16 85 DELTA VS-BODY
502R DELTA VZ (NOM 5Ql)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTAVS-BODY
(123t26t27) BURN +Z
NULL DELTA VS
4-12
VERIFY AGS RESIDUALS 50OR 501R 502R DELTA VX _ DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
CDH
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
KEY V67E (RESET W MATRIX) F 06 99 +0200E +O0020E +00005E
PRO
507+0 Z-AXIS BORESIGHT
(VHF RANGING WITH CSM) VHF A XMTR - VOICERNG VHF B XMTR - OFF VHF B RCVR - ON TELEMETRY PCM - HI
(12331) KEY V37E33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 a TIG CDH (NOM 1242425) -120 amp00 10 (AGS 0 TIME)
(CONVERT TO MINUTES)
411+0 THRUST ALONG Z-BODY AXIS ENTER IF YOU DONT TARGET CSI
373R (NOM 26443 310R TIME TO CDH
4-13
423R DESIRED ALT RATE AT CDH
402R DELTA Hshy
450R DELTA VX
452R DELTA VZ
623+0 Z-AXIS PARALLEL TO CSM PLANE
IPRO F 16 45 MKS TFI -00001
-52 RESET ET
KEY V93E (REINIT W MATRIX WHEN MARKS =4)
KEY V32E (MARKS = 3)
F 06 75 DELTA HCDH DELTA TCDHTPI DELTA TTPI PRO
F 06 81 DELTA VCDH-LV CDH(N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
-47 KEY VSOE (OUT-OF-PLANE)
_ TIG CDH (NOM 124t24t25) -3000 TIME FROM CDH
F 06 16 l1 LOAD TIG PLANE CHANGE (NOM 123amp54-253 PRO
F 06 90 Y YDOT PSI N90 CSM
VYDOT PRO
-42 KEY V32E (MARKS=1O)
F 06 75 DELTA HCDH DELTA TCDIHTPI DELTA TTPITPI PRO
F 06 81 DELTA VCDH-LV
4-14
CDH (NS1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -OO1
KEY V34E (TERMINATE) F 37 B8
PLANE CHANGE
KEY 30E (EXTERNAL DELTA V)
TIG CDH (NOM 124124t25) -3000 TIME FROM CDH
F 06 33 LOAD TIG PLANE CHANGE (NOM 123154T25) PRO
F 06 81 DELTA VS-LV (NOM 00)
-36 COPY RDOT FOR 1ST CDH BU
KEY V90E (OUT-OF-PLANE)
F 06 16 1 1 LOAD TIG PLANE CHANGE (NOM 1231543251 PRO
F 06 90 Y YOOT PSI N90 CSM
YDOT
PRO
F 06 81 DELTA VS-LV(NOM 00)
COPY YDOT AND LOAD NEGATIVE IN R2 PRO
F 06 42 HA HP DELTA V PRO
F 16 45 MKS TFI MGA
PRO
F 37 BB
KEY 41E (RCS THRUSTING)
-30
4-15
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVRI
410+5 EXTERNAL DELTA V 450+0 451-YDOT 452+0 (LOAD CSM -YDOT)
407+0 ROTATE EXTERNAL DELTA V RF
16 95 DELTA VS-BODY
-3035 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATTVHOLD 407+1 FREEZE EXTERNAL DELTAV
F 16 85 DELTA VS-BODY -
NULL DELTA VIS
PRO F 37BB
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
507+0 Z-AXIS BORESIGHT
(12356) KEY 33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 TIG CDH (NOM 124t24t25) -120 OO ZOO (AGS 0 TIME)
(CONVERT TO MINUTES)
373R _ (NOM 2644) 310R TIME TO CDH
423R DESIRED ALT RATE AT CDH
(ADS OF MSFN) S-BAND - SLEW TOP = ACQUIRE HGA LOCK ON VOICE - BUVOICE -- VOICE VERIFY VOICE TLM BIOMED - LEFT (OR RIGHT)
402R DELTAH
4-16
F 16 45
-25
-23
F 06 75
F 06 81
F 16 45
-12
F 06 75
F 06 81
450R DELTA VX
452R DELTA VZ
PRO MKS TFI -00001
KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
COPY ROOT FOR 2ND CDH BU
KEY v32E (MARKS = 5)
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40DEG TO 1OODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + B PRESS IND PSIA
A QUANTITY IND _ PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING a TEMP MON SEL RCS QUAD 1 4 2 3 (120 - 190 DEG F)i
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
CDH(NB1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO MKS TFI -00001
PRO (FINAL COMP)
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
KEY V9OE (OUT-OF-PLANE)
-7
4-17
F 06 16 jj LOAD TIG CDH FROM DATA PAD (NOM 12424251 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT PRO
COPY YOOT FROM CSM AND LOAD NEGATIVE IN R2
CDH(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RDOT FOR 3RD CDH BU
COMPUTE CDH BU
TRANSMIT TGT DELTA VOS TO CSM AND SYNC COUNTDOWN
KEY V47E (INITIALIZE AGS F 06 16 GET OF AGS 0 TIME 120O00OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
KEY V83E F 16 54 R RDOT THETA
SET ORDEAL PRO
317R _ RANGE
440R RANGE RATE 400+3 AGS ALIGN 40OR (00000 COMPLETE)
277R THETA
-6
4-18
PRO F 3 BB
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY V06N86E F 06 86 DELTA VIS-LV
AGS(N86) CHART
DELTA VX(LVD
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
16 85 DELTA VS-BODY
50OR DELTA VX (NOM -0O3)
502R DELTA VZ (NOM 60)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD 407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS BODY
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS 5OOR 50IR 502R DELTA VX -DELTA VY DELTA VZ-
VERIFY PGNS RESIDUALS N85
DELTA VX(LM)
4-19
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
TPI
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO 507+0 Z-AXIS BORESIGHT
(12426) KEY 34E (TPI)
-36 RESET ET
F 06 37 - amp LOAD TIG TPI FROM DATA PAD (NOM 1250246) PRO
F 06 55 +00000 +02660E +13000 OMEGAT PRO
F 16 45 MARKS TFI -00001
-32 KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
-29 KEY V32E (MARKS = 3)
F 06 37 __ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
RESET ET
410+3 TPI SEARCH ROUTINE 307+04300 DELTA T TRANSFER
4-20
-26 310+02600 TFI TPI
303R THETA AT TPI
267R DELTA VTPI
371R DELTA VTPI + DELTA VTPF
KEY V32E (MARKS = 10)
F 06 37 _ _ _ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VIS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
TEMPIPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40ODEG TO IGODEG F A + B PRESS IND 181 +-3 PSIA
TEMPIPRESS MON SEL - HEL
A + B PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD I 4 2 3 (120 - 190 DEG F)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
RESET ET
-13 310+01300 TFI TPI
303R THETA AT TPI
-12 PRO (FINAL COMP) F 06 37 Z TIG TPIj__
4-21
TRANSMIT TIG OF TPI TO CSM-
PRO F 06 58 HP DELTA VTPI DELTA VTRF
PRO F 06 81 DELTA VS-LV
KEY V9OE (OUT-OF-PLANE)
F 06 16 1 LOAD TIG TPI FROM DATA PAD (NOM 12502461 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT
PRO F 06 81 DELTA VS-LV
COPY CSM YDOT AND LOAD NEGATIVE IN R2 N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 59 DELTA VS LOS
N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI MGA
RESET ET
PRO F 37 BB
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (12000t600)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE)
-10
-6
4-22
F 50 16 DOWNLINK COMPLETE PRO (UPDATE COMPLETE)
400+3 AGS ALIGN 400R (00000 COMPLETE)
-9 277R COPY TGT LOS ANGLE
310+00800
303R THETA AT TPI 410+4 DIRECT TRANSFER AT ET=-8 404+0 405+0 406+0 (MONITOR 470 471 4721
373R TIG TPI
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
KEY 41E (RCS THRUSTING) F 50 18 FOAl ANGLES (REQUEST MNVRI
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
-5 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUS
400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
COMPUTE TPI BU
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
4-23
1685 DELTA VS-BODY
50OR DELTA VX(NOM -115)
502R DELTA VZ(NOM 229)
-Z35 OSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS-BODY
(1250246) BURN +Z
VERIFY AGS RESIDUALS 500R 501R 502R DELTAVX DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
MCC1
KEY V76E (PGNS PULSE) PGNSMODECONT-AUTO
KEY V93E (BEFORE 1ST MARK REINITW MATRIX)
+2 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
4-24
(LOS OF MSFN) S-BAND - SLEW TO P = 90 Y = 0 S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
404+0 405+0 406+0
(MONITOR 470 471 4721
+9 277R COPY TGT LOS ANGLE
+12 PRO (COMPUTE MCC FOR TPI+15I F 06 81 DELTA VS-LV
PRO F 06 59 DELTA VS-LOS
PRO F 16 45 MKS TFI MGA
+13 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUOS
COMPUTE MCC1 BU
PRO F 37 BB
+14 KEY 41E (RCS THRUSTING) F 50 18 FOAL ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+1425 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+15 F 16 85 NULL DELTA VS
PRO F 37 BB
MCC2
KEY V76E (PGNS PULSE)
4-25
PGNS MODE CONT-AUTO
KEY V93E (BEFORE 1ST MARK REINIT W MATRIX)
+16 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
404+0 405+0 406+0 (MONITOR 470 471 47)shy
+24 277R COPY TGT LOS ANGLE
+27 PRO (COMPUTE MCC FORTPI+30) F 06 81 DELTA VS-LV
PRO F 06 59 DELIA VPS-LOS
PRO F 16 45 MKS TFI MGA
+28 277R COPY TGT LOS ANGLE
COPY R RDOT FROM TAPEMETER FOR BUS
COMPUTE MCC2 BU
F 37 BB PRO
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+2925 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+30 F 16 85 NULL DELTA VS
PRO F 37 BB
KEY OOE (P001
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
4-26
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT KEY V34E (TERMINATE)
KEY V37E47E (AVE G) F 16 83 DELTA VIS
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT VERIFY TAPE METER WITH DSKY
BRAKING GATE 30 FPS - 6000 FT 20 FPS - 3000 FT 10 FPS - 1500 FT 5 FPS - 600 FT
RENDEZVOUS
STATION KEEPING
5-1
50 ABORT PROCEDURE
This is a specific AGS nominal abort procedure due to a PGNS failure between insertion and station keeping
51
5-2
Nominal AGS Procedures
ASSUMPTIONS
AFTER INSERTION
I INSERTION COMPLETE (RFSIDUALS NULLED) g PGNS FAILURE BEFORE INSERTION 3 RAUAR NOT LOCKED ON
(UI CoNT-AGS ATlI[uUE MON-AGS(CDR) RATE ERR MON-CNPTR(LMP) ATTITUDE MON-AGS(LMP) SHFITRUN-+5 DEG X-POINTER-HI MULT RADAR IEST Sw-OFF LNb GMbL-OFF ENG ARM-OFF X-IRANSL-2 JETS DEAD BAND-MAX PGNS MODE CONT-OFF THROTJET-JET CB IMU OIR-ON HH MOVE-AUTO rRACK TTCATNANSL-ENABLE(CDR)
AL CPL-ON MODE SL-AGS RNGAL1 MON-RNbRNGRT RAIE ERR MON-RNDZ HDR(CDR) AVl CoNT(3)-PULSE AGS MODE CONT-AUTO ACA4JET-DISABLE(CDR) TTCATRANSL-DISABLE(LMP) ACA4JET-DISABLE(LMP)
bO7+U Z-AXIS BOPESIGHT 400+2 Z-AXIS STEERING PULSE TO NULL AGS ERRORS POINT Z-AXIS IN DIRECTION OF CSM MODE CONT-ATT HOLD ATT CONT(3)-MODE CONTROL O unnr - ZirF
5-3
SLEW PATE - LO
SLEW RR ANT TO OqON FUAI VERIFY MAX SIGNAL STRENGTH RH MOOE-AUTO TRACK NO TRACK LIGHT OFF -
ATT CONT(3h-PULSE
CHECK INSERTION VELOCITY WITH TAPEMETER COMPARE EAPEMETER WITH AGS STATE VECTOR DATA I
17R RANGE(NOM 2642)
440R RANGE RATE(NOM -425l)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
cSI
+3 417+1 (RADAR FILTER INITIALIZED) 41b+l (NO BOHESIGHT) b03-XXXXX RANGE RATE
+5 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGF
41b+1 CSI ROUTINE 373+o2065 CSi TIME 275+03028 TPI TIME 605+0077 COTANGENT OF LOS TO CSM 41b+1 (ONE-HALF OFBITAL-PERIOD) 411+0 HCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT
610R TIME TO CST
43 RESET ET
267R VELOCITY TO BE GAINED CSI
402R FLTA H
371R DFLTA V CDH
5-4
372R DFLTA T CSICDH
-42 415+1 (No BORESIGHT) bO6-xXXXX RANGE RATE
-40 415+1 (NO BORESIGHT)503-XXXXX RANGE RATE dORESIGHT ON CSM
415+1 316+XXXXX RANGE
-37 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE
-15 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE UORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-2 415+1 (No BOHESIGHT) bO3-XXXXX RANGF RATE
i1uR TIME TO CS
RESEF ET
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-30 COPY ROOT FOR 1ST CSI 81J
BORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-t7 415+1 (NO BORFSIGHT) 50-XXxXx RANGF RATE
267R VELOCITY TO HE GAINED CSI
402R LELTA H
371R OFLTA V COH
372R OELTA T CSICDH
-5 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 blb+XXXXX RANGE
-i2 415+1 (No BORESIGHT) 5n3-XXXXX RANGE RATE
415+1 (NO BORESIGHT)
5-5
503-XXXXX RANGF RATE
COPY Roor FOR 2NO CSI BU
bORESIGHT ON CSM 415+1 316+XXXXX RANGE
TEMPPRESS MON SEL - FUEL MAN
A AND 8 PRESS 181 +-3 PIG TEMPPRESS MON SEL - PRPLNT
A AND B TEMP IND 4ODEG 0 IOODEG F A AND B PRFSS IND 181 +-3 PSIA
tEMPPRESS MON SEL - HEL
A AND 8 PRESS IND PSIA
A QUANTITY IND- -- PERCENT RFMAINING
8 QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4p 2 3 (120 - 190 DFG F)
415+1 (NO BORESIGHT)-17 503-XXXXX RANGE RATE
-15 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
(LOS OF MSFN) S-BAND - SLEW 10 P = +90t Y U S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
-12 415+1 (No 8ORESIGHT)
503-XXXXX RANGE RATE
267R VFLOCITY TU BE GAINED CSI
402R OFLTA H
372R TIME CSICH
371R PREDICTED VEL 10 RE GAINED COH
263R OLT-OF-PLANE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATL
-10 COPY RANGE AND ROOT FOR 3RD CSI 8U
SORESIGH ON CSM 41b+1
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
LV
-1v-
LMP LOI LOS
MNVR MCC MCCl MCC2 MCC-H MGA MSFN NAV ORDEAL PAD PB PC PDI PGNS PHS PIPA PLM PRO PROG PROP R RCS RDOT REFSMMAT RHC RR SHFT SC SEP SM SXT SYNC TFI THC THETA TIGN TLM TPF TPI TRUN TTCA VG VHF (XXXX) (XXXXX XX)
Lunar Module Pilot Lunar Orbit Injection Line Of Sight Launch Vehicle Maneuver Midcourse Correction First Midcourse Correction Second Midcourse Correction Mission Control Center - Houston Middle Gimbal Angle Manned Space Flight Network Navigation Orbital Rate Drive Earth and Lunar Data Voiced to Crew From Ground Pushbutton Plane Change Powered Descent Initiation Primary Guidance Navigation and Control System Phasing Pulse Integrating Pendulous Accelerometers LM Pitch Angle Proceed Program Propellant Range Reaction Control System Range Rate Reference Stable Member Matrix Rotation Hand Controller Rendezvous Radar Shaft Spacecraft Separation Service Module Sextant Synchronize Time From Ignition Translation Hand Controller Angle Between SC +X Axis and Local Horizontal Time of Ignition Telemetry Terminal Phase Finalization Terminal Phase Initiation Trunnion Translation Thrust Control Assembly Velocity to be Gained Very High Frequency Indicates GET From Liftoff in HoursMinutes Indicates GET From Liftoff in HoursMinutesSeconds
(XXXXXXXXXXXX) (OrdealInertial) Angles (Roll Pitch Yaw) (XXXXXX) Local Vertical DVs
Tracking Stations
ANG BDA CRO CYI GYM HSK HTV MAD MER MIL RED TEX VAN
-v-
Antigua Near Space Support Station Bermuda Near Space Support Station Carnarvon Near Space Support Station Canary Near Space Support Station Guaymas Near Space Support Station Honeysuckle Deep Space Support Station Huntsville Near Space Support Station Madrid Deep Space Support Station Mercury Near Space Support Ship MILA Near Space Support Station Redstone Near Space Support Ship Corpus Christi Near Space Support Station Vanguard Near Space Support Ship
10 PURPOSE
This document contains the primary procedures for the LM-5 active rendezvous with CSM-107 spacecraft in accordance with Detailed Test Objective Section 40 defined in Reference 71
The purpose of the LM Rendezvous Procedures document is to provide a single source of procedures information for use in flight planning in crew training and in preparing onboard data
This is a control document subject to review by all elements of the Apollo Program and to approval by the Procedures Conshyfiguration Control Board Comments should be directed to Mr Stephen P Grega Flight Procedures Branch Flight Crew Support Division Extension 5348
Beyond G mission planning no additional techniques and trajectory information specific to Mission H have been made available as of this date Therefore since Missions G and H are expected to be similar in the area of rendezvous guidance and navigation procedures the G mission final LM Rendezvous Procedures Document will serve -as an H mission preliminary LM Rendezvous and Procedures Document After reviewal by all elements of the Apollo Program and approval by the Procedures Configuration Control Board this document will then evolve into the control document for the Mission H crew procedures
2-1
20 INTRODUCTION
The LM-5CSM-l07 lunar orbit rendezvous exercise will beginduring the twenty-fourth CSM revolution with insertion at 122 35255 and end at approximately 1260000 with post rendezvous station keeping The LM procedures during this period are divided into segments of major activities which are discussed in detail in Section 30
A nominal LM-5CSM-107 mission profile is contained in Figshyure (2-1) This figure shows the locations in time and local horizontal position of the most significant nominal mission events Trajectory data used to generate the mission profile and timeline for procedures development was obtained from Reference 72 The rendezvous navigation update schedule assumed in the procedures is defined in Reference 73
A history of the LM body attitudes during the rendezvous accompanies the major events discussion and is also presented in Figures (2-2) and (2-3) Each figure illustrates the bodyattitudes with respect to the moon sun and earth and indicates FDAI roll pitch and yaw gimbal angles and the ordeal pitch angle for significant events during each lunar orbit
0RBI TR EL
TRAILINGDISPLACEMENT(N MI) 0 0 W60 20240 BE
33I I ] I I I
32 ltrMCCE 1125+-3 C CH (124t24) PLAN CHANGE023 TM)2
R~TC(222
40 1146235 A N MNTTIMETKS FROMISEDRT(GA122plusmn252
-- DAYLIGHT B shy
_ _ _ _ _ _ __E_ _ -- 7 LUNAR IARFAGELM MAJOR EVENTS
122+35 INSERTION 17 124+H7 AGE UPDATE AND ALIGN (R47) 2 122+40 IMU REFSMMAT ALIGN (P52) 1 124+24 CDH THRUSTING (P41) TRAILINGDISPLACEMETIN RI)
3 122+54 AGS UPDATE AND ALIGN (R471 19 124+26 TPI TARGETING IP34 amp AGS) 5 II 20 25 30 4 122+55 CSI TARGETING IP32 amp AGSI 20 124+26-124+51 RR NAVIGATION (P20 18 MARKS) - I I
5 122+54-123+14 RR NAVIGATION (P20 18 MARKS) 21 124+53 AGS UPDATE AND ALIGN (R47)I
6 123+18 COMPUTE CSI BACKUP 22 125+00 COMPUTE TPI BACKUP
7 123+19 AGS UPDATE AND ALIGN (R471 23 125+03 TPI THRUSTING (P411 c
8 123+26 CSI THRUSTING (P411 24 125+05 MCC1 TARGETING IP35) N - M ((25+232
9 123+30 SET W MATRIX 1200025) 25 125+05-125+16 RR NAVIGATION IP20 9 MARKS) 5
2 r INSERT A 10 123+31 CDH TARGETING IP33 amp AGS 26 125+16 COMPUTE MCCI THRUSTING IP41) 5 31 PHAE
11 123+31-123+46 RR NAVIGATION 1P20 14 MARKS) 27 125+18 MCC I THRUSTING (P41)
12 123+47 EXT AV FOR PLANE CHANGE (P20) 28 125+20 MCC2 TARGETING (P351 13 123+54 RCS PLANE CHANGE THRUSTING (P411 29 125+20-125+31 RR NAVIGATION (P20 9 MARKS) 14 123+56 CDH TARGETING (P33 amp AGS) 30 125+31 COMPUTE MCC 2 BACKUP Ideg
15 123+56-124+12 RR NAVIGATION (P20 13 MARKS) 31 125+33 MCC2 THRUSTING [P41)
16 124+15 COMPUTE CDH BACKUP 32 125+48 BRAKING (P47) 27 26TP25+03
33 126+00 STATION KEEPING LT
24
FIGURE 2-1 G MISSION RENDEZVOUS
(CSM-CENTERED RELATIVE MOTION) FOLDOUT FRAME
l D T R2A-e2 TALPFO EDUR ES EPREPAREDBY STEPHENP GRED501I DOUT FRAMW ORBI R B C 0
MISSION G LUNAR ORBIT RENDEZVOUS ATTITUDE TIME HISTORY
OFOR THE LM P33
P20 123+31) (021880)
LMI CSI NrxNMARKS i (123+26+27)
FINAL -
COMP(I123+1l6)
P32 LANDING SITEj P20 30ES (122+50) CSM AT (04650) PRIME MERIDIAN LIFT-OFF
P52 (122+28+11) (122+40)DIRECTION OF (03640)ORBITAL MOTION IS
CLOCKWISE
(18012150)I NERTIAL YAWKLINERTIAL PITCH
ORDEAL PITCH EARTHINERTIAL ROLL
FIGURE 2-2
MISSION G LUNAR ORBIT RENDEZVOUS ATTITUDE TIME HISTORY
FOR THE LM
LM TPF (126+00+00) (01302920)
LM LMC2PLANE CHANGELMPI+30) (123+54+25)
(TPI+30) (0560)(0782400) 7 SUN
P20
(TPI+15) P3
P33(0532480) COMP
---- _ (124+12--- ---
LM TPI (125+02+46) L D (026 627650) (124+24+25)
(0980)
FINAL
DIRECTION OF COMP ORBITAL MOTION IS (124+50)
CLOCKWISE
(18012150)
LL INERTIAL YAW NERTIAL PITCH
ORDEAL PITCH EARTH INERTIAL ROLL
FIGURE 2-3
3-1
30 DISCUSSION OF MAJOR EVENTS
31 Concentric Sequence Initiation
Immediately following Insertion the LM navigated vector will be downlinked to Mission Control Center-Houston this state vector is then uplinked to the CSM The LM commander will perform a Proqram 52 fine alignment to REFSMMAT at approxishymately 12240
The digital autopilot is configured to wide deadband Program P20 is called and an automatic pitch maneuver is initiated to the preferred track attitude At 122 55 CSI targeting parameters are loaded in the PGNS and AGS A period of rendezvous radar marking will then take place from 122-57 to 12315 Upon completion of tracking the LM will obtain an out-of-plane velocity from the CSM to be vectored with the in-plane component of the CSI delta V The CSMs estishymate of out-of-plane velocity is alleged to be better than the LMs estimate (Reference 74)
At approximately 123 20 the LM will voice its CSI solution to the CSM the AGS is updated aligned and targeted in external delta-V with the CDH solution to be excuted Program P41 will then be called and the automatic pitch maneuver bypassed since the burn isto be executed with Z-Axis thrusting The CSI burn occurs nominally at 123 26 27 After verification of the LM CSI burn the CSM will incorporate the LM burn parameters in its CMC LM state vector
32 Constant Delta Height and Plane Change
At 12330 approximately three minutes after the LM CSI burn the W matrix will be set to (200025) and the LM targeting paramters are loaded in both the PGNS and AGS for the CDH maneuver Out-of-plane velocity will then be computed and voiced to the LM from the CSM Program P30 is loaded with the targeting parameters for the LM Plane Change maneuver which will be accomplished in Program P41 30 minutes prior to the CDH maneuver Following the burn the target delta V parameters are voice to the CSM and incorporated into the CMC LM state vector At 12356 the CDH targeting parameters are loaded in both the PGNS and AGS for 1242425 A CDH chart solution is calculated 7 minutes prior to TIG The AGS is updated aligned and targeted in external delta V with the CDH solution to be executed The RCS Thrust Program P41 is called at 12418 and the burn attitude is bypassed since the LM executes CDH by thrusting out individual components of delta V while maintaining radar lock-on
3-2
3 3 Terminal Phase Initiation
Radar tracking is initiated after the CDH maneuver and updating of the LGC continued At 12426 approximately two minutes after the LM CDH burn targeting parameters are loaded in both the PGNS and AGS for the TPI maneuver which will be targeted for a node at intercept Backup measurements are made at the appropriate times The AGS is updated aligned and targeted in external delta V with the TPI solution to be executed The RCS Thrust Program P41 is called at 12456 and the burn attitude is bypassed since the LM is burning along the plus Z-axis with the thrust direction established with the COAS
3 4 Midcourse Corrections
Immediately after TPI the Midcourse Prethrust Program P35 will be called and radar tracking reinitiated Backup measshyurements are made and midcourse corrections chart solutions obtained The MCCl burn will nominally be performed at TPI plus 15 minutes (1251746) If MCCI is to be excuted Program P41 will be called and the burn attitude maneuver is bypassed since the plus Z-axis will remain boresighted at the CSM until docking
Following MCCI Program P35 will be called and targeted for MCC2 at TPI plus 30 minutes (1253246) and executed identishycally to MCCI
3 5 Braking
In preparation for braking the DAP is configured in narrow deadband Program P20 is terminated at 18000 feet but the radar is kept in auto track to provide radar range and range rate displayed on the tapemeter Average G is called by Program P47 prior to braking and attitude hold is selected The braking schedule is followed as contained in Section 4
4-1
40 NOMINAL MISSION PROCEDURES
The procedures included in this section do not specify which crewmember Commander or LM Pilot performs each task These need not be specified since the following basic rules define which crewmember performs each task
41 Commander Tasks
1 All attitude changes whether manual or automatic will be accomplished by the CDR
2 The operation of the DSKY during thrust programs (P40 P41 P42 P47) will be done by the CDR Actual manipulation of the TTCA need not be always done by the CDR but in most cases will be
3 Operation of the rendezvous and landing radar will be done by the CDR
4 The CDR will operate all other systems accessible to only his crew station
42 LM Pilot Tasks
1 AGS operation 2 DSKY operation will be done by the LMP except when keyboard
entries affect the control of spacecraft attitude or thrustshying
3 Backup data logging and chart calculations 4 All logging of maneuver solutions and systems performance 5 The LMP will operate all other systems accessible to only
his crew station
These general rules are guidelines only and may be deviated from by the LM crew if they develop more efficient Task assignments
43 ABBREVIATIONS
The abbreviations used herein are consistant with those in the AOH However in order to condense and simplify the procedures so that they are representative of onboard data a number of addshyitional shorthand conventions have been used To allow the unshyfamiliar reader to understand the procedures contained in this section the following explanations are included
1 AGS - A single asterisk is employed to denote those procedures involving operations to be performed on the DEDA The three number group following an asterisk specifies DEDA address An Rfollowing the address group indicates the address is to be read out A five digit group behind the Rindicates a nominal or expected display If the three number address group is followed by a plus or minus sign a data load is indicated When a single digit follows the plus addition of four zeros behind this digit is assumed Once used these conventions are easily handled and save considerable space
4-2
2 PGNS - The verb-noun addresses in the PGNS are indicated to the left of the procedures column An F is used to indicate a flashing display or absence of an F a static display To the right of the verb-noun on the same line are the contents of the three data registers If numeric quantities appear the DSKY should be correspondingly made to agree by executing a V21 V22 or V23 and performing a data load The procedure of blanking and loading registers is not included since it is repeated often and is highly familiar to the crews
EXAMPLE F 06 33 125-02 46 TIG OF TPI
Expanded this means Load flashing verb 06 noun 33 with the quantity 125 hours 2 minutes and 46 seconds the time of ignition of the RCS engine TPI maneuver Procedurally this is done by keying verb 25 enter loading +000125 in register 1 +00002 in register 2 and +04600 in register 3
If numberic quantities do not follow the verb-noun it is indicated that a computed or information quantity is being displayed via the DSKY If nominal values are listed for possible comparison they appear in parentheses
EXAMPLE- F 06 42 HA HP V
Expanded this means Flashing verb 06 noun 42 has computed height of apogee in register 1 height of perigee in regshyister 2 and velocity to be gained in register 3
3 TIME - The numbers in the left hand column preceded by a plus or minus indicate event timer time referenced to an event Minus indicates event timer counting down to a future event Periodically this same column contains the nominal mission ground elapsed times in parentheses Asterisks following the event time indicate a time critical event which should be accomplished to the nearest second
4-3
4 4 Nominal PGNS Procedures
ASSUMPTIONS
AFTER INSERTION
1 INSERTION COMPLETE (RESIOUALS NULLED) VERIFY V82E (ORBIT) 3 RNDZ RDR LOCKED ON IN MODE II 4 LGC AT FLASHING VERB 37 5 PROPER INITIAL W MATRIX LOADED IN LGC
GUID CONT-PGNS ATTITUDE MON-PGNS(CDR) RATE ERR MON-CMPTR(LMP) ATTITUDE MON-AGS(LMP) SHFTTRUN-+5 DEG X-POINTER-HI MULT RADAR TEST SW-OFF ENG ARM-OFF X-TRANSL-2JETS DEAD BAND-MIN PGNS MODE CONT-AUTO THROTJET-JET CBPGNS IMU OPR-CLOSE RR MODE-LGC TTCATRANSL-ENABLE(COR)
BAL CPL-ON MODE SEL-AGS
RNGALT MON-RNGRNGRT RATE ERR MON-RNDZ RORICOR) ATT CONT-PULSE(3)
AGS MODE CONT-ATT HOLD ACA4JET-DISABLE(CDRJ TTCATRANSL-DISABLE(LMP)
ACA4JET-DISABLE(LMPI
KEY ODE (PO0)
(DOWNLINK LM STATE VECTOR)
KEY V63E (RR SELF TEST)
4-4
F 04 12 00004 00001 PRO
F 16 72 TRUN SHFT PRO
F 16 78 R ROOT VERIFY TAPE METER WITH DSKY
+2 VERIFY INSERTION VELOCITY WITH RNDZ ROR WHERE RANGE = 2642 NM RANGE RATE = -4251 FPS
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
KEY V34E (TERMINATE) KEY V48E (LOAD DAP)
F 01 46 11002 PRO
F 06 47 LMWT CMWT PRO
KEY V56E (KILL AUTO TRACK ENABLE)
+3 KEY V41N72E (COARSE ALIGN RR) F 21 73 +000OOTRUN -077OOSHFT F 04 12 00006 00002 (CONTINUOUS DESIGNATE)
PRO 41 (COARSE ALIGN VERB)
KEY VI6N72E 16 72 MONITOR TRUNSHFT ANGLES
CB PGNS RNDZ RDR-OPEN CB AC BUS A RNDZ RDR-OPEN KEY V44E (TERMINATE RR DESIGNATE)
KEY V83E F 16 54 R ROOT THETA
SET ORDEAL PRO
CS HEATER AOT-CLOSE
CB AOT LAMP-CLOSE
+5 KEY V37E52E (IMU REALIGN)
4-5
410+1 CSI ROUTINE 373+02065 CS TIME 275+03028 TPI TIME
605400777 COTANGENT OF LOS TO-CSM 416+1 (ONE-HALF bRBITAL PERIOD) 411+0 RCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT 310R TIME TO CS
267R VELOCITY TO BE GAINED CSI
402R DELTA H
371R DELTA V CDH
372R _ DELTA T CSICDH
F 04 06 00001 00003 -(REFSMMAT) PRO -
F 50 25 00015 SELECT 1ST STAR ENTR
F 01 70 O02DE LOAD 1ST STAR PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FOAl ANGLES (AUTO MNVRI)
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVR)
F 01 71 002DE
KEY V76E PGNS MODE CONT-ATT HOLD
PRO +10 F 54 71 MARK 1ST STAR
PRO F 01 70 O02DE LOAD 2ND STAR
PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FDA ANGLES -(AUTO MNVRV
F 50 18 FDAI ANGLES (REQUEST PNVRt ENTR (BYPASS MNVR
F 01 71 002DE PGNS MODE CONT-ATT HOLD PRO
-35
4-6
+14 F 54 71 MARK 2ND STAR PRO
F 06 05 STAR ANGLE DIFFERENCE PRO
F 06 93 GYRO TORQUE ANGLES PRO
F 50 25 00014
PRO (CHECK ALIGNMENT IF TIME WILL PERMIT)
F 50 25 00015 SELECT 3RD STAR ENTR
F 01 70 OO2DE LOAD 3RD STAR PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FDAI ANGLES (AUTO MNVR)
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVR)
VERIFY ALIGNMENT VIA AOT
KEY V34E (TERMINATE) F 37 BB
V48E (LOAD DAP) F 01 46 11012
PRO F 06 47 LMWT CMWT
+17 PRO
CB AOT LAMP-OPEN
RESET ET (310R)
(12253) CB AC BUS A RNDZ RDR-CLOSE (WAIT 30 SEC) CB PGNS RNDZ RDR-CLOSE
RR MODE-LGC KEY V37E20E (ACQUIRE RADAR)
PGNS MODE CONT-AUTO F 50 18 FDA ANGLES (REQUEST MNVRJ
PRO (AUTO MNVR) 06 18 FDAI ANGLES (AUTO MNVR)
AGS MODE CONT-AUTO RATEERR MON-CMPTR (LMP)
F 50 18 FDAI ANGLES (REQUEST MNVR)
4-7
ENTR (BYPASS MNVR) NO TRK LT-OFF
F 50 72 RR TRUNSHFT VERIFY RR LOCK ON PRO
DSKY BLANKS
KEY V93E (BEFORE 1ST MARK REINIT W MATRIXI KEY V80E (UPDATE LM SV)
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (i20OOZOO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
400+3 AGS ALIGNshy400R (00000 COMPLETE) 507+0 Z-AXIS BORESIGHT 400+2 ACQUISITION STEERING
CS
(122amp55) KEY V37E32E (CSI)
F 06 11 1 S LOAD TIG CSI FROM DATA PAD (NOM 123S26- 271 PRO
F 06 55 +O000IN +02660E +13000 OMEGAT (CDH 180 DEG AFTER CSI PRO
F 06 37 LOAD TIG TPI FROM DATA PAD (NOM 1251021761 PRO
F 16 45 MKS TFI -00001
-30 COPY RDOT FOR 1ST CSI BU
31OR TIME TO CSI
267R VELOCITY TO BE GAINED CSI
402R DELTA H
371R DELTA V CDH
-22
4-8
372R _ DELTA T CSICDH
KEY V32E (MARKS=5
F 06 75 DELTA H DELTA T CSICDH DELTA T CDHTPI PRO
F 06 81 DELTA VOS-LV (CS) (NOM 501 DELTA VX)
CSI(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (CDH)
(NOM 60 DELTA VX) CDH(82)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
KEY V32E (MARKS=1C)
F 06 75 DELTA H DELTA TCSICDH DELTA TCDHTPI PRD
F 06 81 DELTA VS-LV (CSI) CSI(N811
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 82 DELTA VIS-LV(CDH)
CDH(82)
DELTA VX(LVI
DELTA VY(LV)
DELTA VZ(LV)
-12
4-9
-20 COPY RDOT FOR 2ND CSI BU
F 16 45
F 06 75
F 06 81
F 06 16
F 06 90
PRO MKS TFI -00001
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS NON SEL - PRPLNT A + B TEMP IND 40DEG TO lOODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + 8 PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4v 2 3 (120 - 190 DEG F
(LOS OF MSFN ) S-BAND - SLEW TO P = +90 Y a 0 S-BAND - FWD (OR AFT) S-BAND - DN VOICE BU BIOMED OFF
PRO (FINAL COMP)
267R - VELOCITY TO BE GAINED CSI
402R DELTA H
372R TIME CSICDHL
371R PREDICTED VEL TO BE GAINED CDH
263R OUT-OF-PLANE
DELTA H DELTA TCSICDH DELTA TCDHTPI PRO DELTA VS-LV (CSI)
KEY V9OE (OUT-OF-PLANED
0 LOAD TIG CSI FROM DATA PAD (NOM 12302627) PRO Y YDOT PSI
N90 CSM
YDOT
PRO
-7
4-10
F 06 81 DELTA VS-LV(CSI)
COPY YDOT FROM CSM AND LOAD NEGATIVE IN R2 CSIIN81I
DELTA VX(LV)
DELTA VYILV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (COH)
CDH(82)
DELTA VX(LV)
- DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RANGE AND RDOT FOR 3RD CS BU
COMPUTE CSI BU
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (i2000OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
(TRANSMIT CSI DATA TO CSMI VHF A XMTR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF TELEMETY PCM - LO
KEY VB3E F 16 54 R ROOT THETA
SET ORDEAL PRO
317R RANGE
440R RANGE RATE
4-11
400+3 AGS ALIGN t40OR (00000 COMPLETE)
277R THETA
PRO F 37 BB
-6 KEY 41E (RCS THRUSTING) F 50 18 FDAI-ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTAV 400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTAV 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA RF
TRANSMIT TGT DELTA VS TO CSM AND SYNC COUNTDOWN
16 85 DELTA VS-BODY
502R DELTA VZ (NOM 5Ql)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTAVS-BODY
(123t26t27) BURN +Z
NULL DELTA VS
4-12
VERIFY AGS RESIDUALS 50OR 501R 502R DELTA VX _ DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
CDH
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
KEY V67E (RESET W MATRIX) F 06 99 +0200E +O0020E +00005E
PRO
507+0 Z-AXIS BORESIGHT
(VHF RANGING WITH CSM) VHF A XMTR - VOICERNG VHF B XMTR - OFF VHF B RCVR - ON TELEMETRY PCM - HI
(12331) KEY V37E33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 a TIG CDH (NOM 1242425) -120 amp00 10 (AGS 0 TIME)
(CONVERT TO MINUTES)
411+0 THRUST ALONG Z-BODY AXIS ENTER IF YOU DONT TARGET CSI
373R (NOM 26443 310R TIME TO CDH
4-13
423R DESIRED ALT RATE AT CDH
402R DELTA Hshy
450R DELTA VX
452R DELTA VZ
623+0 Z-AXIS PARALLEL TO CSM PLANE
IPRO F 16 45 MKS TFI -00001
-52 RESET ET
KEY V93E (REINIT W MATRIX WHEN MARKS =4)
KEY V32E (MARKS = 3)
F 06 75 DELTA HCDH DELTA TCDHTPI DELTA TTPI PRO
F 06 81 DELTA VCDH-LV CDH(N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
-47 KEY VSOE (OUT-OF-PLANE)
_ TIG CDH (NOM 124t24t25) -3000 TIME FROM CDH
F 06 16 l1 LOAD TIG PLANE CHANGE (NOM 123amp54-253 PRO
F 06 90 Y YDOT PSI N90 CSM
VYDOT PRO
-42 KEY V32E (MARKS=1O)
F 06 75 DELTA HCDH DELTA TCDIHTPI DELTA TTPITPI PRO
F 06 81 DELTA VCDH-LV
4-14
CDH (NS1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -OO1
KEY V34E (TERMINATE) F 37 B8
PLANE CHANGE
KEY 30E (EXTERNAL DELTA V)
TIG CDH (NOM 124124t25) -3000 TIME FROM CDH
F 06 33 LOAD TIG PLANE CHANGE (NOM 123154T25) PRO
F 06 81 DELTA VS-LV (NOM 00)
-36 COPY RDOT FOR 1ST CDH BU
KEY V90E (OUT-OF-PLANE)
F 06 16 1 1 LOAD TIG PLANE CHANGE (NOM 1231543251 PRO
F 06 90 Y YOOT PSI N90 CSM
YDOT
PRO
F 06 81 DELTA VS-LV(NOM 00)
COPY YDOT AND LOAD NEGATIVE IN R2 PRO
F 06 42 HA HP DELTA V PRO
F 16 45 MKS TFI MGA
PRO
F 37 BB
KEY 41E (RCS THRUSTING)
-30
4-15
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVRI
410+5 EXTERNAL DELTA V 450+0 451-YDOT 452+0 (LOAD CSM -YDOT)
407+0 ROTATE EXTERNAL DELTA V RF
16 95 DELTA VS-BODY
-3035 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATTVHOLD 407+1 FREEZE EXTERNAL DELTAV
F 16 85 DELTA VS-BODY -
NULL DELTA VIS
PRO F 37BB
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
507+0 Z-AXIS BORESIGHT
(12356) KEY 33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 TIG CDH (NOM 124t24t25) -120 OO ZOO (AGS 0 TIME)
(CONVERT TO MINUTES)
373R _ (NOM 2644) 310R TIME TO CDH
423R DESIRED ALT RATE AT CDH
(ADS OF MSFN) S-BAND - SLEW TOP = ACQUIRE HGA LOCK ON VOICE - BUVOICE -- VOICE VERIFY VOICE TLM BIOMED - LEFT (OR RIGHT)
402R DELTAH
4-16
F 16 45
-25
-23
F 06 75
F 06 81
F 16 45
-12
F 06 75
F 06 81
450R DELTA VX
452R DELTA VZ
PRO MKS TFI -00001
KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
COPY ROOT FOR 2ND CDH BU
KEY v32E (MARKS = 5)
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40DEG TO 1OODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + B PRESS IND PSIA
A QUANTITY IND _ PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING a TEMP MON SEL RCS QUAD 1 4 2 3 (120 - 190 DEG F)i
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
CDH(NB1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO MKS TFI -00001
PRO (FINAL COMP)
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
KEY V9OE (OUT-OF-PLANE)
-7
4-17
F 06 16 jj LOAD TIG CDH FROM DATA PAD (NOM 12424251 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT PRO
COPY YOOT FROM CSM AND LOAD NEGATIVE IN R2
CDH(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RDOT FOR 3RD CDH BU
COMPUTE CDH BU
TRANSMIT TGT DELTA VOS TO CSM AND SYNC COUNTDOWN
KEY V47E (INITIALIZE AGS F 06 16 GET OF AGS 0 TIME 120O00OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
KEY V83E F 16 54 R RDOT THETA
SET ORDEAL PRO
317R _ RANGE
440R RANGE RATE 400+3 AGS ALIGN 40OR (00000 COMPLETE)
277R THETA
-6
4-18
PRO F 3 BB
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY V06N86E F 06 86 DELTA VIS-LV
AGS(N86) CHART
DELTA VX(LVD
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
16 85 DELTA VS-BODY
50OR DELTA VX (NOM -0O3)
502R DELTA VZ (NOM 60)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD 407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS BODY
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS 5OOR 50IR 502R DELTA VX -DELTA VY DELTA VZ-
VERIFY PGNS RESIDUALS N85
DELTA VX(LM)
4-19
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
TPI
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO 507+0 Z-AXIS BORESIGHT
(12426) KEY 34E (TPI)
-36 RESET ET
F 06 37 - amp LOAD TIG TPI FROM DATA PAD (NOM 1250246) PRO
F 06 55 +00000 +02660E +13000 OMEGAT PRO
F 16 45 MARKS TFI -00001
-32 KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
-29 KEY V32E (MARKS = 3)
F 06 37 __ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
RESET ET
410+3 TPI SEARCH ROUTINE 307+04300 DELTA T TRANSFER
4-20
-26 310+02600 TFI TPI
303R THETA AT TPI
267R DELTA VTPI
371R DELTA VTPI + DELTA VTPF
KEY V32E (MARKS = 10)
F 06 37 _ _ _ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VIS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
TEMPIPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40ODEG TO IGODEG F A + B PRESS IND 181 +-3 PSIA
TEMPIPRESS MON SEL - HEL
A + B PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD I 4 2 3 (120 - 190 DEG F)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
RESET ET
-13 310+01300 TFI TPI
303R THETA AT TPI
-12 PRO (FINAL COMP) F 06 37 Z TIG TPIj__
4-21
TRANSMIT TIG OF TPI TO CSM-
PRO F 06 58 HP DELTA VTPI DELTA VTRF
PRO F 06 81 DELTA VS-LV
KEY V9OE (OUT-OF-PLANE)
F 06 16 1 LOAD TIG TPI FROM DATA PAD (NOM 12502461 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT
PRO F 06 81 DELTA VS-LV
COPY CSM YDOT AND LOAD NEGATIVE IN R2 N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 59 DELTA VS LOS
N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI MGA
RESET ET
PRO F 37 BB
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (12000t600)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE)
-10
-6
4-22
F 50 16 DOWNLINK COMPLETE PRO (UPDATE COMPLETE)
400+3 AGS ALIGN 400R (00000 COMPLETE)
-9 277R COPY TGT LOS ANGLE
310+00800
303R THETA AT TPI 410+4 DIRECT TRANSFER AT ET=-8 404+0 405+0 406+0 (MONITOR 470 471 4721
373R TIG TPI
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
KEY 41E (RCS THRUSTING) F 50 18 FOAl ANGLES (REQUEST MNVRI
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
-5 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUS
400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
COMPUTE TPI BU
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
4-23
1685 DELTA VS-BODY
50OR DELTA VX(NOM -115)
502R DELTA VZ(NOM 229)
-Z35 OSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS-BODY
(1250246) BURN +Z
VERIFY AGS RESIDUALS 500R 501R 502R DELTAVX DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
MCC1
KEY V76E (PGNS PULSE) PGNSMODECONT-AUTO
KEY V93E (BEFORE 1ST MARK REINITW MATRIX)
+2 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
4-24
(LOS OF MSFN) S-BAND - SLEW TO P = 90 Y = 0 S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
404+0 405+0 406+0
(MONITOR 470 471 4721
+9 277R COPY TGT LOS ANGLE
+12 PRO (COMPUTE MCC FOR TPI+15I F 06 81 DELTA VS-LV
PRO F 06 59 DELTA VS-LOS
PRO F 16 45 MKS TFI MGA
+13 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUOS
COMPUTE MCC1 BU
PRO F 37 BB
+14 KEY 41E (RCS THRUSTING) F 50 18 FOAL ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+1425 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+15 F 16 85 NULL DELTA VS
PRO F 37 BB
MCC2
KEY V76E (PGNS PULSE)
4-25
PGNS MODE CONT-AUTO
KEY V93E (BEFORE 1ST MARK REINIT W MATRIX)
+16 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
404+0 405+0 406+0 (MONITOR 470 471 47)shy
+24 277R COPY TGT LOS ANGLE
+27 PRO (COMPUTE MCC FORTPI+30) F 06 81 DELTA VS-LV
PRO F 06 59 DELIA VPS-LOS
PRO F 16 45 MKS TFI MGA
+28 277R COPY TGT LOS ANGLE
COPY R RDOT FROM TAPEMETER FOR BUS
COMPUTE MCC2 BU
F 37 BB PRO
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+2925 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+30 F 16 85 NULL DELTA VS
PRO F 37 BB
KEY OOE (P001
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
4-26
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT KEY V34E (TERMINATE)
KEY V37E47E (AVE G) F 16 83 DELTA VIS
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT VERIFY TAPE METER WITH DSKY
BRAKING GATE 30 FPS - 6000 FT 20 FPS - 3000 FT 10 FPS - 1500 FT 5 FPS - 600 FT
RENDEZVOUS
STATION KEEPING
5-1
50 ABORT PROCEDURE
This is a specific AGS nominal abort procedure due to a PGNS failure between insertion and station keeping
51
5-2
Nominal AGS Procedures
ASSUMPTIONS
AFTER INSERTION
I INSERTION COMPLETE (RFSIDUALS NULLED) g PGNS FAILURE BEFORE INSERTION 3 RAUAR NOT LOCKED ON
(UI CoNT-AGS ATlI[uUE MON-AGS(CDR) RATE ERR MON-CNPTR(LMP) ATTITUDE MON-AGS(LMP) SHFITRUN-+5 DEG X-POINTER-HI MULT RADAR IEST Sw-OFF LNb GMbL-OFF ENG ARM-OFF X-IRANSL-2 JETS DEAD BAND-MAX PGNS MODE CONT-OFF THROTJET-JET CB IMU OIR-ON HH MOVE-AUTO rRACK TTCATNANSL-ENABLE(CDR)
AL CPL-ON MODE SL-AGS RNGAL1 MON-RNbRNGRT RAIE ERR MON-RNDZ HDR(CDR) AVl CoNT(3)-PULSE AGS MODE CONT-AUTO ACA4JET-DISABLE(CDR) TTCATRANSL-DISABLE(LMP) ACA4JET-DISABLE(LMP)
bO7+U Z-AXIS BOPESIGHT 400+2 Z-AXIS STEERING PULSE TO NULL AGS ERRORS POINT Z-AXIS IN DIRECTION OF CSM MODE CONT-ATT HOLD ATT CONT(3)-MODE CONTROL O unnr - ZirF
5-3
SLEW PATE - LO
SLEW RR ANT TO OqON FUAI VERIFY MAX SIGNAL STRENGTH RH MOOE-AUTO TRACK NO TRACK LIGHT OFF -
ATT CONT(3h-PULSE
CHECK INSERTION VELOCITY WITH TAPEMETER COMPARE EAPEMETER WITH AGS STATE VECTOR DATA I
17R RANGE(NOM 2642)
440R RANGE RATE(NOM -425l)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
cSI
+3 417+1 (RADAR FILTER INITIALIZED) 41b+l (NO BOHESIGHT) b03-XXXXX RANGE RATE
+5 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGF
41b+1 CSI ROUTINE 373+o2065 CSi TIME 275+03028 TPI TIME 605+0077 COTANGENT OF LOS TO CSM 41b+1 (ONE-HALF OFBITAL-PERIOD) 411+0 HCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT
610R TIME TO CST
43 RESET ET
267R VELOCITY TO BE GAINED CSI
402R FLTA H
371R DFLTA V CDH
5-4
372R DFLTA T CSICDH
-42 415+1 (No BORESIGHT) bO6-xXXXX RANGE RATE
-40 415+1 (NO BORESIGHT)503-XXXXX RANGE RATE dORESIGHT ON CSM
415+1 316+XXXXX RANGE
-37 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE
-15 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE UORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-2 415+1 (No BOHESIGHT) bO3-XXXXX RANGF RATE
i1uR TIME TO CS
RESEF ET
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-30 COPY ROOT FOR 1ST CSI 81J
BORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-t7 415+1 (NO BORFSIGHT) 50-XXxXx RANGF RATE
267R VELOCITY TO HE GAINED CSI
402R LELTA H
371R OFLTA V COH
372R OELTA T CSICDH
-5 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 blb+XXXXX RANGE
-i2 415+1 (No BORESIGHT) 5n3-XXXXX RANGE RATE
415+1 (NO BORESIGHT)
5-5
503-XXXXX RANGF RATE
COPY Roor FOR 2NO CSI BU
bORESIGHT ON CSM 415+1 316+XXXXX RANGE
TEMPPRESS MON SEL - FUEL MAN
A AND 8 PRESS 181 +-3 PIG TEMPPRESS MON SEL - PRPLNT
A AND B TEMP IND 4ODEG 0 IOODEG F A AND B PRFSS IND 181 +-3 PSIA
tEMPPRESS MON SEL - HEL
A AND 8 PRESS IND PSIA
A QUANTITY IND- -- PERCENT RFMAINING
8 QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4p 2 3 (120 - 190 DFG F)
415+1 (NO BORESIGHT)-17 503-XXXXX RANGE RATE
-15 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
(LOS OF MSFN) S-BAND - SLEW 10 P = +90t Y U S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
-12 415+1 (No 8ORESIGHT)
503-XXXXX RANGE RATE
267R VFLOCITY TU BE GAINED CSI
402R OFLTA H
372R TIME CSICH
371R PREDICTED VEL 10 RE GAINED COH
263R OLT-OF-PLANE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATL
-10 COPY RANGE AND ROOT FOR 3RD CSI 8U
SORESIGH ON CSM 41b+1
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
Tracking Stations
ANG BDA CRO CYI GYM HSK HTV MAD MER MIL RED TEX VAN
-v-
Antigua Near Space Support Station Bermuda Near Space Support Station Carnarvon Near Space Support Station Canary Near Space Support Station Guaymas Near Space Support Station Honeysuckle Deep Space Support Station Huntsville Near Space Support Station Madrid Deep Space Support Station Mercury Near Space Support Ship MILA Near Space Support Station Redstone Near Space Support Ship Corpus Christi Near Space Support Station Vanguard Near Space Support Ship
10 PURPOSE
This document contains the primary procedures for the LM-5 active rendezvous with CSM-107 spacecraft in accordance with Detailed Test Objective Section 40 defined in Reference 71
The purpose of the LM Rendezvous Procedures document is to provide a single source of procedures information for use in flight planning in crew training and in preparing onboard data
This is a control document subject to review by all elements of the Apollo Program and to approval by the Procedures Conshyfiguration Control Board Comments should be directed to Mr Stephen P Grega Flight Procedures Branch Flight Crew Support Division Extension 5348
Beyond G mission planning no additional techniques and trajectory information specific to Mission H have been made available as of this date Therefore since Missions G and H are expected to be similar in the area of rendezvous guidance and navigation procedures the G mission final LM Rendezvous Procedures Document will serve -as an H mission preliminary LM Rendezvous and Procedures Document After reviewal by all elements of the Apollo Program and approval by the Procedures Configuration Control Board this document will then evolve into the control document for the Mission H crew procedures
2-1
20 INTRODUCTION
The LM-5CSM-l07 lunar orbit rendezvous exercise will beginduring the twenty-fourth CSM revolution with insertion at 122 35255 and end at approximately 1260000 with post rendezvous station keeping The LM procedures during this period are divided into segments of major activities which are discussed in detail in Section 30
A nominal LM-5CSM-107 mission profile is contained in Figshyure (2-1) This figure shows the locations in time and local horizontal position of the most significant nominal mission events Trajectory data used to generate the mission profile and timeline for procedures development was obtained from Reference 72 The rendezvous navigation update schedule assumed in the procedures is defined in Reference 73
A history of the LM body attitudes during the rendezvous accompanies the major events discussion and is also presented in Figures (2-2) and (2-3) Each figure illustrates the bodyattitudes with respect to the moon sun and earth and indicates FDAI roll pitch and yaw gimbal angles and the ordeal pitch angle for significant events during each lunar orbit
0RBI TR EL
TRAILINGDISPLACEMENT(N MI) 0 0 W60 20240 BE
33I I ] I I I
32 ltrMCCE 1125+-3 C CH (124t24) PLAN CHANGE023 TM)2
R~TC(222
40 1146235 A N MNTTIMETKS FROMISEDRT(GA122plusmn252
-- DAYLIGHT B shy
_ _ _ _ _ _ __E_ _ -- 7 LUNAR IARFAGELM MAJOR EVENTS
122+35 INSERTION 17 124+H7 AGE UPDATE AND ALIGN (R47) 2 122+40 IMU REFSMMAT ALIGN (P52) 1 124+24 CDH THRUSTING (P41) TRAILINGDISPLACEMETIN RI)
3 122+54 AGS UPDATE AND ALIGN (R471 19 124+26 TPI TARGETING IP34 amp AGS) 5 II 20 25 30 4 122+55 CSI TARGETING IP32 amp AGSI 20 124+26-124+51 RR NAVIGATION (P20 18 MARKS) - I I
5 122+54-123+14 RR NAVIGATION (P20 18 MARKS) 21 124+53 AGS UPDATE AND ALIGN (R47)I
6 123+18 COMPUTE CSI BACKUP 22 125+00 COMPUTE TPI BACKUP
7 123+19 AGS UPDATE AND ALIGN (R471 23 125+03 TPI THRUSTING (P411 c
8 123+26 CSI THRUSTING (P411 24 125+05 MCC1 TARGETING IP35) N - M ((25+232
9 123+30 SET W MATRIX 1200025) 25 125+05-125+16 RR NAVIGATION IP20 9 MARKS) 5
2 r INSERT A 10 123+31 CDH TARGETING IP33 amp AGS 26 125+16 COMPUTE MCCI THRUSTING IP41) 5 31 PHAE
11 123+31-123+46 RR NAVIGATION 1P20 14 MARKS) 27 125+18 MCC I THRUSTING (P41)
12 123+47 EXT AV FOR PLANE CHANGE (P20) 28 125+20 MCC2 TARGETING (P351 13 123+54 RCS PLANE CHANGE THRUSTING (P411 29 125+20-125+31 RR NAVIGATION (P20 9 MARKS) 14 123+56 CDH TARGETING (P33 amp AGS) 30 125+31 COMPUTE MCC 2 BACKUP Ideg
15 123+56-124+12 RR NAVIGATION (P20 13 MARKS) 31 125+33 MCC2 THRUSTING [P41)
16 124+15 COMPUTE CDH BACKUP 32 125+48 BRAKING (P47) 27 26TP25+03
33 126+00 STATION KEEPING LT
24
FIGURE 2-1 G MISSION RENDEZVOUS
(CSM-CENTERED RELATIVE MOTION) FOLDOUT FRAME
l D T R2A-e2 TALPFO EDUR ES EPREPAREDBY STEPHENP GRED501I DOUT FRAMW ORBI R B C 0
MISSION G LUNAR ORBIT RENDEZVOUS ATTITUDE TIME HISTORY
OFOR THE LM P33
P20 123+31) (021880)
LMI CSI NrxNMARKS i (123+26+27)
FINAL -
COMP(I123+1l6)
P32 LANDING SITEj P20 30ES (122+50) CSM AT (04650) PRIME MERIDIAN LIFT-OFF
P52 (122+28+11) (122+40)DIRECTION OF (03640)ORBITAL MOTION IS
CLOCKWISE
(18012150)I NERTIAL YAWKLINERTIAL PITCH
ORDEAL PITCH EARTHINERTIAL ROLL
FIGURE 2-2
MISSION G LUNAR ORBIT RENDEZVOUS ATTITUDE TIME HISTORY
FOR THE LM
LM TPF (126+00+00) (01302920)
LM LMC2PLANE CHANGELMPI+30) (123+54+25)
(TPI+30) (0560)(0782400) 7 SUN
P20
(TPI+15) P3
P33(0532480) COMP
---- _ (124+12--- ---
LM TPI (125+02+46) L D (026 627650) (124+24+25)
(0980)
FINAL
DIRECTION OF COMP ORBITAL MOTION IS (124+50)
CLOCKWISE
(18012150)
LL INERTIAL YAW NERTIAL PITCH
ORDEAL PITCH EARTH INERTIAL ROLL
FIGURE 2-3
3-1
30 DISCUSSION OF MAJOR EVENTS
31 Concentric Sequence Initiation
Immediately following Insertion the LM navigated vector will be downlinked to Mission Control Center-Houston this state vector is then uplinked to the CSM The LM commander will perform a Proqram 52 fine alignment to REFSMMAT at approxishymately 12240
The digital autopilot is configured to wide deadband Program P20 is called and an automatic pitch maneuver is initiated to the preferred track attitude At 122 55 CSI targeting parameters are loaded in the PGNS and AGS A period of rendezvous radar marking will then take place from 122-57 to 12315 Upon completion of tracking the LM will obtain an out-of-plane velocity from the CSM to be vectored with the in-plane component of the CSI delta V The CSMs estishymate of out-of-plane velocity is alleged to be better than the LMs estimate (Reference 74)
At approximately 123 20 the LM will voice its CSI solution to the CSM the AGS is updated aligned and targeted in external delta-V with the CDH solution to be excuted Program P41 will then be called and the automatic pitch maneuver bypassed since the burn isto be executed with Z-Axis thrusting The CSI burn occurs nominally at 123 26 27 After verification of the LM CSI burn the CSM will incorporate the LM burn parameters in its CMC LM state vector
32 Constant Delta Height and Plane Change
At 12330 approximately three minutes after the LM CSI burn the W matrix will be set to (200025) and the LM targeting paramters are loaded in both the PGNS and AGS for the CDH maneuver Out-of-plane velocity will then be computed and voiced to the LM from the CSM Program P30 is loaded with the targeting parameters for the LM Plane Change maneuver which will be accomplished in Program P41 30 minutes prior to the CDH maneuver Following the burn the target delta V parameters are voice to the CSM and incorporated into the CMC LM state vector At 12356 the CDH targeting parameters are loaded in both the PGNS and AGS for 1242425 A CDH chart solution is calculated 7 minutes prior to TIG The AGS is updated aligned and targeted in external delta V with the CDH solution to be executed The RCS Thrust Program P41 is called at 12418 and the burn attitude is bypassed since the LM executes CDH by thrusting out individual components of delta V while maintaining radar lock-on
3-2
3 3 Terminal Phase Initiation
Radar tracking is initiated after the CDH maneuver and updating of the LGC continued At 12426 approximately two minutes after the LM CDH burn targeting parameters are loaded in both the PGNS and AGS for the TPI maneuver which will be targeted for a node at intercept Backup measurements are made at the appropriate times The AGS is updated aligned and targeted in external delta V with the TPI solution to be executed The RCS Thrust Program P41 is called at 12456 and the burn attitude is bypassed since the LM is burning along the plus Z-axis with the thrust direction established with the COAS
3 4 Midcourse Corrections
Immediately after TPI the Midcourse Prethrust Program P35 will be called and radar tracking reinitiated Backup measshyurements are made and midcourse corrections chart solutions obtained The MCCl burn will nominally be performed at TPI plus 15 minutes (1251746) If MCCI is to be excuted Program P41 will be called and the burn attitude maneuver is bypassed since the plus Z-axis will remain boresighted at the CSM until docking
Following MCCI Program P35 will be called and targeted for MCC2 at TPI plus 30 minutes (1253246) and executed identishycally to MCCI
3 5 Braking
In preparation for braking the DAP is configured in narrow deadband Program P20 is terminated at 18000 feet but the radar is kept in auto track to provide radar range and range rate displayed on the tapemeter Average G is called by Program P47 prior to braking and attitude hold is selected The braking schedule is followed as contained in Section 4
4-1
40 NOMINAL MISSION PROCEDURES
The procedures included in this section do not specify which crewmember Commander or LM Pilot performs each task These need not be specified since the following basic rules define which crewmember performs each task
41 Commander Tasks
1 All attitude changes whether manual or automatic will be accomplished by the CDR
2 The operation of the DSKY during thrust programs (P40 P41 P42 P47) will be done by the CDR Actual manipulation of the TTCA need not be always done by the CDR but in most cases will be
3 Operation of the rendezvous and landing radar will be done by the CDR
4 The CDR will operate all other systems accessible to only his crew station
42 LM Pilot Tasks
1 AGS operation 2 DSKY operation will be done by the LMP except when keyboard
entries affect the control of spacecraft attitude or thrustshying
3 Backup data logging and chart calculations 4 All logging of maneuver solutions and systems performance 5 The LMP will operate all other systems accessible to only
his crew station
These general rules are guidelines only and may be deviated from by the LM crew if they develop more efficient Task assignments
43 ABBREVIATIONS
The abbreviations used herein are consistant with those in the AOH However in order to condense and simplify the procedures so that they are representative of onboard data a number of addshyitional shorthand conventions have been used To allow the unshyfamiliar reader to understand the procedures contained in this section the following explanations are included
1 AGS - A single asterisk is employed to denote those procedures involving operations to be performed on the DEDA The three number group following an asterisk specifies DEDA address An Rfollowing the address group indicates the address is to be read out A five digit group behind the Rindicates a nominal or expected display If the three number address group is followed by a plus or minus sign a data load is indicated When a single digit follows the plus addition of four zeros behind this digit is assumed Once used these conventions are easily handled and save considerable space
4-2
2 PGNS - The verb-noun addresses in the PGNS are indicated to the left of the procedures column An F is used to indicate a flashing display or absence of an F a static display To the right of the verb-noun on the same line are the contents of the three data registers If numeric quantities appear the DSKY should be correspondingly made to agree by executing a V21 V22 or V23 and performing a data load The procedure of blanking and loading registers is not included since it is repeated often and is highly familiar to the crews
EXAMPLE F 06 33 125-02 46 TIG OF TPI
Expanded this means Load flashing verb 06 noun 33 with the quantity 125 hours 2 minutes and 46 seconds the time of ignition of the RCS engine TPI maneuver Procedurally this is done by keying verb 25 enter loading +000125 in register 1 +00002 in register 2 and +04600 in register 3
If numberic quantities do not follow the verb-noun it is indicated that a computed or information quantity is being displayed via the DSKY If nominal values are listed for possible comparison they appear in parentheses
EXAMPLE- F 06 42 HA HP V
Expanded this means Flashing verb 06 noun 42 has computed height of apogee in register 1 height of perigee in regshyister 2 and velocity to be gained in register 3
3 TIME - The numbers in the left hand column preceded by a plus or minus indicate event timer time referenced to an event Minus indicates event timer counting down to a future event Periodically this same column contains the nominal mission ground elapsed times in parentheses Asterisks following the event time indicate a time critical event which should be accomplished to the nearest second
4-3
4 4 Nominal PGNS Procedures
ASSUMPTIONS
AFTER INSERTION
1 INSERTION COMPLETE (RESIOUALS NULLED) VERIFY V82E (ORBIT) 3 RNDZ RDR LOCKED ON IN MODE II 4 LGC AT FLASHING VERB 37 5 PROPER INITIAL W MATRIX LOADED IN LGC
GUID CONT-PGNS ATTITUDE MON-PGNS(CDR) RATE ERR MON-CMPTR(LMP) ATTITUDE MON-AGS(LMP) SHFTTRUN-+5 DEG X-POINTER-HI MULT RADAR TEST SW-OFF ENG ARM-OFF X-TRANSL-2JETS DEAD BAND-MIN PGNS MODE CONT-AUTO THROTJET-JET CBPGNS IMU OPR-CLOSE RR MODE-LGC TTCATRANSL-ENABLE(COR)
BAL CPL-ON MODE SEL-AGS
RNGALT MON-RNGRNGRT RATE ERR MON-RNDZ RORICOR) ATT CONT-PULSE(3)
AGS MODE CONT-ATT HOLD ACA4JET-DISABLE(CDRJ TTCATRANSL-DISABLE(LMP)
ACA4JET-DISABLE(LMPI
KEY ODE (PO0)
(DOWNLINK LM STATE VECTOR)
KEY V63E (RR SELF TEST)
4-4
F 04 12 00004 00001 PRO
F 16 72 TRUN SHFT PRO
F 16 78 R ROOT VERIFY TAPE METER WITH DSKY
+2 VERIFY INSERTION VELOCITY WITH RNDZ ROR WHERE RANGE = 2642 NM RANGE RATE = -4251 FPS
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
KEY V34E (TERMINATE) KEY V48E (LOAD DAP)
F 01 46 11002 PRO
F 06 47 LMWT CMWT PRO
KEY V56E (KILL AUTO TRACK ENABLE)
+3 KEY V41N72E (COARSE ALIGN RR) F 21 73 +000OOTRUN -077OOSHFT F 04 12 00006 00002 (CONTINUOUS DESIGNATE)
PRO 41 (COARSE ALIGN VERB)
KEY VI6N72E 16 72 MONITOR TRUNSHFT ANGLES
CB PGNS RNDZ RDR-OPEN CB AC BUS A RNDZ RDR-OPEN KEY V44E (TERMINATE RR DESIGNATE)
KEY V83E F 16 54 R ROOT THETA
SET ORDEAL PRO
CS HEATER AOT-CLOSE
CB AOT LAMP-CLOSE
+5 KEY V37E52E (IMU REALIGN)
4-5
410+1 CSI ROUTINE 373+02065 CS TIME 275+03028 TPI TIME
605400777 COTANGENT OF LOS TO-CSM 416+1 (ONE-HALF bRBITAL PERIOD) 411+0 RCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT 310R TIME TO CS
267R VELOCITY TO BE GAINED CSI
402R DELTA H
371R DELTA V CDH
372R _ DELTA T CSICDH
F 04 06 00001 00003 -(REFSMMAT) PRO -
F 50 25 00015 SELECT 1ST STAR ENTR
F 01 70 O02DE LOAD 1ST STAR PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FOAl ANGLES (AUTO MNVRI)
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVR)
F 01 71 002DE
KEY V76E PGNS MODE CONT-ATT HOLD
PRO +10 F 54 71 MARK 1ST STAR
PRO F 01 70 O02DE LOAD 2ND STAR
PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FDA ANGLES -(AUTO MNVRV
F 50 18 FDAI ANGLES (REQUEST PNVRt ENTR (BYPASS MNVR
F 01 71 002DE PGNS MODE CONT-ATT HOLD PRO
-35
4-6
+14 F 54 71 MARK 2ND STAR PRO
F 06 05 STAR ANGLE DIFFERENCE PRO
F 06 93 GYRO TORQUE ANGLES PRO
F 50 25 00014
PRO (CHECK ALIGNMENT IF TIME WILL PERMIT)
F 50 25 00015 SELECT 3RD STAR ENTR
F 01 70 OO2DE LOAD 3RD STAR PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FDAI ANGLES (AUTO MNVR)
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVR)
VERIFY ALIGNMENT VIA AOT
KEY V34E (TERMINATE) F 37 BB
V48E (LOAD DAP) F 01 46 11012
PRO F 06 47 LMWT CMWT
+17 PRO
CB AOT LAMP-OPEN
RESET ET (310R)
(12253) CB AC BUS A RNDZ RDR-CLOSE (WAIT 30 SEC) CB PGNS RNDZ RDR-CLOSE
RR MODE-LGC KEY V37E20E (ACQUIRE RADAR)
PGNS MODE CONT-AUTO F 50 18 FDA ANGLES (REQUEST MNVRJ
PRO (AUTO MNVR) 06 18 FDAI ANGLES (AUTO MNVR)
AGS MODE CONT-AUTO RATEERR MON-CMPTR (LMP)
F 50 18 FDAI ANGLES (REQUEST MNVR)
4-7
ENTR (BYPASS MNVR) NO TRK LT-OFF
F 50 72 RR TRUNSHFT VERIFY RR LOCK ON PRO
DSKY BLANKS
KEY V93E (BEFORE 1ST MARK REINIT W MATRIXI KEY V80E (UPDATE LM SV)
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (i20OOZOO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
400+3 AGS ALIGNshy400R (00000 COMPLETE) 507+0 Z-AXIS BORESIGHT 400+2 ACQUISITION STEERING
CS
(122amp55) KEY V37E32E (CSI)
F 06 11 1 S LOAD TIG CSI FROM DATA PAD (NOM 123S26- 271 PRO
F 06 55 +O000IN +02660E +13000 OMEGAT (CDH 180 DEG AFTER CSI PRO
F 06 37 LOAD TIG TPI FROM DATA PAD (NOM 1251021761 PRO
F 16 45 MKS TFI -00001
-30 COPY RDOT FOR 1ST CSI BU
31OR TIME TO CSI
267R VELOCITY TO BE GAINED CSI
402R DELTA H
371R DELTA V CDH
-22
4-8
372R _ DELTA T CSICDH
KEY V32E (MARKS=5
F 06 75 DELTA H DELTA T CSICDH DELTA T CDHTPI PRO
F 06 81 DELTA VOS-LV (CS) (NOM 501 DELTA VX)
CSI(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (CDH)
(NOM 60 DELTA VX) CDH(82)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
KEY V32E (MARKS=1C)
F 06 75 DELTA H DELTA TCSICDH DELTA TCDHTPI PRD
F 06 81 DELTA VS-LV (CSI) CSI(N811
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 82 DELTA VIS-LV(CDH)
CDH(82)
DELTA VX(LVI
DELTA VY(LV)
DELTA VZ(LV)
-12
4-9
-20 COPY RDOT FOR 2ND CSI BU
F 16 45
F 06 75
F 06 81
F 06 16
F 06 90
PRO MKS TFI -00001
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS NON SEL - PRPLNT A + B TEMP IND 40DEG TO lOODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + 8 PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4v 2 3 (120 - 190 DEG F
(LOS OF MSFN ) S-BAND - SLEW TO P = +90 Y a 0 S-BAND - FWD (OR AFT) S-BAND - DN VOICE BU BIOMED OFF
PRO (FINAL COMP)
267R - VELOCITY TO BE GAINED CSI
402R DELTA H
372R TIME CSICDHL
371R PREDICTED VEL TO BE GAINED CDH
263R OUT-OF-PLANE
DELTA H DELTA TCSICDH DELTA TCDHTPI PRO DELTA VS-LV (CSI)
KEY V9OE (OUT-OF-PLANED
0 LOAD TIG CSI FROM DATA PAD (NOM 12302627) PRO Y YDOT PSI
N90 CSM
YDOT
PRO
-7
4-10
F 06 81 DELTA VS-LV(CSI)
COPY YDOT FROM CSM AND LOAD NEGATIVE IN R2 CSIIN81I
DELTA VX(LV)
DELTA VYILV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (COH)
CDH(82)
DELTA VX(LV)
- DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RANGE AND RDOT FOR 3RD CS BU
COMPUTE CSI BU
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (i2000OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
(TRANSMIT CSI DATA TO CSMI VHF A XMTR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF TELEMETY PCM - LO
KEY VB3E F 16 54 R ROOT THETA
SET ORDEAL PRO
317R RANGE
440R RANGE RATE
4-11
400+3 AGS ALIGN t40OR (00000 COMPLETE)
277R THETA
PRO F 37 BB
-6 KEY 41E (RCS THRUSTING) F 50 18 FDAI-ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTAV 400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTAV 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA RF
TRANSMIT TGT DELTA VS TO CSM AND SYNC COUNTDOWN
16 85 DELTA VS-BODY
502R DELTA VZ (NOM 5Ql)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTAVS-BODY
(123t26t27) BURN +Z
NULL DELTA VS
4-12
VERIFY AGS RESIDUALS 50OR 501R 502R DELTA VX _ DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
CDH
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
KEY V67E (RESET W MATRIX) F 06 99 +0200E +O0020E +00005E
PRO
507+0 Z-AXIS BORESIGHT
(VHF RANGING WITH CSM) VHF A XMTR - VOICERNG VHF B XMTR - OFF VHF B RCVR - ON TELEMETRY PCM - HI
(12331) KEY V37E33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 a TIG CDH (NOM 1242425) -120 amp00 10 (AGS 0 TIME)
(CONVERT TO MINUTES)
411+0 THRUST ALONG Z-BODY AXIS ENTER IF YOU DONT TARGET CSI
373R (NOM 26443 310R TIME TO CDH
4-13
423R DESIRED ALT RATE AT CDH
402R DELTA Hshy
450R DELTA VX
452R DELTA VZ
623+0 Z-AXIS PARALLEL TO CSM PLANE
IPRO F 16 45 MKS TFI -00001
-52 RESET ET
KEY V93E (REINIT W MATRIX WHEN MARKS =4)
KEY V32E (MARKS = 3)
F 06 75 DELTA HCDH DELTA TCDHTPI DELTA TTPI PRO
F 06 81 DELTA VCDH-LV CDH(N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
-47 KEY VSOE (OUT-OF-PLANE)
_ TIG CDH (NOM 124t24t25) -3000 TIME FROM CDH
F 06 16 l1 LOAD TIG PLANE CHANGE (NOM 123amp54-253 PRO
F 06 90 Y YDOT PSI N90 CSM
VYDOT PRO
-42 KEY V32E (MARKS=1O)
F 06 75 DELTA HCDH DELTA TCDIHTPI DELTA TTPITPI PRO
F 06 81 DELTA VCDH-LV
4-14
CDH (NS1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -OO1
KEY V34E (TERMINATE) F 37 B8
PLANE CHANGE
KEY 30E (EXTERNAL DELTA V)
TIG CDH (NOM 124124t25) -3000 TIME FROM CDH
F 06 33 LOAD TIG PLANE CHANGE (NOM 123154T25) PRO
F 06 81 DELTA VS-LV (NOM 00)
-36 COPY RDOT FOR 1ST CDH BU
KEY V90E (OUT-OF-PLANE)
F 06 16 1 1 LOAD TIG PLANE CHANGE (NOM 1231543251 PRO
F 06 90 Y YOOT PSI N90 CSM
YDOT
PRO
F 06 81 DELTA VS-LV(NOM 00)
COPY YDOT AND LOAD NEGATIVE IN R2 PRO
F 06 42 HA HP DELTA V PRO
F 16 45 MKS TFI MGA
PRO
F 37 BB
KEY 41E (RCS THRUSTING)
-30
4-15
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVRI
410+5 EXTERNAL DELTA V 450+0 451-YDOT 452+0 (LOAD CSM -YDOT)
407+0 ROTATE EXTERNAL DELTA V RF
16 95 DELTA VS-BODY
-3035 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATTVHOLD 407+1 FREEZE EXTERNAL DELTAV
F 16 85 DELTA VS-BODY -
NULL DELTA VIS
PRO F 37BB
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
507+0 Z-AXIS BORESIGHT
(12356) KEY 33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 TIG CDH (NOM 124t24t25) -120 OO ZOO (AGS 0 TIME)
(CONVERT TO MINUTES)
373R _ (NOM 2644) 310R TIME TO CDH
423R DESIRED ALT RATE AT CDH
(ADS OF MSFN) S-BAND - SLEW TOP = ACQUIRE HGA LOCK ON VOICE - BUVOICE -- VOICE VERIFY VOICE TLM BIOMED - LEFT (OR RIGHT)
402R DELTAH
4-16
F 16 45
-25
-23
F 06 75
F 06 81
F 16 45
-12
F 06 75
F 06 81
450R DELTA VX
452R DELTA VZ
PRO MKS TFI -00001
KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
COPY ROOT FOR 2ND CDH BU
KEY v32E (MARKS = 5)
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40DEG TO 1OODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + B PRESS IND PSIA
A QUANTITY IND _ PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING a TEMP MON SEL RCS QUAD 1 4 2 3 (120 - 190 DEG F)i
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
CDH(NB1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO MKS TFI -00001
PRO (FINAL COMP)
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
KEY V9OE (OUT-OF-PLANE)
-7
4-17
F 06 16 jj LOAD TIG CDH FROM DATA PAD (NOM 12424251 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT PRO
COPY YOOT FROM CSM AND LOAD NEGATIVE IN R2
CDH(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RDOT FOR 3RD CDH BU
COMPUTE CDH BU
TRANSMIT TGT DELTA VOS TO CSM AND SYNC COUNTDOWN
KEY V47E (INITIALIZE AGS F 06 16 GET OF AGS 0 TIME 120O00OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
KEY V83E F 16 54 R RDOT THETA
SET ORDEAL PRO
317R _ RANGE
440R RANGE RATE 400+3 AGS ALIGN 40OR (00000 COMPLETE)
277R THETA
-6
4-18
PRO F 3 BB
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY V06N86E F 06 86 DELTA VIS-LV
AGS(N86) CHART
DELTA VX(LVD
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
16 85 DELTA VS-BODY
50OR DELTA VX (NOM -0O3)
502R DELTA VZ (NOM 60)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD 407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS BODY
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS 5OOR 50IR 502R DELTA VX -DELTA VY DELTA VZ-
VERIFY PGNS RESIDUALS N85
DELTA VX(LM)
4-19
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
TPI
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO 507+0 Z-AXIS BORESIGHT
(12426) KEY 34E (TPI)
-36 RESET ET
F 06 37 - amp LOAD TIG TPI FROM DATA PAD (NOM 1250246) PRO
F 06 55 +00000 +02660E +13000 OMEGAT PRO
F 16 45 MARKS TFI -00001
-32 KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
-29 KEY V32E (MARKS = 3)
F 06 37 __ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
RESET ET
410+3 TPI SEARCH ROUTINE 307+04300 DELTA T TRANSFER
4-20
-26 310+02600 TFI TPI
303R THETA AT TPI
267R DELTA VTPI
371R DELTA VTPI + DELTA VTPF
KEY V32E (MARKS = 10)
F 06 37 _ _ _ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VIS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
TEMPIPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40ODEG TO IGODEG F A + B PRESS IND 181 +-3 PSIA
TEMPIPRESS MON SEL - HEL
A + B PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD I 4 2 3 (120 - 190 DEG F)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
RESET ET
-13 310+01300 TFI TPI
303R THETA AT TPI
-12 PRO (FINAL COMP) F 06 37 Z TIG TPIj__
4-21
TRANSMIT TIG OF TPI TO CSM-
PRO F 06 58 HP DELTA VTPI DELTA VTRF
PRO F 06 81 DELTA VS-LV
KEY V9OE (OUT-OF-PLANE)
F 06 16 1 LOAD TIG TPI FROM DATA PAD (NOM 12502461 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT
PRO F 06 81 DELTA VS-LV
COPY CSM YDOT AND LOAD NEGATIVE IN R2 N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 59 DELTA VS LOS
N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI MGA
RESET ET
PRO F 37 BB
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (12000t600)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE)
-10
-6
4-22
F 50 16 DOWNLINK COMPLETE PRO (UPDATE COMPLETE)
400+3 AGS ALIGN 400R (00000 COMPLETE)
-9 277R COPY TGT LOS ANGLE
310+00800
303R THETA AT TPI 410+4 DIRECT TRANSFER AT ET=-8 404+0 405+0 406+0 (MONITOR 470 471 4721
373R TIG TPI
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
KEY 41E (RCS THRUSTING) F 50 18 FOAl ANGLES (REQUEST MNVRI
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
-5 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUS
400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
COMPUTE TPI BU
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
4-23
1685 DELTA VS-BODY
50OR DELTA VX(NOM -115)
502R DELTA VZ(NOM 229)
-Z35 OSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS-BODY
(1250246) BURN +Z
VERIFY AGS RESIDUALS 500R 501R 502R DELTAVX DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
MCC1
KEY V76E (PGNS PULSE) PGNSMODECONT-AUTO
KEY V93E (BEFORE 1ST MARK REINITW MATRIX)
+2 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
4-24
(LOS OF MSFN) S-BAND - SLEW TO P = 90 Y = 0 S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
404+0 405+0 406+0
(MONITOR 470 471 4721
+9 277R COPY TGT LOS ANGLE
+12 PRO (COMPUTE MCC FOR TPI+15I F 06 81 DELTA VS-LV
PRO F 06 59 DELTA VS-LOS
PRO F 16 45 MKS TFI MGA
+13 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUOS
COMPUTE MCC1 BU
PRO F 37 BB
+14 KEY 41E (RCS THRUSTING) F 50 18 FOAL ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+1425 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+15 F 16 85 NULL DELTA VS
PRO F 37 BB
MCC2
KEY V76E (PGNS PULSE)
4-25
PGNS MODE CONT-AUTO
KEY V93E (BEFORE 1ST MARK REINIT W MATRIX)
+16 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
404+0 405+0 406+0 (MONITOR 470 471 47)shy
+24 277R COPY TGT LOS ANGLE
+27 PRO (COMPUTE MCC FORTPI+30) F 06 81 DELTA VS-LV
PRO F 06 59 DELIA VPS-LOS
PRO F 16 45 MKS TFI MGA
+28 277R COPY TGT LOS ANGLE
COPY R RDOT FROM TAPEMETER FOR BUS
COMPUTE MCC2 BU
F 37 BB PRO
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+2925 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+30 F 16 85 NULL DELTA VS
PRO F 37 BB
KEY OOE (P001
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
4-26
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT KEY V34E (TERMINATE)
KEY V37E47E (AVE G) F 16 83 DELTA VIS
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT VERIFY TAPE METER WITH DSKY
BRAKING GATE 30 FPS - 6000 FT 20 FPS - 3000 FT 10 FPS - 1500 FT 5 FPS - 600 FT
RENDEZVOUS
STATION KEEPING
5-1
50 ABORT PROCEDURE
This is a specific AGS nominal abort procedure due to a PGNS failure between insertion and station keeping
51
5-2
Nominal AGS Procedures
ASSUMPTIONS
AFTER INSERTION
I INSERTION COMPLETE (RFSIDUALS NULLED) g PGNS FAILURE BEFORE INSERTION 3 RAUAR NOT LOCKED ON
(UI CoNT-AGS ATlI[uUE MON-AGS(CDR) RATE ERR MON-CNPTR(LMP) ATTITUDE MON-AGS(LMP) SHFITRUN-+5 DEG X-POINTER-HI MULT RADAR IEST Sw-OFF LNb GMbL-OFF ENG ARM-OFF X-IRANSL-2 JETS DEAD BAND-MAX PGNS MODE CONT-OFF THROTJET-JET CB IMU OIR-ON HH MOVE-AUTO rRACK TTCATNANSL-ENABLE(CDR)
AL CPL-ON MODE SL-AGS RNGAL1 MON-RNbRNGRT RAIE ERR MON-RNDZ HDR(CDR) AVl CoNT(3)-PULSE AGS MODE CONT-AUTO ACA4JET-DISABLE(CDR) TTCATRANSL-DISABLE(LMP) ACA4JET-DISABLE(LMP)
bO7+U Z-AXIS BOPESIGHT 400+2 Z-AXIS STEERING PULSE TO NULL AGS ERRORS POINT Z-AXIS IN DIRECTION OF CSM MODE CONT-ATT HOLD ATT CONT(3)-MODE CONTROL O unnr - ZirF
5-3
SLEW PATE - LO
SLEW RR ANT TO OqON FUAI VERIFY MAX SIGNAL STRENGTH RH MOOE-AUTO TRACK NO TRACK LIGHT OFF -
ATT CONT(3h-PULSE
CHECK INSERTION VELOCITY WITH TAPEMETER COMPARE EAPEMETER WITH AGS STATE VECTOR DATA I
17R RANGE(NOM 2642)
440R RANGE RATE(NOM -425l)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
cSI
+3 417+1 (RADAR FILTER INITIALIZED) 41b+l (NO BOHESIGHT) b03-XXXXX RANGE RATE
+5 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGF
41b+1 CSI ROUTINE 373+o2065 CSi TIME 275+03028 TPI TIME 605+0077 COTANGENT OF LOS TO CSM 41b+1 (ONE-HALF OFBITAL-PERIOD) 411+0 HCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT
610R TIME TO CST
43 RESET ET
267R VELOCITY TO BE GAINED CSI
402R FLTA H
371R DFLTA V CDH
5-4
372R DFLTA T CSICDH
-42 415+1 (No BORESIGHT) bO6-xXXXX RANGE RATE
-40 415+1 (NO BORESIGHT)503-XXXXX RANGE RATE dORESIGHT ON CSM
415+1 316+XXXXX RANGE
-37 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE
-15 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE UORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-2 415+1 (No BOHESIGHT) bO3-XXXXX RANGF RATE
i1uR TIME TO CS
RESEF ET
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-30 COPY ROOT FOR 1ST CSI 81J
BORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-t7 415+1 (NO BORFSIGHT) 50-XXxXx RANGF RATE
267R VELOCITY TO HE GAINED CSI
402R LELTA H
371R OFLTA V COH
372R OELTA T CSICDH
-5 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 blb+XXXXX RANGE
-i2 415+1 (No BORESIGHT) 5n3-XXXXX RANGE RATE
415+1 (NO BORESIGHT)
5-5
503-XXXXX RANGF RATE
COPY Roor FOR 2NO CSI BU
bORESIGHT ON CSM 415+1 316+XXXXX RANGE
TEMPPRESS MON SEL - FUEL MAN
A AND 8 PRESS 181 +-3 PIG TEMPPRESS MON SEL - PRPLNT
A AND B TEMP IND 4ODEG 0 IOODEG F A AND B PRFSS IND 181 +-3 PSIA
tEMPPRESS MON SEL - HEL
A AND 8 PRESS IND PSIA
A QUANTITY IND- -- PERCENT RFMAINING
8 QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4p 2 3 (120 - 190 DFG F)
415+1 (NO BORESIGHT)-17 503-XXXXX RANGE RATE
-15 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
(LOS OF MSFN) S-BAND - SLEW 10 P = +90t Y U S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
-12 415+1 (No 8ORESIGHT)
503-XXXXX RANGE RATE
267R VFLOCITY TU BE GAINED CSI
402R OFLTA H
372R TIME CSICH
371R PREDICTED VEL 10 RE GAINED COH
263R OLT-OF-PLANE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATL
-10 COPY RANGE AND ROOT FOR 3RD CSI 8U
SORESIGH ON CSM 41b+1
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
10 PURPOSE
This document contains the primary procedures for the LM-5 active rendezvous with CSM-107 spacecraft in accordance with Detailed Test Objective Section 40 defined in Reference 71
The purpose of the LM Rendezvous Procedures document is to provide a single source of procedures information for use in flight planning in crew training and in preparing onboard data
This is a control document subject to review by all elements of the Apollo Program and to approval by the Procedures Conshyfiguration Control Board Comments should be directed to Mr Stephen P Grega Flight Procedures Branch Flight Crew Support Division Extension 5348
Beyond G mission planning no additional techniques and trajectory information specific to Mission H have been made available as of this date Therefore since Missions G and H are expected to be similar in the area of rendezvous guidance and navigation procedures the G mission final LM Rendezvous Procedures Document will serve -as an H mission preliminary LM Rendezvous and Procedures Document After reviewal by all elements of the Apollo Program and approval by the Procedures Configuration Control Board this document will then evolve into the control document for the Mission H crew procedures
2-1
20 INTRODUCTION
The LM-5CSM-l07 lunar orbit rendezvous exercise will beginduring the twenty-fourth CSM revolution with insertion at 122 35255 and end at approximately 1260000 with post rendezvous station keeping The LM procedures during this period are divided into segments of major activities which are discussed in detail in Section 30
A nominal LM-5CSM-107 mission profile is contained in Figshyure (2-1) This figure shows the locations in time and local horizontal position of the most significant nominal mission events Trajectory data used to generate the mission profile and timeline for procedures development was obtained from Reference 72 The rendezvous navigation update schedule assumed in the procedures is defined in Reference 73
A history of the LM body attitudes during the rendezvous accompanies the major events discussion and is also presented in Figures (2-2) and (2-3) Each figure illustrates the bodyattitudes with respect to the moon sun and earth and indicates FDAI roll pitch and yaw gimbal angles and the ordeal pitch angle for significant events during each lunar orbit
0RBI TR EL
TRAILINGDISPLACEMENT(N MI) 0 0 W60 20240 BE
33I I ] I I I
32 ltrMCCE 1125+-3 C CH (124t24) PLAN CHANGE023 TM)2
R~TC(222
40 1146235 A N MNTTIMETKS FROMISEDRT(GA122plusmn252
-- DAYLIGHT B shy
_ _ _ _ _ _ __E_ _ -- 7 LUNAR IARFAGELM MAJOR EVENTS
122+35 INSERTION 17 124+H7 AGE UPDATE AND ALIGN (R47) 2 122+40 IMU REFSMMAT ALIGN (P52) 1 124+24 CDH THRUSTING (P41) TRAILINGDISPLACEMETIN RI)
3 122+54 AGS UPDATE AND ALIGN (R471 19 124+26 TPI TARGETING IP34 amp AGS) 5 II 20 25 30 4 122+55 CSI TARGETING IP32 amp AGSI 20 124+26-124+51 RR NAVIGATION (P20 18 MARKS) - I I
5 122+54-123+14 RR NAVIGATION (P20 18 MARKS) 21 124+53 AGS UPDATE AND ALIGN (R47)I
6 123+18 COMPUTE CSI BACKUP 22 125+00 COMPUTE TPI BACKUP
7 123+19 AGS UPDATE AND ALIGN (R471 23 125+03 TPI THRUSTING (P411 c
8 123+26 CSI THRUSTING (P411 24 125+05 MCC1 TARGETING IP35) N - M ((25+232
9 123+30 SET W MATRIX 1200025) 25 125+05-125+16 RR NAVIGATION IP20 9 MARKS) 5
2 r INSERT A 10 123+31 CDH TARGETING IP33 amp AGS 26 125+16 COMPUTE MCCI THRUSTING IP41) 5 31 PHAE
11 123+31-123+46 RR NAVIGATION 1P20 14 MARKS) 27 125+18 MCC I THRUSTING (P41)
12 123+47 EXT AV FOR PLANE CHANGE (P20) 28 125+20 MCC2 TARGETING (P351 13 123+54 RCS PLANE CHANGE THRUSTING (P411 29 125+20-125+31 RR NAVIGATION (P20 9 MARKS) 14 123+56 CDH TARGETING (P33 amp AGS) 30 125+31 COMPUTE MCC 2 BACKUP Ideg
15 123+56-124+12 RR NAVIGATION (P20 13 MARKS) 31 125+33 MCC2 THRUSTING [P41)
16 124+15 COMPUTE CDH BACKUP 32 125+48 BRAKING (P47) 27 26TP25+03
33 126+00 STATION KEEPING LT
24
FIGURE 2-1 G MISSION RENDEZVOUS
(CSM-CENTERED RELATIVE MOTION) FOLDOUT FRAME
l D T R2A-e2 TALPFO EDUR ES EPREPAREDBY STEPHENP GRED501I DOUT FRAMW ORBI R B C 0
MISSION G LUNAR ORBIT RENDEZVOUS ATTITUDE TIME HISTORY
OFOR THE LM P33
P20 123+31) (021880)
LMI CSI NrxNMARKS i (123+26+27)
FINAL -
COMP(I123+1l6)
P32 LANDING SITEj P20 30ES (122+50) CSM AT (04650) PRIME MERIDIAN LIFT-OFF
P52 (122+28+11) (122+40)DIRECTION OF (03640)ORBITAL MOTION IS
CLOCKWISE
(18012150)I NERTIAL YAWKLINERTIAL PITCH
ORDEAL PITCH EARTHINERTIAL ROLL
FIGURE 2-2
MISSION G LUNAR ORBIT RENDEZVOUS ATTITUDE TIME HISTORY
FOR THE LM
LM TPF (126+00+00) (01302920)
LM LMC2PLANE CHANGELMPI+30) (123+54+25)
(TPI+30) (0560)(0782400) 7 SUN
P20
(TPI+15) P3
P33(0532480) COMP
---- _ (124+12--- ---
LM TPI (125+02+46) L D (026 627650) (124+24+25)
(0980)
FINAL
DIRECTION OF COMP ORBITAL MOTION IS (124+50)
CLOCKWISE
(18012150)
LL INERTIAL YAW NERTIAL PITCH
ORDEAL PITCH EARTH INERTIAL ROLL
FIGURE 2-3
3-1
30 DISCUSSION OF MAJOR EVENTS
31 Concentric Sequence Initiation
Immediately following Insertion the LM navigated vector will be downlinked to Mission Control Center-Houston this state vector is then uplinked to the CSM The LM commander will perform a Proqram 52 fine alignment to REFSMMAT at approxishymately 12240
The digital autopilot is configured to wide deadband Program P20 is called and an automatic pitch maneuver is initiated to the preferred track attitude At 122 55 CSI targeting parameters are loaded in the PGNS and AGS A period of rendezvous radar marking will then take place from 122-57 to 12315 Upon completion of tracking the LM will obtain an out-of-plane velocity from the CSM to be vectored with the in-plane component of the CSI delta V The CSMs estishymate of out-of-plane velocity is alleged to be better than the LMs estimate (Reference 74)
At approximately 123 20 the LM will voice its CSI solution to the CSM the AGS is updated aligned and targeted in external delta-V with the CDH solution to be excuted Program P41 will then be called and the automatic pitch maneuver bypassed since the burn isto be executed with Z-Axis thrusting The CSI burn occurs nominally at 123 26 27 After verification of the LM CSI burn the CSM will incorporate the LM burn parameters in its CMC LM state vector
32 Constant Delta Height and Plane Change
At 12330 approximately three minutes after the LM CSI burn the W matrix will be set to (200025) and the LM targeting paramters are loaded in both the PGNS and AGS for the CDH maneuver Out-of-plane velocity will then be computed and voiced to the LM from the CSM Program P30 is loaded with the targeting parameters for the LM Plane Change maneuver which will be accomplished in Program P41 30 minutes prior to the CDH maneuver Following the burn the target delta V parameters are voice to the CSM and incorporated into the CMC LM state vector At 12356 the CDH targeting parameters are loaded in both the PGNS and AGS for 1242425 A CDH chart solution is calculated 7 minutes prior to TIG The AGS is updated aligned and targeted in external delta V with the CDH solution to be executed The RCS Thrust Program P41 is called at 12418 and the burn attitude is bypassed since the LM executes CDH by thrusting out individual components of delta V while maintaining radar lock-on
3-2
3 3 Terminal Phase Initiation
Radar tracking is initiated after the CDH maneuver and updating of the LGC continued At 12426 approximately two minutes after the LM CDH burn targeting parameters are loaded in both the PGNS and AGS for the TPI maneuver which will be targeted for a node at intercept Backup measurements are made at the appropriate times The AGS is updated aligned and targeted in external delta V with the TPI solution to be executed The RCS Thrust Program P41 is called at 12456 and the burn attitude is bypassed since the LM is burning along the plus Z-axis with the thrust direction established with the COAS
3 4 Midcourse Corrections
Immediately after TPI the Midcourse Prethrust Program P35 will be called and radar tracking reinitiated Backup measshyurements are made and midcourse corrections chart solutions obtained The MCCl burn will nominally be performed at TPI plus 15 minutes (1251746) If MCCI is to be excuted Program P41 will be called and the burn attitude maneuver is bypassed since the plus Z-axis will remain boresighted at the CSM until docking
Following MCCI Program P35 will be called and targeted for MCC2 at TPI plus 30 minutes (1253246) and executed identishycally to MCCI
3 5 Braking
In preparation for braking the DAP is configured in narrow deadband Program P20 is terminated at 18000 feet but the radar is kept in auto track to provide radar range and range rate displayed on the tapemeter Average G is called by Program P47 prior to braking and attitude hold is selected The braking schedule is followed as contained in Section 4
4-1
40 NOMINAL MISSION PROCEDURES
The procedures included in this section do not specify which crewmember Commander or LM Pilot performs each task These need not be specified since the following basic rules define which crewmember performs each task
41 Commander Tasks
1 All attitude changes whether manual or automatic will be accomplished by the CDR
2 The operation of the DSKY during thrust programs (P40 P41 P42 P47) will be done by the CDR Actual manipulation of the TTCA need not be always done by the CDR but in most cases will be
3 Operation of the rendezvous and landing radar will be done by the CDR
4 The CDR will operate all other systems accessible to only his crew station
42 LM Pilot Tasks
1 AGS operation 2 DSKY operation will be done by the LMP except when keyboard
entries affect the control of spacecraft attitude or thrustshying
3 Backup data logging and chart calculations 4 All logging of maneuver solutions and systems performance 5 The LMP will operate all other systems accessible to only
his crew station
These general rules are guidelines only and may be deviated from by the LM crew if they develop more efficient Task assignments
43 ABBREVIATIONS
The abbreviations used herein are consistant with those in the AOH However in order to condense and simplify the procedures so that they are representative of onboard data a number of addshyitional shorthand conventions have been used To allow the unshyfamiliar reader to understand the procedures contained in this section the following explanations are included
1 AGS - A single asterisk is employed to denote those procedures involving operations to be performed on the DEDA The three number group following an asterisk specifies DEDA address An Rfollowing the address group indicates the address is to be read out A five digit group behind the Rindicates a nominal or expected display If the three number address group is followed by a plus or minus sign a data load is indicated When a single digit follows the plus addition of four zeros behind this digit is assumed Once used these conventions are easily handled and save considerable space
4-2
2 PGNS - The verb-noun addresses in the PGNS are indicated to the left of the procedures column An F is used to indicate a flashing display or absence of an F a static display To the right of the verb-noun on the same line are the contents of the three data registers If numeric quantities appear the DSKY should be correspondingly made to agree by executing a V21 V22 or V23 and performing a data load The procedure of blanking and loading registers is not included since it is repeated often and is highly familiar to the crews
EXAMPLE F 06 33 125-02 46 TIG OF TPI
Expanded this means Load flashing verb 06 noun 33 with the quantity 125 hours 2 minutes and 46 seconds the time of ignition of the RCS engine TPI maneuver Procedurally this is done by keying verb 25 enter loading +000125 in register 1 +00002 in register 2 and +04600 in register 3
If numberic quantities do not follow the verb-noun it is indicated that a computed or information quantity is being displayed via the DSKY If nominal values are listed for possible comparison they appear in parentheses
EXAMPLE- F 06 42 HA HP V
Expanded this means Flashing verb 06 noun 42 has computed height of apogee in register 1 height of perigee in regshyister 2 and velocity to be gained in register 3
3 TIME - The numbers in the left hand column preceded by a plus or minus indicate event timer time referenced to an event Minus indicates event timer counting down to a future event Periodically this same column contains the nominal mission ground elapsed times in parentheses Asterisks following the event time indicate a time critical event which should be accomplished to the nearest second
4-3
4 4 Nominal PGNS Procedures
ASSUMPTIONS
AFTER INSERTION
1 INSERTION COMPLETE (RESIOUALS NULLED) VERIFY V82E (ORBIT) 3 RNDZ RDR LOCKED ON IN MODE II 4 LGC AT FLASHING VERB 37 5 PROPER INITIAL W MATRIX LOADED IN LGC
GUID CONT-PGNS ATTITUDE MON-PGNS(CDR) RATE ERR MON-CMPTR(LMP) ATTITUDE MON-AGS(LMP) SHFTTRUN-+5 DEG X-POINTER-HI MULT RADAR TEST SW-OFF ENG ARM-OFF X-TRANSL-2JETS DEAD BAND-MIN PGNS MODE CONT-AUTO THROTJET-JET CBPGNS IMU OPR-CLOSE RR MODE-LGC TTCATRANSL-ENABLE(COR)
BAL CPL-ON MODE SEL-AGS
RNGALT MON-RNGRNGRT RATE ERR MON-RNDZ RORICOR) ATT CONT-PULSE(3)
AGS MODE CONT-ATT HOLD ACA4JET-DISABLE(CDRJ TTCATRANSL-DISABLE(LMP)
ACA4JET-DISABLE(LMPI
KEY ODE (PO0)
(DOWNLINK LM STATE VECTOR)
KEY V63E (RR SELF TEST)
4-4
F 04 12 00004 00001 PRO
F 16 72 TRUN SHFT PRO
F 16 78 R ROOT VERIFY TAPE METER WITH DSKY
+2 VERIFY INSERTION VELOCITY WITH RNDZ ROR WHERE RANGE = 2642 NM RANGE RATE = -4251 FPS
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
KEY V34E (TERMINATE) KEY V48E (LOAD DAP)
F 01 46 11002 PRO
F 06 47 LMWT CMWT PRO
KEY V56E (KILL AUTO TRACK ENABLE)
+3 KEY V41N72E (COARSE ALIGN RR) F 21 73 +000OOTRUN -077OOSHFT F 04 12 00006 00002 (CONTINUOUS DESIGNATE)
PRO 41 (COARSE ALIGN VERB)
KEY VI6N72E 16 72 MONITOR TRUNSHFT ANGLES
CB PGNS RNDZ RDR-OPEN CB AC BUS A RNDZ RDR-OPEN KEY V44E (TERMINATE RR DESIGNATE)
KEY V83E F 16 54 R ROOT THETA
SET ORDEAL PRO
CS HEATER AOT-CLOSE
CB AOT LAMP-CLOSE
+5 KEY V37E52E (IMU REALIGN)
4-5
410+1 CSI ROUTINE 373+02065 CS TIME 275+03028 TPI TIME
605400777 COTANGENT OF LOS TO-CSM 416+1 (ONE-HALF bRBITAL PERIOD) 411+0 RCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT 310R TIME TO CS
267R VELOCITY TO BE GAINED CSI
402R DELTA H
371R DELTA V CDH
372R _ DELTA T CSICDH
F 04 06 00001 00003 -(REFSMMAT) PRO -
F 50 25 00015 SELECT 1ST STAR ENTR
F 01 70 O02DE LOAD 1ST STAR PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FOAl ANGLES (AUTO MNVRI)
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVR)
F 01 71 002DE
KEY V76E PGNS MODE CONT-ATT HOLD
PRO +10 F 54 71 MARK 1ST STAR
PRO F 01 70 O02DE LOAD 2ND STAR
PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FDA ANGLES -(AUTO MNVRV
F 50 18 FDAI ANGLES (REQUEST PNVRt ENTR (BYPASS MNVR
F 01 71 002DE PGNS MODE CONT-ATT HOLD PRO
-35
4-6
+14 F 54 71 MARK 2ND STAR PRO
F 06 05 STAR ANGLE DIFFERENCE PRO
F 06 93 GYRO TORQUE ANGLES PRO
F 50 25 00014
PRO (CHECK ALIGNMENT IF TIME WILL PERMIT)
F 50 25 00015 SELECT 3RD STAR ENTR
F 01 70 OO2DE LOAD 3RD STAR PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FDAI ANGLES (AUTO MNVR)
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVR)
VERIFY ALIGNMENT VIA AOT
KEY V34E (TERMINATE) F 37 BB
V48E (LOAD DAP) F 01 46 11012
PRO F 06 47 LMWT CMWT
+17 PRO
CB AOT LAMP-OPEN
RESET ET (310R)
(12253) CB AC BUS A RNDZ RDR-CLOSE (WAIT 30 SEC) CB PGNS RNDZ RDR-CLOSE
RR MODE-LGC KEY V37E20E (ACQUIRE RADAR)
PGNS MODE CONT-AUTO F 50 18 FDA ANGLES (REQUEST MNVRJ
PRO (AUTO MNVR) 06 18 FDAI ANGLES (AUTO MNVR)
AGS MODE CONT-AUTO RATEERR MON-CMPTR (LMP)
F 50 18 FDAI ANGLES (REQUEST MNVR)
4-7
ENTR (BYPASS MNVR) NO TRK LT-OFF
F 50 72 RR TRUNSHFT VERIFY RR LOCK ON PRO
DSKY BLANKS
KEY V93E (BEFORE 1ST MARK REINIT W MATRIXI KEY V80E (UPDATE LM SV)
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (i20OOZOO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
400+3 AGS ALIGNshy400R (00000 COMPLETE) 507+0 Z-AXIS BORESIGHT 400+2 ACQUISITION STEERING
CS
(122amp55) KEY V37E32E (CSI)
F 06 11 1 S LOAD TIG CSI FROM DATA PAD (NOM 123S26- 271 PRO
F 06 55 +O000IN +02660E +13000 OMEGAT (CDH 180 DEG AFTER CSI PRO
F 06 37 LOAD TIG TPI FROM DATA PAD (NOM 1251021761 PRO
F 16 45 MKS TFI -00001
-30 COPY RDOT FOR 1ST CSI BU
31OR TIME TO CSI
267R VELOCITY TO BE GAINED CSI
402R DELTA H
371R DELTA V CDH
-22
4-8
372R _ DELTA T CSICDH
KEY V32E (MARKS=5
F 06 75 DELTA H DELTA T CSICDH DELTA T CDHTPI PRO
F 06 81 DELTA VOS-LV (CS) (NOM 501 DELTA VX)
CSI(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (CDH)
(NOM 60 DELTA VX) CDH(82)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
KEY V32E (MARKS=1C)
F 06 75 DELTA H DELTA TCSICDH DELTA TCDHTPI PRD
F 06 81 DELTA VS-LV (CSI) CSI(N811
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 82 DELTA VIS-LV(CDH)
CDH(82)
DELTA VX(LVI
DELTA VY(LV)
DELTA VZ(LV)
-12
4-9
-20 COPY RDOT FOR 2ND CSI BU
F 16 45
F 06 75
F 06 81
F 06 16
F 06 90
PRO MKS TFI -00001
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS NON SEL - PRPLNT A + B TEMP IND 40DEG TO lOODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + 8 PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4v 2 3 (120 - 190 DEG F
(LOS OF MSFN ) S-BAND - SLEW TO P = +90 Y a 0 S-BAND - FWD (OR AFT) S-BAND - DN VOICE BU BIOMED OFF
PRO (FINAL COMP)
267R - VELOCITY TO BE GAINED CSI
402R DELTA H
372R TIME CSICDHL
371R PREDICTED VEL TO BE GAINED CDH
263R OUT-OF-PLANE
DELTA H DELTA TCSICDH DELTA TCDHTPI PRO DELTA VS-LV (CSI)
KEY V9OE (OUT-OF-PLANED
0 LOAD TIG CSI FROM DATA PAD (NOM 12302627) PRO Y YDOT PSI
N90 CSM
YDOT
PRO
-7
4-10
F 06 81 DELTA VS-LV(CSI)
COPY YDOT FROM CSM AND LOAD NEGATIVE IN R2 CSIIN81I
DELTA VX(LV)
DELTA VYILV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (COH)
CDH(82)
DELTA VX(LV)
- DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RANGE AND RDOT FOR 3RD CS BU
COMPUTE CSI BU
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (i2000OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
(TRANSMIT CSI DATA TO CSMI VHF A XMTR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF TELEMETY PCM - LO
KEY VB3E F 16 54 R ROOT THETA
SET ORDEAL PRO
317R RANGE
440R RANGE RATE
4-11
400+3 AGS ALIGN t40OR (00000 COMPLETE)
277R THETA
PRO F 37 BB
-6 KEY 41E (RCS THRUSTING) F 50 18 FDAI-ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTAV 400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTAV 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA RF
TRANSMIT TGT DELTA VS TO CSM AND SYNC COUNTDOWN
16 85 DELTA VS-BODY
502R DELTA VZ (NOM 5Ql)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTAVS-BODY
(123t26t27) BURN +Z
NULL DELTA VS
4-12
VERIFY AGS RESIDUALS 50OR 501R 502R DELTA VX _ DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
CDH
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
KEY V67E (RESET W MATRIX) F 06 99 +0200E +O0020E +00005E
PRO
507+0 Z-AXIS BORESIGHT
(VHF RANGING WITH CSM) VHF A XMTR - VOICERNG VHF B XMTR - OFF VHF B RCVR - ON TELEMETRY PCM - HI
(12331) KEY V37E33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 a TIG CDH (NOM 1242425) -120 amp00 10 (AGS 0 TIME)
(CONVERT TO MINUTES)
411+0 THRUST ALONG Z-BODY AXIS ENTER IF YOU DONT TARGET CSI
373R (NOM 26443 310R TIME TO CDH
4-13
423R DESIRED ALT RATE AT CDH
402R DELTA Hshy
450R DELTA VX
452R DELTA VZ
623+0 Z-AXIS PARALLEL TO CSM PLANE
IPRO F 16 45 MKS TFI -00001
-52 RESET ET
KEY V93E (REINIT W MATRIX WHEN MARKS =4)
KEY V32E (MARKS = 3)
F 06 75 DELTA HCDH DELTA TCDHTPI DELTA TTPI PRO
F 06 81 DELTA VCDH-LV CDH(N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
-47 KEY VSOE (OUT-OF-PLANE)
_ TIG CDH (NOM 124t24t25) -3000 TIME FROM CDH
F 06 16 l1 LOAD TIG PLANE CHANGE (NOM 123amp54-253 PRO
F 06 90 Y YDOT PSI N90 CSM
VYDOT PRO
-42 KEY V32E (MARKS=1O)
F 06 75 DELTA HCDH DELTA TCDIHTPI DELTA TTPITPI PRO
F 06 81 DELTA VCDH-LV
4-14
CDH (NS1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -OO1
KEY V34E (TERMINATE) F 37 B8
PLANE CHANGE
KEY 30E (EXTERNAL DELTA V)
TIG CDH (NOM 124124t25) -3000 TIME FROM CDH
F 06 33 LOAD TIG PLANE CHANGE (NOM 123154T25) PRO
F 06 81 DELTA VS-LV (NOM 00)
-36 COPY RDOT FOR 1ST CDH BU
KEY V90E (OUT-OF-PLANE)
F 06 16 1 1 LOAD TIG PLANE CHANGE (NOM 1231543251 PRO
F 06 90 Y YOOT PSI N90 CSM
YDOT
PRO
F 06 81 DELTA VS-LV(NOM 00)
COPY YDOT AND LOAD NEGATIVE IN R2 PRO
F 06 42 HA HP DELTA V PRO
F 16 45 MKS TFI MGA
PRO
F 37 BB
KEY 41E (RCS THRUSTING)
-30
4-15
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVRI
410+5 EXTERNAL DELTA V 450+0 451-YDOT 452+0 (LOAD CSM -YDOT)
407+0 ROTATE EXTERNAL DELTA V RF
16 95 DELTA VS-BODY
-3035 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATTVHOLD 407+1 FREEZE EXTERNAL DELTAV
F 16 85 DELTA VS-BODY -
NULL DELTA VIS
PRO F 37BB
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
507+0 Z-AXIS BORESIGHT
(12356) KEY 33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 TIG CDH (NOM 124t24t25) -120 OO ZOO (AGS 0 TIME)
(CONVERT TO MINUTES)
373R _ (NOM 2644) 310R TIME TO CDH
423R DESIRED ALT RATE AT CDH
(ADS OF MSFN) S-BAND - SLEW TOP = ACQUIRE HGA LOCK ON VOICE - BUVOICE -- VOICE VERIFY VOICE TLM BIOMED - LEFT (OR RIGHT)
402R DELTAH
4-16
F 16 45
-25
-23
F 06 75
F 06 81
F 16 45
-12
F 06 75
F 06 81
450R DELTA VX
452R DELTA VZ
PRO MKS TFI -00001
KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
COPY ROOT FOR 2ND CDH BU
KEY v32E (MARKS = 5)
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40DEG TO 1OODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + B PRESS IND PSIA
A QUANTITY IND _ PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING a TEMP MON SEL RCS QUAD 1 4 2 3 (120 - 190 DEG F)i
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
CDH(NB1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO MKS TFI -00001
PRO (FINAL COMP)
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
KEY V9OE (OUT-OF-PLANE)
-7
4-17
F 06 16 jj LOAD TIG CDH FROM DATA PAD (NOM 12424251 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT PRO
COPY YOOT FROM CSM AND LOAD NEGATIVE IN R2
CDH(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RDOT FOR 3RD CDH BU
COMPUTE CDH BU
TRANSMIT TGT DELTA VOS TO CSM AND SYNC COUNTDOWN
KEY V47E (INITIALIZE AGS F 06 16 GET OF AGS 0 TIME 120O00OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
KEY V83E F 16 54 R RDOT THETA
SET ORDEAL PRO
317R _ RANGE
440R RANGE RATE 400+3 AGS ALIGN 40OR (00000 COMPLETE)
277R THETA
-6
4-18
PRO F 3 BB
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY V06N86E F 06 86 DELTA VIS-LV
AGS(N86) CHART
DELTA VX(LVD
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
16 85 DELTA VS-BODY
50OR DELTA VX (NOM -0O3)
502R DELTA VZ (NOM 60)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD 407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS BODY
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS 5OOR 50IR 502R DELTA VX -DELTA VY DELTA VZ-
VERIFY PGNS RESIDUALS N85
DELTA VX(LM)
4-19
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
TPI
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO 507+0 Z-AXIS BORESIGHT
(12426) KEY 34E (TPI)
-36 RESET ET
F 06 37 - amp LOAD TIG TPI FROM DATA PAD (NOM 1250246) PRO
F 06 55 +00000 +02660E +13000 OMEGAT PRO
F 16 45 MARKS TFI -00001
-32 KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
-29 KEY V32E (MARKS = 3)
F 06 37 __ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
RESET ET
410+3 TPI SEARCH ROUTINE 307+04300 DELTA T TRANSFER
4-20
-26 310+02600 TFI TPI
303R THETA AT TPI
267R DELTA VTPI
371R DELTA VTPI + DELTA VTPF
KEY V32E (MARKS = 10)
F 06 37 _ _ _ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VIS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
TEMPIPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40ODEG TO IGODEG F A + B PRESS IND 181 +-3 PSIA
TEMPIPRESS MON SEL - HEL
A + B PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD I 4 2 3 (120 - 190 DEG F)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
RESET ET
-13 310+01300 TFI TPI
303R THETA AT TPI
-12 PRO (FINAL COMP) F 06 37 Z TIG TPIj__
4-21
TRANSMIT TIG OF TPI TO CSM-
PRO F 06 58 HP DELTA VTPI DELTA VTRF
PRO F 06 81 DELTA VS-LV
KEY V9OE (OUT-OF-PLANE)
F 06 16 1 LOAD TIG TPI FROM DATA PAD (NOM 12502461 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT
PRO F 06 81 DELTA VS-LV
COPY CSM YDOT AND LOAD NEGATIVE IN R2 N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 59 DELTA VS LOS
N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI MGA
RESET ET
PRO F 37 BB
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (12000t600)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE)
-10
-6
4-22
F 50 16 DOWNLINK COMPLETE PRO (UPDATE COMPLETE)
400+3 AGS ALIGN 400R (00000 COMPLETE)
-9 277R COPY TGT LOS ANGLE
310+00800
303R THETA AT TPI 410+4 DIRECT TRANSFER AT ET=-8 404+0 405+0 406+0 (MONITOR 470 471 4721
373R TIG TPI
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
KEY 41E (RCS THRUSTING) F 50 18 FOAl ANGLES (REQUEST MNVRI
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
-5 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUS
400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
COMPUTE TPI BU
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
4-23
1685 DELTA VS-BODY
50OR DELTA VX(NOM -115)
502R DELTA VZ(NOM 229)
-Z35 OSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS-BODY
(1250246) BURN +Z
VERIFY AGS RESIDUALS 500R 501R 502R DELTAVX DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
MCC1
KEY V76E (PGNS PULSE) PGNSMODECONT-AUTO
KEY V93E (BEFORE 1ST MARK REINITW MATRIX)
+2 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
4-24
(LOS OF MSFN) S-BAND - SLEW TO P = 90 Y = 0 S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
404+0 405+0 406+0
(MONITOR 470 471 4721
+9 277R COPY TGT LOS ANGLE
+12 PRO (COMPUTE MCC FOR TPI+15I F 06 81 DELTA VS-LV
PRO F 06 59 DELTA VS-LOS
PRO F 16 45 MKS TFI MGA
+13 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUOS
COMPUTE MCC1 BU
PRO F 37 BB
+14 KEY 41E (RCS THRUSTING) F 50 18 FOAL ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+1425 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+15 F 16 85 NULL DELTA VS
PRO F 37 BB
MCC2
KEY V76E (PGNS PULSE)
4-25
PGNS MODE CONT-AUTO
KEY V93E (BEFORE 1ST MARK REINIT W MATRIX)
+16 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
404+0 405+0 406+0 (MONITOR 470 471 47)shy
+24 277R COPY TGT LOS ANGLE
+27 PRO (COMPUTE MCC FORTPI+30) F 06 81 DELTA VS-LV
PRO F 06 59 DELIA VPS-LOS
PRO F 16 45 MKS TFI MGA
+28 277R COPY TGT LOS ANGLE
COPY R RDOT FROM TAPEMETER FOR BUS
COMPUTE MCC2 BU
F 37 BB PRO
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+2925 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+30 F 16 85 NULL DELTA VS
PRO F 37 BB
KEY OOE (P001
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
4-26
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT KEY V34E (TERMINATE)
KEY V37E47E (AVE G) F 16 83 DELTA VIS
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT VERIFY TAPE METER WITH DSKY
BRAKING GATE 30 FPS - 6000 FT 20 FPS - 3000 FT 10 FPS - 1500 FT 5 FPS - 600 FT
RENDEZVOUS
STATION KEEPING
5-1
50 ABORT PROCEDURE
This is a specific AGS nominal abort procedure due to a PGNS failure between insertion and station keeping
51
5-2
Nominal AGS Procedures
ASSUMPTIONS
AFTER INSERTION
I INSERTION COMPLETE (RFSIDUALS NULLED) g PGNS FAILURE BEFORE INSERTION 3 RAUAR NOT LOCKED ON
(UI CoNT-AGS ATlI[uUE MON-AGS(CDR) RATE ERR MON-CNPTR(LMP) ATTITUDE MON-AGS(LMP) SHFITRUN-+5 DEG X-POINTER-HI MULT RADAR IEST Sw-OFF LNb GMbL-OFF ENG ARM-OFF X-IRANSL-2 JETS DEAD BAND-MAX PGNS MODE CONT-OFF THROTJET-JET CB IMU OIR-ON HH MOVE-AUTO rRACK TTCATNANSL-ENABLE(CDR)
AL CPL-ON MODE SL-AGS RNGAL1 MON-RNbRNGRT RAIE ERR MON-RNDZ HDR(CDR) AVl CoNT(3)-PULSE AGS MODE CONT-AUTO ACA4JET-DISABLE(CDR) TTCATRANSL-DISABLE(LMP) ACA4JET-DISABLE(LMP)
bO7+U Z-AXIS BOPESIGHT 400+2 Z-AXIS STEERING PULSE TO NULL AGS ERRORS POINT Z-AXIS IN DIRECTION OF CSM MODE CONT-ATT HOLD ATT CONT(3)-MODE CONTROL O unnr - ZirF
5-3
SLEW PATE - LO
SLEW RR ANT TO OqON FUAI VERIFY MAX SIGNAL STRENGTH RH MOOE-AUTO TRACK NO TRACK LIGHT OFF -
ATT CONT(3h-PULSE
CHECK INSERTION VELOCITY WITH TAPEMETER COMPARE EAPEMETER WITH AGS STATE VECTOR DATA I
17R RANGE(NOM 2642)
440R RANGE RATE(NOM -425l)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
cSI
+3 417+1 (RADAR FILTER INITIALIZED) 41b+l (NO BOHESIGHT) b03-XXXXX RANGE RATE
+5 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGF
41b+1 CSI ROUTINE 373+o2065 CSi TIME 275+03028 TPI TIME 605+0077 COTANGENT OF LOS TO CSM 41b+1 (ONE-HALF OFBITAL-PERIOD) 411+0 HCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT
610R TIME TO CST
43 RESET ET
267R VELOCITY TO BE GAINED CSI
402R FLTA H
371R DFLTA V CDH
5-4
372R DFLTA T CSICDH
-42 415+1 (No BORESIGHT) bO6-xXXXX RANGE RATE
-40 415+1 (NO BORESIGHT)503-XXXXX RANGE RATE dORESIGHT ON CSM
415+1 316+XXXXX RANGE
-37 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE
-15 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE UORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-2 415+1 (No BOHESIGHT) bO3-XXXXX RANGF RATE
i1uR TIME TO CS
RESEF ET
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-30 COPY ROOT FOR 1ST CSI 81J
BORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-t7 415+1 (NO BORFSIGHT) 50-XXxXx RANGF RATE
267R VELOCITY TO HE GAINED CSI
402R LELTA H
371R OFLTA V COH
372R OELTA T CSICDH
-5 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 blb+XXXXX RANGE
-i2 415+1 (No BORESIGHT) 5n3-XXXXX RANGE RATE
415+1 (NO BORESIGHT)
5-5
503-XXXXX RANGF RATE
COPY Roor FOR 2NO CSI BU
bORESIGHT ON CSM 415+1 316+XXXXX RANGE
TEMPPRESS MON SEL - FUEL MAN
A AND 8 PRESS 181 +-3 PIG TEMPPRESS MON SEL - PRPLNT
A AND B TEMP IND 4ODEG 0 IOODEG F A AND B PRFSS IND 181 +-3 PSIA
tEMPPRESS MON SEL - HEL
A AND 8 PRESS IND PSIA
A QUANTITY IND- -- PERCENT RFMAINING
8 QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4p 2 3 (120 - 190 DFG F)
415+1 (NO BORESIGHT)-17 503-XXXXX RANGE RATE
-15 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
(LOS OF MSFN) S-BAND - SLEW 10 P = +90t Y U S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
-12 415+1 (No 8ORESIGHT)
503-XXXXX RANGE RATE
267R VFLOCITY TU BE GAINED CSI
402R OFLTA H
372R TIME CSICH
371R PREDICTED VEL 10 RE GAINED COH
263R OLT-OF-PLANE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATL
-10 COPY RANGE AND ROOT FOR 3RD CSI 8U
SORESIGH ON CSM 41b+1
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
2-1
20 INTRODUCTION
The LM-5CSM-l07 lunar orbit rendezvous exercise will beginduring the twenty-fourth CSM revolution with insertion at 122 35255 and end at approximately 1260000 with post rendezvous station keeping The LM procedures during this period are divided into segments of major activities which are discussed in detail in Section 30
A nominal LM-5CSM-107 mission profile is contained in Figshyure (2-1) This figure shows the locations in time and local horizontal position of the most significant nominal mission events Trajectory data used to generate the mission profile and timeline for procedures development was obtained from Reference 72 The rendezvous navigation update schedule assumed in the procedures is defined in Reference 73
A history of the LM body attitudes during the rendezvous accompanies the major events discussion and is also presented in Figures (2-2) and (2-3) Each figure illustrates the bodyattitudes with respect to the moon sun and earth and indicates FDAI roll pitch and yaw gimbal angles and the ordeal pitch angle for significant events during each lunar orbit
0RBI TR EL
TRAILINGDISPLACEMENT(N MI) 0 0 W60 20240 BE
33I I ] I I I
32 ltrMCCE 1125+-3 C CH (124t24) PLAN CHANGE023 TM)2
R~TC(222
40 1146235 A N MNTTIMETKS FROMISEDRT(GA122plusmn252
-- DAYLIGHT B shy
_ _ _ _ _ _ __E_ _ -- 7 LUNAR IARFAGELM MAJOR EVENTS
122+35 INSERTION 17 124+H7 AGE UPDATE AND ALIGN (R47) 2 122+40 IMU REFSMMAT ALIGN (P52) 1 124+24 CDH THRUSTING (P41) TRAILINGDISPLACEMETIN RI)
3 122+54 AGS UPDATE AND ALIGN (R471 19 124+26 TPI TARGETING IP34 amp AGS) 5 II 20 25 30 4 122+55 CSI TARGETING IP32 amp AGSI 20 124+26-124+51 RR NAVIGATION (P20 18 MARKS) - I I
5 122+54-123+14 RR NAVIGATION (P20 18 MARKS) 21 124+53 AGS UPDATE AND ALIGN (R47)I
6 123+18 COMPUTE CSI BACKUP 22 125+00 COMPUTE TPI BACKUP
7 123+19 AGS UPDATE AND ALIGN (R471 23 125+03 TPI THRUSTING (P411 c
8 123+26 CSI THRUSTING (P411 24 125+05 MCC1 TARGETING IP35) N - M ((25+232
9 123+30 SET W MATRIX 1200025) 25 125+05-125+16 RR NAVIGATION IP20 9 MARKS) 5
2 r INSERT A 10 123+31 CDH TARGETING IP33 amp AGS 26 125+16 COMPUTE MCCI THRUSTING IP41) 5 31 PHAE
11 123+31-123+46 RR NAVIGATION 1P20 14 MARKS) 27 125+18 MCC I THRUSTING (P41)
12 123+47 EXT AV FOR PLANE CHANGE (P20) 28 125+20 MCC2 TARGETING (P351 13 123+54 RCS PLANE CHANGE THRUSTING (P411 29 125+20-125+31 RR NAVIGATION (P20 9 MARKS) 14 123+56 CDH TARGETING (P33 amp AGS) 30 125+31 COMPUTE MCC 2 BACKUP Ideg
15 123+56-124+12 RR NAVIGATION (P20 13 MARKS) 31 125+33 MCC2 THRUSTING [P41)
16 124+15 COMPUTE CDH BACKUP 32 125+48 BRAKING (P47) 27 26TP25+03
33 126+00 STATION KEEPING LT
24
FIGURE 2-1 G MISSION RENDEZVOUS
(CSM-CENTERED RELATIVE MOTION) FOLDOUT FRAME
l D T R2A-e2 TALPFO EDUR ES EPREPAREDBY STEPHENP GRED501I DOUT FRAMW ORBI R B C 0
MISSION G LUNAR ORBIT RENDEZVOUS ATTITUDE TIME HISTORY
OFOR THE LM P33
P20 123+31) (021880)
LMI CSI NrxNMARKS i (123+26+27)
FINAL -
COMP(I123+1l6)
P32 LANDING SITEj P20 30ES (122+50) CSM AT (04650) PRIME MERIDIAN LIFT-OFF
P52 (122+28+11) (122+40)DIRECTION OF (03640)ORBITAL MOTION IS
CLOCKWISE
(18012150)I NERTIAL YAWKLINERTIAL PITCH
ORDEAL PITCH EARTHINERTIAL ROLL
FIGURE 2-2
MISSION G LUNAR ORBIT RENDEZVOUS ATTITUDE TIME HISTORY
FOR THE LM
LM TPF (126+00+00) (01302920)
LM LMC2PLANE CHANGELMPI+30) (123+54+25)
(TPI+30) (0560)(0782400) 7 SUN
P20
(TPI+15) P3
P33(0532480) COMP
---- _ (124+12--- ---
LM TPI (125+02+46) L D (026 627650) (124+24+25)
(0980)
FINAL
DIRECTION OF COMP ORBITAL MOTION IS (124+50)
CLOCKWISE
(18012150)
LL INERTIAL YAW NERTIAL PITCH
ORDEAL PITCH EARTH INERTIAL ROLL
FIGURE 2-3
3-1
30 DISCUSSION OF MAJOR EVENTS
31 Concentric Sequence Initiation
Immediately following Insertion the LM navigated vector will be downlinked to Mission Control Center-Houston this state vector is then uplinked to the CSM The LM commander will perform a Proqram 52 fine alignment to REFSMMAT at approxishymately 12240
The digital autopilot is configured to wide deadband Program P20 is called and an automatic pitch maneuver is initiated to the preferred track attitude At 122 55 CSI targeting parameters are loaded in the PGNS and AGS A period of rendezvous radar marking will then take place from 122-57 to 12315 Upon completion of tracking the LM will obtain an out-of-plane velocity from the CSM to be vectored with the in-plane component of the CSI delta V The CSMs estishymate of out-of-plane velocity is alleged to be better than the LMs estimate (Reference 74)
At approximately 123 20 the LM will voice its CSI solution to the CSM the AGS is updated aligned and targeted in external delta-V with the CDH solution to be excuted Program P41 will then be called and the automatic pitch maneuver bypassed since the burn isto be executed with Z-Axis thrusting The CSI burn occurs nominally at 123 26 27 After verification of the LM CSI burn the CSM will incorporate the LM burn parameters in its CMC LM state vector
32 Constant Delta Height and Plane Change
At 12330 approximately three minutes after the LM CSI burn the W matrix will be set to (200025) and the LM targeting paramters are loaded in both the PGNS and AGS for the CDH maneuver Out-of-plane velocity will then be computed and voiced to the LM from the CSM Program P30 is loaded with the targeting parameters for the LM Plane Change maneuver which will be accomplished in Program P41 30 minutes prior to the CDH maneuver Following the burn the target delta V parameters are voice to the CSM and incorporated into the CMC LM state vector At 12356 the CDH targeting parameters are loaded in both the PGNS and AGS for 1242425 A CDH chart solution is calculated 7 minutes prior to TIG The AGS is updated aligned and targeted in external delta V with the CDH solution to be executed The RCS Thrust Program P41 is called at 12418 and the burn attitude is bypassed since the LM executes CDH by thrusting out individual components of delta V while maintaining radar lock-on
3-2
3 3 Terminal Phase Initiation
Radar tracking is initiated after the CDH maneuver and updating of the LGC continued At 12426 approximately two minutes after the LM CDH burn targeting parameters are loaded in both the PGNS and AGS for the TPI maneuver which will be targeted for a node at intercept Backup measurements are made at the appropriate times The AGS is updated aligned and targeted in external delta V with the TPI solution to be executed The RCS Thrust Program P41 is called at 12456 and the burn attitude is bypassed since the LM is burning along the plus Z-axis with the thrust direction established with the COAS
3 4 Midcourse Corrections
Immediately after TPI the Midcourse Prethrust Program P35 will be called and radar tracking reinitiated Backup measshyurements are made and midcourse corrections chart solutions obtained The MCCl burn will nominally be performed at TPI plus 15 minutes (1251746) If MCCI is to be excuted Program P41 will be called and the burn attitude maneuver is bypassed since the plus Z-axis will remain boresighted at the CSM until docking
Following MCCI Program P35 will be called and targeted for MCC2 at TPI plus 30 minutes (1253246) and executed identishycally to MCCI
3 5 Braking
In preparation for braking the DAP is configured in narrow deadband Program P20 is terminated at 18000 feet but the radar is kept in auto track to provide radar range and range rate displayed on the tapemeter Average G is called by Program P47 prior to braking and attitude hold is selected The braking schedule is followed as contained in Section 4
4-1
40 NOMINAL MISSION PROCEDURES
The procedures included in this section do not specify which crewmember Commander or LM Pilot performs each task These need not be specified since the following basic rules define which crewmember performs each task
41 Commander Tasks
1 All attitude changes whether manual or automatic will be accomplished by the CDR
2 The operation of the DSKY during thrust programs (P40 P41 P42 P47) will be done by the CDR Actual manipulation of the TTCA need not be always done by the CDR but in most cases will be
3 Operation of the rendezvous and landing radar will be done by the CDR
4 The CDR will operate all other systems accessible to only his crew station
42 LM Pilot Tasks
1 AGS operation 2 DSKY operation will be done by the LMP except when keyboard
entries affect the control of spacecraft attitude or thrustshying
3 Backup data logging and chart calculations 4 All logging of maneuver solutions and systems performance 5 The LMP will operate all other systems accessible to only
his crew station
These general rules are guidelines only and may be deviated from by the LM crew if they develop more efficient Task assignments
43 ABBREVIATIONS
The abbreviations used herein are consistant with those in the AOH However in order to condense and simplify the procedures so that they are representative of onboard data a number of addshyitional shorthand conventions have been used To allow the unshyfamiliar reader to understand the procedures contained in this section the following explanations are included
1 AGS - A single asterisk is employed to denote those procedures involving operations to be performed on the DEDA The three number group following an asterisk specifies DEDA address An Rfollowing the address group indicates the address is to be read out A five digit group behind the Rindicates a nominal or expected display If the three number address group is followed by a plus or minus sign a data load is indicated When a single digit follows the plus addition of four zeros behind this digit is assumed Once used these conventions are easily handled and save considerable space
4-2
2 PGNS - The verb-noun addresses in the PGNS are indicated to the left of the procedures column An F is used to indicate a flashing display or absence of an F a static display To the right of the verb-noun on the same line are the contents of the three data registers If numeric quantities appear the DSKY should be correspondingly made to agree by executing a V21 V22 or V23 and performing a data load The procedure of blanking and loading registers is not included since it is repeated often and is highly familiar to the crews
EXAMPLE F 06 33 125-02 46 TIG OF TPI
Expanded this means Load flashing verb 06 noun 33 with the quantity 125 hours 2 minutes and 46 seconds the time of ignition of the RCS engine TPI maneuver Procedurally this is done by keying verb 25 enter loading +000125 in register 1 +00002 in register 2 and +04600 in register 3
If numberic quantities do not follow the verb-noun it is indicated that a computed or information quantity is being displayed via the DSKY If nominal values are listed for possible comparison they appear in parentheses
EXAMPLE- F 06 42 HA HP V
Expanded this means Flashing verb 06 noun 42 has computed height of apogee in register 1 height of perigee in regshyister 2 and velocity to be gained in register 3
3 TIME - The numbers in the left hand column preceded by a plus or minus indicate event timer time referenced to an event Minus indicates event timer counting down to a future event Periodically this same column contains the nominal mission ground elapsed times in parentheses Asterisks following the event time indicate a time critical event which should be accomplished to the nearest second
4-3
4 4 Nominal PGNS Procedures
ASSUMPTIONS
AFTER INSERTION
1 INSERTION COMPLETE (RESIOUALS NULLED) VERIFY V82E (ORBIT) 3 RNDZ RDR LOCKED ON IN MODE II 4 LGC AT FLASHING VERB 37 5 PROPER INITIAL W MATRIX LOADED IN LGC
GUID CONT-PGNS ATTITUDE MON-PGNS(CDR) RATE ERR MON-CMPTR(LMP) ATTITUDE MON-AGS(LMP) SHFTTRUN-+5 DEG X-POINTER-HI MULT RADAR TEST SW-OFF ENG ARM-OFF X-TRANSL-2JETS DEAD BAND-MIN PGNS MODE CONT-AUTO THROTJET-JET CBPGNS IMU OPR-CLOSE RR MODE-LGC TTCATRANSL-ENABLE(COR)
BAL CPL-ON MODE SEL-AGS
RNGALT MON-RNGRNGRT RATE ERR MON-RNDZ RORICOR) ATT CONT-PULSE(3)
AGS MODE CONT-ATT HOLD ACA4JET-DISABLE(CDRJ TTCATRANSL-DISABLE(LMP)
ACA4JET-DISABLE(LMPI
KEY ODE (PO0)
(DOWNLINK LM STATE VECTOR)
KEY V63E (RR SELF TEST)
4-4
F 04 12 00004 00001 PRO
F 16 72 TRUN SHFT PRO
F 16 78 R ROOT VERIFY TAPE METER WITH DSKY
+2 VERIFY INSERTION VELOCITY WITH RNDZ ROR WHERE RANGE = 2642 NM RANGE RATE = -4251 FPS
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
KEY V34E (TERMINATE) KEY V48E (LOAD DAP)
F 01 46 11002 PRO
F 06 47 LMWT CMWT PRO
KEY V56E (KILL AUTO TRACK ENABLE)
+3 KEY V41N72E (COARSE ALIGN RR) F 21 73 +000OOTRUN -077OOSHFT F 04 12 00006 00002 (CONTINUOUS DESIGNATE)
PRO 41 (COARSE ALIGN VERB)
KEY VI6N72E 16 72 MONITOR TRUNSHFT ANGLES
CB PGNS RNDZ RDR-OPEN CB AC BUS A RNDZ RDR-OPEN KEY V44E (TERMINATE RR DESIGNATE)
KEY V83E F 16 54 R ROOT THETA
SET ORDEAL PRO
CS HEATER AOT-CLOSE
CB AOT LAMP-CLOSE
+5 KEY V37E52E (IMU REALIGN)
4-5
410+1 CSI ROUTINE 373+02065 CS TIME 275+03028 TPI TIME
605400777 COTANGENT OF LOS TO-CSM 416+1 (ONE-HALF bRBITAL PERIOD) 411+0 RCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT 310R TIME TO CS
267R VELOCITY TO BE GAINED CSI
402R DELTA H
371R DELTA V CDH
372R _ DELTA T CSICDH
F 04 06 00001 00003 -(REFSMMAT) PRO -
F 50 25 00015 SELECT 1ST STAR ENTR
F 01 70 O02DE LOAD 1ST STAR PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FOAl ANGLES (AUTO MNVRI)
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVR)
F 01 71 002DE
KEY V76E PGNS MODE CONT-ATT HOLD
PRO +10 F 54 71 MARK 1ST STAR
PRO F 01 70 O02DE LOAD 2ND STAR
PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FDA ANGLES -(AUTO MNVRV
F 50 18 FDAI ANGLES (REQUEST PNVRt ENTR (BYPASS MNVR
F 01 71 002DE PGNS MODE CONT-ATT HOLD PRO
-35
4-6
+14 F 54 71 MARK 2ND STAR PRO
F 06 05 STAR ANGLE DIFFERENCE PRO
F 06 93 GYRO TORQUE ANGLES PRO
F 50 25 00014
PRO (CHECK ALIGNMENT IF TIME WILL PERMIT)
F 50 25 00015 SELECT 3RD STAR ENTR
F 01 70 OO2DE LOAD 3RD STAR PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FDAI ANGLES (AUTO MNVR)
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVR)
VERIFY ALIGNMENT VIA AOT
KEY V34E (TERMINATE) F 37 BB
V48E (LOAD DAP) F 01 46 11012
PRO F 06 47 LMWT CMWT
+17 PRO
CB AOT LAMP-OPEN
RESET ET (310R)
(12253) CB AC BUS A RNDZ RDR-CLOSE (WAIT 30 SEC) CB PGNS RNDZ RDR-CLOSE
RR MODE-LGC KEY V37E20E (ACQUIRE RADAR)
PGNS MODE CONT-AUTO F 50 18 FDA ANGLES (REQUEST MNVRJ
PRO (AUTO MNVR) 06 18 FDAI ANGLES (AUTO MNVR)
AGS MODE CONT-AUTO RATEERR MON-CMPTR (LMP)
F 50 18 FDAI ANGLES (REQUEST MNVR)
4-7
ENTR (BYPASS MNVR) NO TRK LT-OFF
F 50 72 RR TRUNSHFT VERIFY RR LOCK ON PRO
DSKY BLANKS
KEY V93E (BEFORE 1ST MARK REINIT W MATRIXI KEY V80E (UPDATE LM SV)
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (i20OOZOO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
400+3 AGS ALIGNshy400R (00000 COMPLETE) 507+0 Z-AXIS BORESIGHT 400+2 ACQUISITION STEERING
CS
(122amp55) KEY V37E32E (CSI)
F 06 11 1 S LOAD TIG CSI FROM DATA PAD (NOM 123S26- 271 PRO
F 06 55 +O000IN +02660E +13000 OMEGAT (CDH 180 DEG AFTER CSI PRO
F 06 37 LOAD TIG TPI FROM DATA PAD (NOM 1251021761 PRO
F 16 45 MKS TFI -00001
-30 COPY RDOT FOR 1ST CSI BU
31OR TIME TO CSI
267R VELOCITY TO BE GAINED CSI
402R DELTA H
371R DELTA V CDH
-22
4-8
372R _ DELTA T CSICDH
KEY V32E (MARKS=5
F 06 75 DELTA H DELTA T CSICDH DELTA T CDHTPI PRO
F 06 81 DELTA VOS-LV (CS) (NOM 501 DELTA VX)
CSI(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (CDH)
(NOM 60 DELTA VX) CDH(82)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
KEY V32E (MARKS=1C)
F 06 75 DELTA H DELTA TCSICDH DELTA TCDHTPI PRD
F 06 81 DELTA VS-LV (CSI) CSI(N811
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 82 DELTA VIS-LV(CDH)
CDH(82)
DELTA VX(LVI
DELTA VY(LV)
DELTA VZ(LV)
-12
4-9
-20 COPY RDOT FOR 2ND CSI BU
F 16 45
F 06 75
F 06 81
F 06 16
F 06 90
PRO MKS TFI -00001
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS NON SEL - PRPLNT A + B TEMP IND 40DEG TO lOODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + 8 PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4v 2 3 (120 - 190 DEG F
(LOS OF MSFN ) S-BAND - SLEW TO P = +90 Y a 0 S-BAND - FWD (OR AFT) S-BAND - DN VOICE BU BIOMED OFF
PRO (FINAL COMP)
267R - VELOCITY TO BE GAINED CSI
402R DELTA H
372R TIME CSICDHL
371R PREDICTED VEL TO BE GAINED CDH
263R OUT-OF-PLANE
DELTA H DELTA TCSICDH DELTA TCDHTPI PRO DELTA VS-LV (CSI)
KEY V9OE (OUT-OF-PLANED
0 LOAD TIG CSI FROM DATA PAD (NOM 12302627) PRO Y YDOT PSI
N90 CSM
YDOT
PRO
-7
4-10
F 06 81 DELTA VS-LV(CSI)
COPY YDOT FROM CSM AND LOAD NEGATIVE IN R2 CSIIN81I
DELTA VX(LV)
DELTA VYILV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (COH)
CDH(82)
DELTA VX(LV)
- DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RANGE AND RDOT FOR 3RD CS BU
COMPUTE CSI BU
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (i2000OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
(TRANSMIT CSI DATA TO CSMI VHF A XMTR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF TELEMETY PCM - LO
KEY VB3E F 16 54 R ROOT THETA
SET ORDEAL PRO
317R RANGE
440R RANGE RATE
4-11
400+3 AGS ALIGN t40OR (00000 COMPLETE)
277R THETA
PRO F 37 BB
-6 KEY 41E (RCS THRUSTING) F 50 18 FDAI-ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTAV 400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTAV 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA RF
TRANSMIT TGT DELTA VS TO CSM AND SYNC COUNTDOWN
16 85 DELTA VS-BODY
502R DELTA VZ (NOM 5Ql)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTAVS-BODY
(123t26t27) BURN +Z
NULL DELTA VS
4-12
VERIFY AGS RESIDUALS 50OR 501R 502R DELTA VX _ DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
CDH
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
KEY V67E (RESET W MATRIX) F 06 99 +0200E +O0020E +00005E
PRO
507+0 Z-AXIS BORESIGHT
(VHF RANGING WITH CSM) VHF A XMTR - VOICERNG VHF B XMTR - OFF VHF B RCVR - ON TELEMETRY PCM - HI
(12331) KEY V37E33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 a TIG CDH (NOM 1242425) -120 amp00 10 (AGS 0 TIME)
(CONVERT TO MINUTES)
411+0 THRUST ALONG Z-BODY AXIS ENTER IF YOU DONT TARGET CSI
373R (NOM 26443 310R TIME TO CDH
4-13
423R DESIRED ALT RATE AT CDH
402R DELTA Hshy
450R DELTA VX
452R DELTA VZ
623+0 Z-AXIS PARALLEL TO CSM PLANE
IPRO F 16 45 MKS TFI -00001
-52 RESET ET
KEY V93E (REINIT W MATRIX WHEN MARKS =4)
KEY V32E (MARKS = 3)
F 06 75 DELTA HCDH DELTA TCDHTPI DELTA TTPI PRO
F 06 81 DELTA VCDH-LV CDH(N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
-47 KEY VSOE (OUT-OF-PLANE)
_ TIG CDH (NOM 124t24t25) -3000 TIME FROM CDH
F 06 16 l1 LOAD TIG PLANE CHANGE (NOM 123amp54-253 PRO
F 06 90 Y YDOT PSI N90 CSM
VYDOT PRO
-42 KEY V32E (MARKS=1O)
F 06 75 DELTA HCDH DELTA TCDIHTPI DELTA TTPITPI PRO
F 06 81 DELTA VCDH-LV
4-14
CDH (NS1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -OO1
KEY V34E (TERMINATE) F 37 B8
PLANE CHANGE
KEY 30E (EXTERNAL DELTA V)
TIG CDH (NOM 124124t25) -3000 TIME FROM CDH
F 06 33 LOAD TIG PLANE CHANGE (NOM 123154T25) PRO
F 06 81 DELTA VS-LV (NOM 00)
-36 COPY RDOT FOR 1ST CDH BU
KEY V90E (OUT-OF-PLANE)
F 06 16 1 1 LOAD TIG PLANE CHANGE (NOM 1231543251 PRO
F 06 90 Y YOOT PSI N90 CSM
YDOT
PRO
F 06 81 DELTA VS-LV(NOM 00)
COPY YDOT AND LOAD NEGATIVE IN R2 PRO
F 06 42 HA HP DELTA V PRO
F 16 45 MKS TFI MGA
PRO
F 37 BB
KEY 41E (RCS THRUSTING)
-30
4-15
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVRI
410+5 EXTERNAL DELTA V 450+0 451-YDOT 452+0 (LOAD CSM -YDOT)
407+0 ROTATE EXTERNAL DELTA V RF
16 95 DELTA VS-BODY
-3035 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATTVHOLD 407+1 FREEZE EXTERNAL DELTAV
F 16 85 DELTA VS-BODY -
NULL DELTA VIS
PRO F 37BB
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
507+0 Z-AXIS BORESIGHT
(12356) KEY 33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 TIG CDH (NOM 124t24t25) -120 OO ZOO (AGS 0 TIME)
(CONVERT TO MINUTES)
373R _ (NOM 2644) 310R TIME TO CDH
423R DESIRED ALT RATE AT CDH
(ADS OF MSFN) S-BAND - SLEW TOP = ACQUIRE HGA LOCK ON VOICE - BUVOICE -- VOICE VERIFY VOICE TLM BIOMED - LEFT (OR RIGHT)
402R DELTAH
4-16
F 16 45
-25
-23
F 06 75
F 06 81
F 16 45
-12
F 06 75
F 06 81
450R DELTA VX
452R DELTA VZ
PRO MKS TFI -00001
KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
COPY ROOT FOR 2ND CDH BU
KEY v32E (MARKS = 5)
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40DEG TO 1OODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + B PRESS IND PSIA
A QUANTITY IND _ PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING a TEMP MON SEL RCS QUAD 1 4 2 3 (120 - 190 DEG F)i
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
CDH(NB1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO MKS TFI -00001
PRO (FINAL COMP)
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
KEY V9OE (OUT-OF-PLANE)
-7
4-17
F 06 16 jj LOAD TIG CDH FROM DATA PAD (NOM 12424251 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT PRO
COPY YOOT FROM CSM AND LOAD NEGATIVE IN R2
CDH(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RDOT FOR 3RD CDH BU
COMPUTE CDH BU
TRANSMIT TGT DELTA VOS TO CSM AND SYNC COUNTDOWN
KEY V47E (INITIALIZE AGS F 06 16 GET OF AGS 0 TIME 120O00OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
KEY V83E F 16 54 R RDOT THETA
SET ORDEAL PRO
317R _ RANGE
440R RANGE RATE 400+3 AGS ALIGN 40OR (00000 COMPLETE)
277R THETA
-6
4-18
PRO F 3 BB
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY V06N86E F 06 86 DELTA VIS-LV
AGS(N86) CHART
DELTA VX(LVD
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
16 85 DELTA VS-BODY
50OR DELTA VX (NOM -0O3)
502R DELTA VZ (NOM 60)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD 407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS BODY
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS 5OOR 50IR 502R DELTA VX -DELTA VY DELTA VZ-
VERIFY PGNS RESIDUALS N85
DELTA VX(LM)
4-19
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
TPI
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO 507+0 Z-AXIS BORESIGHT
(12426) KEY 34E (TPI)
-36 RESET ET
F 06 37 - amp LOAD TIG TPI FROM DATA PAD (NOM 1250246) PRO
F 06 55 +00000 +02660E +13000 OMEGAT PRO
F 16 45 MARKS TFI -00001
-32 KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
-29 KEY V32E (MARKS = 3)
F 06 37 __ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
RESET ET
410+3 TPI SEARCH ROUTINE 307+04300 DELTA T TRANSFER
4-20
-26 310+02600 TFI TPI
303R THETA AT TPI
267R DELTA VTPI
371R DELTA VTPI + DELTA VTPF
KEY V32E (MARKS = 10)
F 06 37 _ _ _ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VIS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
TEMPIPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40ODEG TO IGODEG F A + B PRESS IND 181 +-3 PSIA
TEMPIPRESS MON SEL - HEL
A + B PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD I 4 2 3 (120 - 190 DEG F)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
RESET ET
-13 310+01300 TFI TPI
303R THETA AT TPI
-12 PRO (FINAL COMP) F 06 37 Z TIG TPIj__
4-21
TRANSMIT TIG OF TPI TO CSM-
PRO F 06 58 HP DELTA VTPI DELTA VTRF
PRO F 06 81 DELTA VS-LV
KEY V9OE (OUT-OF-PLANE)
F 06 16 1 LOAD TIG TPI FROM DATA PAD (NOM 12502461 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT
PRO F 06 81 DELTA VS-LV
COPY CSM YDOT AND LOAD NEGATIVE IN R2 N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 59 DELTA VS LOS
N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI MGA
RESET ET
PRO F 37 BB
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (12000t600)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE)
-10
-6
4-22
F 50 16 DOWNLINK COMPLETE PRO (UPDATE COMPLETE)
400+3 AGS ALIGN 400R (00000 COMPLETE)
-9 277R COPY TGT LOS ANGLE
310+00800
303R THETA AT TPI 410+4 DIRECT TRANSFER AT ET=-8 404+0 405+0 406+0 (MONITOR 470 471 4721
373R TIG TPI
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
KEY 41E (RCS THRUSTING) F 50 18 FOAl ANGLES (REQUEST MNVRI
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
-5 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUS
400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
COMPUTE TPI BU
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
4-23
1685 DELTA VS-BODY
50OR DELTA VX(NOM -115)
502R DELTA VZ(NOM 229)
-Z35 OSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS-BODY
(1250246) BURN +Z
VERIFY AGS RESIDUALS 500R 501R 502R DELTAVX DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
MCC1
KEY V76E (PGNS PULSE) PGNSMODECONT-AUTO
KEY V93E (BEFORE 1ST MARK REINITW MATRIX)
+2 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
4-24
(LOS OF MSFN) S-BAND - SLEW TO P = 90 Y = 0 S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
404+0 405+0 406+0
(MONITOR 470 471 4721
+9 277R COPY TGT LOS ANGLE
+12 PRO (COMPUTE MCC FOR TPI+15I F 06 81 DELTA VS-LV
PRO F 06 59 DELTA VS-LOS
PRO F 16 45 MKS TFI MGA
+13 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUOS
COMPUTE MCC1 BU
PRO F 37 BB
+14 KEY 41E (RCS THRUSTING) F 50 18 FOAL ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+1425 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+15 F 16 85 NULL DELTA VS
PRO F 37 BB
MCC2
KEY V76E (PGNS PULSE)
4-25
PGNS MODE CONT-AUTO
KEY V93E (BEFORE 1ST MARK REINIT W MATRIX)
+16 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
404+0 405+0 406+0 (MONITOR 470 471 47)shy
+24 277R COPY TGT LOS ANGLE
+27 PRO (COMPUTE MCC FORTPI+30) F 06 81 DELTA VS-LV
PRO F 06 59 DELIA VPS-LOS
PRO F 16 45 MKS TFI MGA
+28 277R COPY TGT LOS ANGLE
COPY R RDOT FROM TAPEMETER FOR BUS
COMPUTE MCC2 BU
F 37 BB PRO
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+2925 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+30 F 16 85 NULL DELTA VS
PRO F 37 BB
KEY OOE (P001
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
4-26
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT KEY V34E (TERMINATE)
KEY V37E47E (AVE G) F 16 83 DELTA VIS
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT VERIFY TAPE METER WITH DSKY
BRAKING GATE 30 FPS - 6000 FT 20 FPS - 3000 FT 10 FPS - 1500 FT 5 FPS - 600 FT
RENDEZVOUS
STATION KEEPING
5-1
50 ABORT PROCEDURE
This is a specific AGS nominal abort procedure due to a PGNS failure between insertion and station keeping
51
5-2
Nominal AGS Procedures
ASSUMPTIONS
AFTER INSERTION
I INSERTION COMPLETE (RFSIDUALS NULLED) g PGNS FAILURE BEFORE INSERTION 3 RAUAR NOT LOCKED ON
(UI CoNT-AGS ATlI[uUE MON-AGS(CDR) RATE ERR MON-CNPTR(LMP) ATTITUDE MON-AGS(LMP) SHFITRUN-+5 DEG X-POINTER-HI MULT RADAR IEST Sw-OFF LNb GMbL-OFF ENG ARM-OFF X-IRANSL-2 JETS DEAD BAND-MAX PGNS MODE CONT-OFF THROTJET-JET CB IMU OIR-ON HH MOVE-AUTO rRACK TTCATNANSL-ENABLE(CDR)
AL CPL-ON MODE SL-AGS RNGAL1 MON-RNbRNGRT RAIE ERR MON-RNDZ HDR(CDR) AVl CoNT(3)-PULSE AGS MODE CONT-AUTO ACA4JET-DISABLE(CDR) TTCATRANSL-DISABLE(LMP) ACA4JET-DISABLE(LMP)
bO7+U Z-AXIS BOPESIGHT 400+2 Z-AXIS STEERING PULSE TO NULL AGS ERRORS POINT Z-AXIS IN DIRECTION OF CSM MODE CONT-ATT HOLD ATT CONT(3)-MODE CONTROL O unnr - ZirF
5-3
SLEW PATE - LO
SLEW RR ANT TO OqON FUAI VERIFY MAX SIGNAL STRENGTH RH MOOE-AUTO TRACK NO TRACK LIGHT OFF -
ATT CONT(3h-PULSE
CHECK INSERTION VELOCITY WITH TAPEMETER COMPARE EAPEMETER WITH AGS STATE VECTOR DATA I
17R RANGE(NOM 2642)
440R RANGE RATE(NOM -425l)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
cSI
+3 417+1 (RADAR FILTER INITIALIZED) 41b+l (NO BOHESIGHT) b03-XXXXX RANGE RATE
+5 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGF
41b+1 CSI ROUTINE 373+o2065 CSi TIME 275+03028 TPI TIME 605+0077 COTANGENT OF LOS TO CSM 41b+1 (ONE-HALF OFBITAL-PERIOD) 411+0 HCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT
610R TIME TO CST
43 RESET ET
267R VELOCITY TO BE GAINED CSI
402R FLTA H
371R DFLTA V CDH
5-4
372R DFLTA T CSICDH
-42 415+1 (No BORESIGHT) bO6-xXXXX RANGE RATE
-40 415+1 (NO BORESIGHT)503-XXXXX RANGE RATE dORESIGHT ON CSM
415+1 316+XXXXX RANGE
-37 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE
-15 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE UORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-2 415+1 (No BOHESIGHT) bO3-XXXXX RANGF RATE
i1uR TIME TO CS
RESEF ET
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-30 COPY ROOT FOR 1ST CSI 81J
BORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-t7 415+1 (NO BORFSIGHT) 50-XXxXx RANGF RATE
267R VELOCITY TO HE GAINED CSI
402R LELTA H
371R OFLTA V COH
372R OELTA T CSICDH
-5 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 blb+XXXXX RANGE
-i2 415+1 (No BORESIGHT) 5n3-XXXXX RANGE RATE
415+1 (NO BORESIGHT)
5-5
503-XXXXX RANGF RATE
COPY Roor FOR 2NO CSI BU
bORESIGHT ON CSM 415+1 316+XXXXX RANGE
TEMPPRESS MON SEL - FUEL MAN
A AND 8 PRESS 181 +-3 PIG TEMPPRESS MON SEL - PRPLNT
A AND B TEMP IND 4ODEG 0 IOODEG F A AND B PRFSS IND 181 +-3 PSIA
tEMPPRESS MON SEL - HEL
A AND 8 PRESS IND PSIA
A QUANTITY IND- -- PERCENT RFMAINING
8 QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4p 2 3 (120 - 190 DFG F)
415+1 (NO BORESIGHT)-17 503-XXXXX RANGE RATE
-15 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
(LOS OF MSFN) S-BAND - SLEW 10 P = +90t Y U S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
-12 415+1 (No 8ORESIGHT)
503-XXXXX RANGE RATE
267R VFLOCITY TU BE GAINED CSI
402R OFLTA H
372R TIME CSICH
371R PREDICTED VEL 10 RE GAINED COH
263R OLT-OF-PLANE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATL
-10 COPY RANGE AND ROOT FOR 3RD CSI 8U
SORESIGH ON CSM 41b+1
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
0RBI TR EL
TRAILINGDISPLACEMENT(N MI) 0 0 W60 20240 BE
33I I ] I I I
32 ltrMCCE 1125+-3 C CH (124t24) PLAN CHANGE023 TM)2
R~TC(222
40 1146235 A N MNTTIMETKS FROMISEDRT(GA122plusmn252
-- DAYLIGHT B shy
_ _ _ _ _ _ __E_ _ -- 7 LUNAR IARFAGELM MAJOR EVENTS
122+35 INSERTION 17 124+H7 AGE UPDATE AND ALIGN (R47) 2 122+40 IMU REFSMMAT ALIGN (P52) 1 124+24 CDH THRUSTING (P41) TRAILINGDISPLACEMETIN RI)
3 122+54 AGS UPDATE AND ALIGN (R471 19 124+26 TPI TARGETING IP34 amp AGS) 5 II 20 25 30 4 122+55 CSI TARGETING IP32 amp AGSI 20 124+26-124+51 RR NAVIGATION (P20 18 MARKS) - I I
5 122+54-123+14 RR NAVIGATION (P20 18 MARKS) 21 124+53 AGS UPDATE AND ALIGN (R47)I
6 123+18 COMPUTE CSI BACKUP 22 125+00 COMPUTE TPI BACKUP
7 123+19 AGS UPDATE AND ALIGN (R471 23 125+03 TPI THRUSTING (P411 c
8 123+26 CSI THRUSTING (P411 24 125+05 MCC1 TARGETING IP35) N - M ((25+232
9 123+30 SET W MATRIX 1200025) 25 125+05-125+16 RR NAVIGATION IP20 9 MARKS) 5
2 r INSERT A 10 123+31 CDH TARGETING IP33 amp AGS 26 125+16 COMPUTE MCCI THRUSTING IP41) 5 31 PHAE
11 123+31-123+46 RR NAVIGATION 1P20 14 MARKS) 27 125+18 MCC I THRUSTING (P41)
12 123+47 EXT AV FOR PLANE CHANGE (P20) 28 125+20 MCC2 TARGETING (P351 13 123+54 RCS PLANE CHANGE THRUSTING (P411 29 125+20-125+31 RR NAVIGATION (P20 9 MARKS) 14 123+56 CDH TARGETING (P33 amp AGS) 30 125+31 COMPUTE MCC 2 BACKUP Ideg
15 123+56-124+12 RR NAVIGATION (P20 13 MARKS) 31 125+33 MCC2 THRUSTING [P41)
16 124+15 COMPUTE CDH BACKUP 32 125+48 BRAKING (P47) 27 26TP25+03
33 126+00 STATION KEEPING LT
24
FIGURE 2-1 G MISSION RENDEZVOUS
(CSM-CENTERED RELATIVE MOTION) FOLDOUT FRAME
l D T R2A-e2 TALPFO EDUR ES EPREPAREDBY STEPHENP GRED501I DOUT FRAMW ORBI R B C 0
MISSION G LUNAR ORBIT RENDEZVOUS ATTITUDE TIME HISTORY
OFOR THE LM P33
P20 123+31) (021880)
LMI CSI NrxNMARKS i (123+26+27)
FINAL -
COMP(I123+1l6)
P32 LANDING SITEj P20 30ES (122+50) CSM AT (04650) PRIME MERIDIAN LIFT-OFF
P52 (122+28+11) (122+40)DIRECTION OF (03640)ORBITAL MOTION IS
CLOCKWISE
(18012150)I NERTIAL YAWKLINERTIAL PITCH
ORDEAL PITCH EARTHINERTIAL ROLL
FIGURE 2-2
MISSION G LUNAR ORBIT RENDEZVOUS ATTITUDE TIME HISTORY
FOR THE LM
LM TPF (126+00+00) (01302920)
LM LMC2PLANE CHANGELMPI+30) (123+54+25)
(TPI+30) (0560)(0782400) 7 SUN
P20
(TPI+15) P3
P33(0532480) COMP
---- _ (124+12--- ---
LM TPI (125+02+46) L D (026 627650) (124+24+25)
(0980)
FINAL
DIRECTION OF COMP ORBITAL MOTION IS (124+50)
CLOCKWISE
(18012150)
LL INERTIAL YAW NERTIAL PITCH
ORDEAL PITCH EARTH INERTIAL ROLL
FIGURE 2-3
3-1
30 DISCUSSION OF MAJOR EVENTS
31 Concentric Sequence Initiation
Immediately following Insertion the LM navigated vector will be downlinked to Mission Control Center-Houston this state vector is then uplinked to the CSM The LM commander will perform a Proqram 52 fine alignment to REFSMMAT at approxishymately 12240
The digital autopilot is configured to wide deadband Program P20 is called and an automatic pitch maneuver is initiated to the preferred track attitude At 122 55 CSI targeting parameters are loaded in the PGNS and AGS A period of rendezvous radar marking will then take place from 122-57 to 12315 Upon completion of tracking the LM will obtain an out-of-plane velocity from the CSM to be vectored with the in-plane component of the CSI delta V The CSMs estishymate of out-of-plane velocity is alleged to be better than the LMs estimate (Reference 74)
At approximately 123 20 the LM will voice its CSI solution to the CSM the AGS is updated aligned and targeted in external delta-V with the CDH solution to be excuted Program P41 will then be called and the automatic pitch maneuver bypassed since the burn isto be executed with Z-Axis thrusting The CSI burn occurs nominally at 123 26 27 After verification of the LM CSI burn the CSM will incorporate the LM burn parameters in its CMC LM state vector
32 Constant Delta Height and Plane Change
At 12330 approximately three minutes after the LM CSI burn the W matrix will be set to (200025) and the LM targeting paramters are loaded in both the PGNS and AGS for the CDH maneuver Out-of-plane velocity will then be computed and voiced to the LM from the CSM Program P30 is loaded with the targeting parameters for the LM Plane Change maneuver which will be accomplished in Program P41 30 minutes prior to the CDH maneuver Following the burn the target delta V parameters are voice to the CSM and incorporated into the CMC LM state vector At 12356 the CDH targeting parameters are loaded in both the PGNS and AGS for 1242425 A CDH chart solution is calculated 7 minutes prior to TIG The AGS is updated aligned and targeted in external delta V with the CDH solution to be executed The RCS Thrust Program P41 is called at 12418 and the burn attitude is bypassed since the LM executes CDH by thrusting out individual components of delta V while maintaining radar lock-on
3-2
3 3 Terminal Phase Initiation
Radar tracking is initiated after the CDH maneuver and updating of the LGC continued At 12426 approximately two minutes after the LM CDH burn targeting parameters are loaded in both the PGNS and AGS for the TPI maneuver which will be targeted for a node at intercept Backup measurements are made at the appropriate times The AGS is updated aligned and targeted in external delta V with the TPI solution to be executed The RCS Thrust Program P41 is called at 12456 and the burn attitude is bypassed since the LM is burning along the plus Z-axis with the thrust direction established with the COAS
3 4 Midcourse Corrections
Immediately after TPI the Midcourse Prethrust Program P35 will be called and radar tracking reinitiated Backup measshyurements are made and midcourse corrections chart solutions obtained The MCCl burn will nominally be performed at TPI plus 15 minutes (1251746) If MCCI is to be excuted Program P41 will be called and the burn attitude maneuver is bypassed since the plus Z-axis will remain boresighted at the CSM until docking
Following MCCI Program P35 will be called and targeted for MCC2 at TPI plus 30 minutes (1253246) and executed identishycally to MCCI
3 5 Braking
In preparation for braking the DAP is configured in narrow deadband Program P20 is terminated at 18000 feet but the radar is kept in auto track to provide radar range and range rate displayed on the tapemeter Average G is called by Program P47 prior to braking and attitude hold is selected The braking schedule is followed as contained in Section 4
4-1
40 NOMINAL MISSION PROCEDURES
The procedures included in this section do not specify which crewmember Commander or LM Pilot performs each task These need not be specified since the following basic rules define which crewmember performs each task
41 Commander Tasks
1 All attitude changes whether manual or automatic will be accomplished by the CDR
2 The operation of the DSKY during thrust programs (P40 P41 P42 P47) will be done by the CDR Actual manipulation of the TTCA need not be always done by the CDR but in most cases will be
3 Operation of the rendezvous and landing radar will be done by the CDR
4 The CDR will operate all other systems accessible to only his crew station
42 LM Pilot Tasks
1 AGS operation 2 DSKY operation will be done by the LMP except when keyboard
entries affect the control of spacecraft attitude or thrustshying
3 Backup data logging and chart calculations 4 All logging of maneuver solutions and systems performance 5 The LMP will operate all other systems accessible to only
his crew station
These general rules are guidelines only and may be deviated from by the LM crew if they develop more efficient Task assignments
43 ABBREVIATIONS
The abbreviations used herein are consistant with those in the AOH However in order to condense and simplify the procedures so that they are representative of onboard data a number of addshyitional shorthand conventions have been used To allow the unshyfamiliar reader to understand the procedures contained in this section the following explanations are included
1 AGS - A single asterisk is employed to denote those procedures involving operations to be performed on the DEDA The three number group following an asterisk specifies DEDA address An Rfollowing the address group indicates the address is to be read out A five digit group behind the Rindicates a nominal or expected display If the three number address group is followed by a plus or minus sign a data load is indicated When a single digit follows the plus addition of four zeros behind this digit is assumed Once used these conventions are easily handled and save considerable space
4-2
2 PGNS - The verb-noun addresses in the PGNS are indicated to the left of the procedures column An F is used to indicate a flashing display or absence of an F a static display To the right of the verb-noun on the same line are the contents of the three data registers If numeric quantities appear the DSKY should be correspondingly made to agree by executing a V21 V22 or V23 and performing a data load The procedure of blanking and loading registers is not included since it is repeated often and is highly familiar to the crews
EXAMPLE F 06 33 125-02 46 TIG OF TPI
Expanded this means Load flashing verb 06 noun 33 with the quantity 125 hours 2 minutes and 46 seconds the time of ignition of the RCS engine TPI maneuver Procedurally this is done by keying verb 25 enter loading +000125 in register 1 +00002 in register 2 and +04600 in register 3
If numberic quantities do not follow the verb-noun it is indicated that a computed or information quantity is being displayed via the DSKY If nominal values are listed for possible comparison they appear in parentheses
EXAMPLE- F 06 42 HA HP V
Expanded this means Flashing verb 06 noun 42 has computed height of apogee in register 1 height of perigee in regshyister 2 and velocity to be gained in register 3
3 TIME - The numbers in the left hand column preceded by a plus or minus indicate event timer time referenced to an event Minus indicates event timer counting down to a future event Periodically this same column contains the nominal mission ground elapsed times in parentheses Asterisks following the event time indicate a time critical event which should be accomplished to the nearest second
4-3
4 4 Nominal PGNS Procedures
ASSUMPTIONS
AFTER INSERTION
1 INSERTION COMPLETE (RESIOUALS NULLED) VERIFY V82E (ORBIT) 3 RNDZ RDR LOCKED ON IN MODE II 4 LGC AT FLASHING VERB 37 5 PROPER INITIAL W MATRIX LOADED IN LGC
GUID CONT-PGNS ATTITUDE MON-PGNS(CDR) RATE ERR MON-CMPTR(LMP) ATTITUDE MON-AGS(LMP) SHFTTRUN-+5 DEG X-POINTER-HI MULT RADAR TEST SW-OFF ENG ARM-OFF X-TRANSL-2JETS DEAD BAND-MIN PGNS MODE CONT-AUTO THROTJET-JET CBPGNS IMU OPR-CLOSE RR MODE-LGC TTCATRANSL-ENABLE(COR)
BAL CPL-ON MODE SEL-AGS
RNGALT MON-RNGRNGRT RATE ERR MON-RNDZ RORICOR) ATT CONT-PULSE(3)
AGS MODE CONT-ATT HOLD ACA4JET-DISABLE(CDRJ TTCATRANSL-DISABLE(LMP)
ACA4JET-DISABLE(LMPI
KEY ODE (PO0)
(DOWNLINK LM STATE VECTOR)
KEY V63E (RR SELF TEST)
4-4
F 04 12 00004 00001 PRO
F 16 72 TRUN SHFT PRO
F 16 78 R ROOT VERIFY TAPE METER WITH DSKY
+2 VERIFY INSERTION VELOCITY WITH RNDZ ROR WHERE RANGE = 2642 NM RANGE RATE = -4251 FPS
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
KEY V34E (TERMINATE) KEY V48E (LOAD DAP)
F 01 46 11002 PRO
F 06 47 LMWT CMWT PRO
KEY V56E (KILL AUTO TRACK ENABLE)
+3 KEY V41N72E (COARSE ALIGN RR) F 21 73 +000OOTRUN -077OOSHFT F 04 12 00006 00002 (CONTINUOUS DESIGNATE)
PRO 41 (COARSE ALIGN VERB)
KEY VI6N72E 16 72 MONITOR TRUNSHFT ANGLES
CB PGNS RNDZ RDR-OPEN CB AC BUS A RNDZ RDR-OPEN KEY V44E (TERMINATE RR DESIGNATE)
KEY V83E F 16 54 R ROOT THETA
SET ORDEAL PRO
CS HEATER AOT-CLOSE
CB AOT LAMP-CLOSE
+5 KEY V37E52E (IMU REALIGN)
4-5
410+1 CSI ROUTINE 373+02065 CS TIME 275+03028 TPI TIME
605400777 COTANGENT OF LOS TO-CSM 416+1 (ONE-HALF bRBITAL PERIOD) 411+0 RCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT 310R TIME TO CS
267R VELOCITY TO BE GAINED CSI
402R DELTA H
371R DELTA V CDH
372R _ DELTA T CSICDH
F 04 06 00001 00003 -(REFSMMAT) PRO -
F 50 25 00015 SELECT 1ST STAR ENTR
F 01 70 O02DE LOAD 1ST STAR PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FOAl ANGLES (AUTO MNVRI)
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVR)
F 01 71 002DE
KEY V76E PGNS MODE CONT-ATT HOLD
PRO +10 F 54 71 MARK 1ST STAR
PRO F 01 70 O02DE LOAD 2ND STAR
PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FDA ANGLES -(AUTO MNVRV
F 50 18 FDAI ANGLES (REQUEST PNVRt ENTR (BYPASS MNVR
F 01 71 002DE PGNS MODE CONT-ATT HOLD PRO
-35
4-6
+14 F 54 71 MARK 2ND STAR PRO
F 06 05 STAR ANGLE DIFFERENCE PRO
F 06 93 GYRO TORQUE ANGLES PRO
F 50 25 00014
PRO (CHECK ALIGNMENT IF TIME WILL PERMIT)
F 50 25 00015 SELECT 3RD STAR ENTR
F 01 70 OO2DE LOAD 3RD STAR PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FDAI ANGLES (AUTO MNVR)
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVR)
VERIFY ALIGNMENT VIA AOT
KEY V34E (TERMINATE) F 37 BB
V48E (LOAD DAP) F 01 46 11012
PRO F 06 47 LMWT CMWT
+17 PRO
CB AOT LAMP-OPEN
RESET ET (310R)
(12253) CB AC BUS A RNDZ RDR-CLOSE (WAIT 30 SEC) CB PGNS RNDZ RDR-CLOSE
RR MODE-LGC KEY V37E20E (ACQUIRE RADAR)
PGNS MODE CONT-AUTO F 50 18 FDA ANGLES (REQUEST MNVRJ
PRO (AUTO MNVR) 06 18 FDAI ANGLES (AUTO MNVR)
AGS MODE CONT-AUTO RATEERR MON-CMPTR (LMP)
F 50 18 FDAI ANGLES (REQUEST MNVR)
4-7
ENTR (BYPASS MNVR) NO TRK LT-OFF
F 50 72 RR TRUNSHFT VERIFY RR LOCK ON PRO
DSKY BLANKS
KEY V93E (BEFORE 1ST MARK REINIT W MATRIXI KEY V80E (UPDATE LM SV)
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (i20OOZOO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
400+3 AGS ALIGNshy400R (00000 COMPLETE) 507+0 Z-AXIS BORESIGHT 400+2 ACQUISITION STEERING
CS
(122amp55) KEY V37E32E (CSI)
F 06 11 1 S LOAD TIG CSI FROM DATA PAD (NOM 123S26- 271 PRO
F 06 55 +O000IN +02660E +13000 OMEGAT (CDH 180 DEG AFTER CSI PRO
F 06 37 LOAD TIG TPI FROM DATA PAD (NOM 1251021761 PRO
F 16 45 MKS TFI -00001
-30 COPY RDOT FOR 1ST CSI BU
31OR TIME TO CSI
267R VELOCITY TO BE GAINED CSI
402R DELTA H
371R DELTA V CDH
-22
4-8
372R _ DELTA T CSICDH
KEY V32E (MARKS=5
F 06 75 DELTA H DELTA T CSICDH DELTA T CDHTPI PRO
F 06 81 DELTA VOS-LV (CS) (NOM 501 DELTA VX)
CSI(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (CDH)
(NOM 60 DELTA VX) CDH(82)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
KEY V32E (MARKS=1C)
F 06 75 DELTA H DELTA TCSICDH DELTA TCDHTPI PRD
F 06 81 DELTA VS-LV (CSI) CSI(N811
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 82 DELTA VIS-LV(CDH)
CDH(82)
DELTA VX(LVI
DELTA VY(LV)
DELTA VZ(LV)
-12
4-9
-20 COPY RDOT FOR 2ND CSI BU
F 16 45
F 06 75
F 06 81
F 06 16
F 06 90
PRO MKS TFI -00001
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS NON SEL - PRPLNT A + B TEMP IND 40DEG TO lOODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + 8 PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4v 2 3 (120 - 190 DEG F
(LOS OF MSFN ) S-BAND - SLEW TO P = +90 Y a 0 S-BAND - FWD (OR AFT) S-BAND - DN VOICE BU BIOMED OFF
PRO (FINAL COMP)
267R - VELOCITY TO BE GAINED CSI
402R DELTA H
372R TIME CSICDHL
371R PREDICTED VEL TO BE GAINED CDH
263R OUT-OF-PLANE
DELTA H DELTA TCSICDH DELTA TCDHTPI PRO DELTA VS-LV (CSI)
KEY V9OE (OUT-OF-PLANED
0 LOAD TIG CSI FROM DATA PAD (NOM 12302627) PRO Y YDOT PSI
N90 CSM
YDOT
PRO
-7
4-10
F 06 81 DELTA VS-LV(CSI)
COPY YDOT FROM CSM AND LOAD NEGATIVE IN R2 CSIIN81I
DELTA VX(LV)
DELTA VYILV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (COH)
CDH(82)
DELTA VX(LV)
- DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RANGE AND RDOT FOR 3RD CS BU
COMPUTE CSI BU
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (i2000OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
(TRANSMIT CSI DATA TO CSMI VHF A XMTR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF TELEMETY PCM - LO
KEY VB3E F 16 54 R ROOT THETA
SET ORDEAL PRO
317R RANGE
440R RANGE RATE
4-11
400+3 AGS ALIGN t40OR (00000 COMPLETE)
277R THETA
PRO F 37 BB
-6 KEY 41E (RCS THRUSTING) F 50 18 FDAI-ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTAV 400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTAV 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA RF
TRANSMIT TGT DELTA VS TO CSM AND SYNC COUNTDOWN
16 85 DELTA VS-BODY
502R DELTA VZ (NOM 5Ql)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTAVS-BODY
(123t26t27) BURN +Z
NULL DELTA VS
4-12
VERIFY AGS RESIDUALS 50OR 501R 502R DELTA VX _ DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
CDH
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
KEY V67E (RESET W MATRIX) F 06 99 +0200E +O0020E +00005E
PRO
507+0 Z-AXIS BORESIGHT
(VHF RANGING WITH CSM) VHF A XMTR - VOICERNG VHF B XMTR - OFF VHF B RCVR - ON TELEMETRY PCM - HI
(12331) KEY V37E33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 a TIG CDH (NOM 1242425) -120 amp00 10 (AGS 0 TIME)
(CONVERT TO MINUTES)
411+0 THRUST ALONG Z-BODY AXIS ENTER IF YOU DONT TARGET CSI
373R (NOM 26443 310R TIME TO CDH
4-13
423R DESIRED ALT RATE AT CDH
402R DELTA Hshy
450R DELTA VX
452R DELTA VZ
623+0 Z-AXIS PARALLEL TO CSM PLANE
IPRO F 16 45 MKS TFI -00001
-52 RESET ET
KEY V93E (REINIT W MATRIX WHEN MARKS =4)
KEY V32E (MARKS = 3)
F 06 75 DELTA HCDH DELTA TCDHTPI DELTA TTPI PRO
F 06 81 DELTA VCDH-LV CDH(N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
-47 KEY VSOE (OUT-OF-PLANE)
_ TIG CDH (NOM 124t24t25) -3000 TIME FROM CDH
F 06 16 l1 LOAD TIG PLANE CHANGE (NOM 123amp54-253 PRO
F 06 90 Y YDOT PSI N90 CSM
VYDOT PRO
-42 KEY V32E (MARKS=1O)
F 06 75 DELTA HCDH DELTA TCDIHTPI DELTA TTPITPI PRO
F 06 81 DELTA VCDH-LV
4-14
CDH (NS1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -OO1
KEY V34E (TERMINATE) F 37 B8
PLANE CHANGE
KEY 30E (EXTERNAL DELTA V)
TIG CDH (NOM 124124t25) -3000 TIME FROM CDH
F 06 33 LOAD TIG PLANE CHANGE (NOM 123154T25) PRO
F 06 81 DELTA VS-LV (NOM 00)
-36 COPY RDOT FOR 1ST CDH BU
KEY V90E (OUT-OF-PLANE)
F 06 16 1 1 LOAD TIG PLANE CHANGE (NOM 1231543251 PRO
F 06 90 Y YOOT PSI N90 CSM
YDOT
PRO
F 06 81 DELTA VS-LV(NOM 00)
COPY YDOT AND LOAD NEGATIVE IN R2 PRO
F 06 42 HA HP DELTA V PRO
F 16 45 MKS TFI MGA
PRO
F 37 BB
KEY 41E (RCS THRUSTING)
-30
4-15
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVRI
410+5 EXTERNAL DELTA V 450+0 451-YDOT 452+0 (LOAD CSM -YDOT)
407+0 ROTATE EXTERNAL DELTA V RF
16 95 DELTA VS-BODY
-3035 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATTVHOLD 407+1 FREEZE EXTERNAL DELTAV
F 16 85 DELTA VS-BODY -
NULL DELTA VIS
PRO F 37BB
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
507+0 Z-AXIS BORESIGHT
(12356) KEY 33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 TIG CDH (NOM 124t24t25) -120 OO ZOO (AGS 0 TIME)
(CONVERT TO MINUTES)
373R _ (NOM 2644) 310R TIME TO CDH
423R DESIRED ALT RATE AT CDH
(ADS OF MSFN) S-BAND - SLEW TOP = ACQUIRE HGA LOCK ON VOICE - BUVOICE -- VOICE VERIFY VOICE TLM BIOMED - LEFT (OR RIGHT)
402R DELTAH
4-16
F 16 45
-25
-23
F 06 75
F 06 81
F 16 45
-12
F 06 75
F 06 81
450R DELTA VX
452R DELTA VZ
PRO MKS TFI -00001
KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
COPY ROOT FOR 2ND CDH BU
KEY v32E (MARKS = 5)
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40DEG TO 1OODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + B PRESS IND PSIA
A QUANTITY IND _ PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING a TEMP MON SEL RCS QUAD 1 4 2 3 (120 - 190 DEG F)i
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
CDH(NB1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO MKS TFI -00001
PRO (FINAL COMP)
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
KEY V9OE (OUT-OF-PLANE)
-7
4-17
F 06 16 jj LOAD TIG CDH FROM DATA PAD (NOM 12424251 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT PRO
COPY YOOT FROM CSM AND LOAD NEGATIVE IN R2
CDH(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RDOT FOR 3RD CDH BU
COMPUTE CDH BU
TRANSMIT TGT DELTA VOS TO CSM AND SYNC COUNTDOWN
KEY V47E (INITIALIZE AGS F 06 16 GET OF AGS 0 TIME 120O00OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
KEY V83E F 16 54 R RDOT THETA
SET ORDEAL PRO
317R _ RANGE
440R RANGE RATE 400+3 AGS ALIGN 40OR (00000 COMPLETE)
277R THETA
-6
4-18
PRO F 3 BB
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY V06N86E F 06 86 DELTA VIS-LV
AGS(N86) CHART
DELTA VX(LVD
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
16 85 DELTA VS-BODY
50OR DELTA VX (NOM -0O3)
502R DELTA VZ (NOM 60)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD 407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS BODY
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS 5OOR 50IR 502R DELTA VX -DELTA VY DELTA VZ-
VERIFY PGNS RESIDUALS N85
DELTA VX(LM)
4-19
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
TPI
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO 507+0 Z-AXIS BORESIGHT
(12426) KEY 34E (TPI)
-36 RESET ET
F 06 37 - amp LOAD TIG TPI FROM DATA PAD (NOM 1250246) PRO
F 06 55 +00000 +02660E +13000 OMEGAT PRO
F 16 45 MARKS TFI -00001
-32 KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
-29 KEY V32E (MARKS = 3)
F 06 37 __ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
RESET ET
410+3 TPI SEARCH ROUTINE 307+04300 DELTA T TRANSFER
4-20
-26 310+02600 TFI TPI
303R THETA AT TPI
267R DELTA VTPI
371R DELTA VTPI + DELTA VTPF
KEY V32E (MARKS = 10)
F 06 37 _ _ _ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VIS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
TEMPIPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40ODEG TO IGODEG F A + B PRESS IND 181 +-3 PSIA
TEMPIPRESS MON SEL - HEL
A + B PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD I 4 2 3 (120 - 190 DEG F)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
RESET ET
-13 310+01300 TFI TPI
303R THETA AT TPI
-12 PRO (FINAL COMP) F 06 37 Z TIG TPIj__
4-21
TRANSMIT TIG OF TPI TO CSM-
PRO F 06 58 HP DELTA VTPI DELTA VTRF
PRO F 06 81 DELTA VS-LV
KEY V9OE (OUT-OF-PLANE)
F 06 16 1 LOAD TIG TPI FROM DATA PAD (NOM 12502461 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT
PRO F 06 81 DELTA VS-LV
COPY CSM YDOT AND LOAD NEGATIVE IN R2 N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 59 DELTA VS LOS
N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI MGA
RESET ET
PRO F 37 BB
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (12000t600)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE)
-10
-6
4-22
F 50 16 DOWNLINK COMPLETE PRO (UPDATE COMPLETE)
400+3 AGS ALIGN 400R (00000 COMPLETE)
-9 277R COPY TGT LOS ANGLE
310+00800
303R THETA AT TPI 410+4 DIRECT TRANSFER AT ET=-8 404+0 405+0 406+0 (MONITOR 470 471 4721
373R TIG TPI
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
KEY 41E (RCS THRUSTING) F 50 18 FOAl ANGLES (REQUEST MNVRI
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
-5 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUS
400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
COMPUTE TPI BU
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
4-23
1685 DELTA VS-BODY
50OR DELTA VX(NOM -115)
502R DELTA VZ(NOM 229)
-Z35 OSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS-BODY
(1250246) BURN +Z
VERIFY AGS RESIDUALS 500R 501R 502R DELTAVX DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
MCC1
KEY V76E (PGNS PULSE) PGNSMODECONT-AUTO
KEY V93E (BEFORE 1ST MARK REINITW MATRIX)
+2 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
4-24
(LOS OF MSFN) S-BAND - SLEW TO P = 90 Y = 0 S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
404+0 405+0 406+0
(MONITOR 470 471 4721
+9 277R COPY TGT LOS ANGLE
+12 PRO (COMPUTE MCC FOR TPI+15I F 06 81 DELTA VS-LV
PRO F 06 59 DELTA VS-LOS
PRO F 16 45 MKS TFI MGA
+13 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUOS
COMPUTE MCC1 BU
PRO F 37 BB
+14 KEY 41E (RCS THRUSTING) F 50 18 FOAL ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+1425 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+15 F 16 85 NULL DELTA VS
PRO F 37 BB
MCC2
KEY V76E (PGNS PULSE)
4-25
PGNS MODE CONT-AUTO
KEY V93E (BEFORE 1ST MARK REINIT W MATRIX)
+16 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
404+0 405+0 406+0 (MONITOR 470 471 47)shy
+24 277R COPY TGT LOS ANGLE
+27 PRO (COMPUTE MCC FORTPI+30) F 06 81 DELTA VS-LV
PRO F 06 59 DELIA VPS-LOS
PRO F 16 45 MKS TFI MGA
+28 277R COPY TGT LOS ANGLE
COPY R RDOT FROM TAPEMETER FOR BUS
COMPUTE MCC2 BU
F 37 BB PRO
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+2925 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+30 F 16 85 NULL DELTA VS
PRO F 37 BB
KEY OOE (P001
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
4-26
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT KEY V34E (TERMINATE)
KEY V37E47E (AVE G) F 16 83 DELTA VIS
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT VERIFY TAPE METER WITH DSKY
BRAKING GATE 30 FPS - 6000 FT 20 FPS - 3000 FT 10 FPS - 1500 FT 5 FPS - 600 FT
RENDEZVOUS
STATION KEEPING
5-1
50 ABORT PROCEDURE
This is a specific AGS nominal abort procedure due to a PGNS failure between insertion and station keeping
51
5-2
Nominal AGS Procedures
ASSUMPTIONS
AFTER INSERTION
I INSERTION COMPLETE (RFSIDUALS NULLED) g PGNS FAILURE BEFORE INSERTION 3 RAUAR NOT LOCKED ON
(UI CoNT-AGS ATlI[uUE MON-AGS(CDR) RATE ERR MON-CNPTR(LMP) ATTITUDE MON-AGS(LMP) SHFITRUN-+5 DEG X-POINTER-HI MULT RADAR IEST Sw-OFF LNb GMbL-OFF ENG ARM-OFF X-IRANSL-2 JETS DEAD BAND-MAX PGNS MODE CONT-OFF THROTJET-JET CB IMU OIR-ON HH MOVE-AUTO rRACK TTCATNANSL-ENABLE(CDR)
AL CPL-ON MODE SL-AGS RNGAL1 MON-RNbRNGRT RAIE ERR MON-RNDZ HDR(CDR) AVl CoNT(3)-PULSE AGS MODE CONT-AUTO ACA4JET-DISABLE(CDR) TTCATRANSL-DISABLE(LMP) ACA4JET-DISABLE(LMP)
bO7+U Z-AXIS BOPESIGHT 400+2 Z-AXIS STEERING PULSE TO NULL AGS ERRORS POINT Z-AXIS IN DIRECTION OF CSM MODE CONT-ATT HOLD ATT CONT(3)-MODE CONTROL O unnr - ZirF
5-3
SLEW PATE - LO
SLEW RR ANT TO OqON FUAI VERIFY MAX SIGNAL STRENGTH RH MOOE-AUTO TRACK NO TRACK LIGHT OFF -
ATT CONT(3h-PULSE
CHECK INSERTION VELOCITY WITH TAPEMETER COMPARE EAPEMETER WITH AGS STATE VECTOR DATA I
17R RANGE(NOM 2642)
440R RANGE RATE(NOM -425l)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
cSI
+3 417+1 (RADAR FILTER INITIALIZED) 41b+l (NO BOHESIGHT) b03-XXXXX RANGE RATE
+5 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGF
41b+1 CSI ROUTINE 373+o2065 CSi TIME 275+03028 TPI TIME 605+0077 COTANGENT OF LOS TO CSM 41b+1 (ONE-HALF OFBITAL-PERIOD) 411+0 HCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT
610R TIME TO CST
43 RESET ET
267R VELOCITY TO BE GAINED CSI
402R FLTA H
371R DFLTA V CDH
5-4
372R DFLTA T CSICDH
-42 415+1 (No BORESIGHT) bO6-xXXXX RANGE RATE
-40 415+1 (NO BORESIGHT)503-XXXXX RANGE RATE dORESIGHT ON CSM
415+1 316+XXXXX RANGE
-37 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE
-15 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE UORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-2 415+1 (No BOHESIGHT) bO3-XXXXX RANGF RATE
i1uR TIME TO CS
RESEF ET
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-30 COPY ROOT FOR 1ST CSI 81J
BORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-t7 415+1 (NO BORFSIGHT) 50-XXxXx RANGF RATE
267R VELOCITY TO HE GAINED CSI
402R LELTA H
371R OFLTA V COH
372R OELTA T CSICDH
-5 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 blb+XXXXX RANGE
-i2 415+1 (No BORESIGHT) 5n3-XXXXX RANGE RATE
415+1 (NO BORESIGHT)
5-5
503-XXXXX RANGF RATE
COPY Roor FOR 2NO CSI BU
bORESIGHT ON CSM 415+1 316+XXXXX RANGE
TEMPPRESS MON SEL - FUEL MAN
A AND 8 PRESS 181 +-3 PIG TEMPPRESS MON SEL - PRPLNT
A AND B TEMP IND 4ODEG 0 IOODEG F A AND B PRFSS IND 181 +-3 PSIA
tEMPPRESS MON SEL - HEL
A AND 8 PRESS IND PSIA
A QUANTITY IND- -- PERCENT RFMAINING
8 QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4p 2 3 (120 - 190 DFG F)
415+1 (NO BORESIGHT)-17 503-XXXXX RANGE RATE
-15 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
(LOS OF MSFN) S-BAND - SLEW 10 P = +90t Y U S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
-12 415+1 (No 8ORESIGHT)
503-XXXXX RANGE RATE
267R VFLOCITY TU BE GAINED CSI
402R OFLTA H
372R TIME CSICH
371R PREDICTED VEL 10 RE GAINED COH
263R OLT-OF-PLANE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATL
-10 COPY RANGE AND ROOT FOR 3RD CSI 8U
SORESIGH ON CSM 41b+1
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
MISSION G LUNAR ORBIT RENDEZVOUS ATTITUDE TIME HISTORY
OFOR THE LM P33
P20 123+31) (021880)
LMI CSI NrxNMARKS i (123+26+27)
FINAL -
COMP(I123+1l6)
P32 LANDING SITEj P20 30ES (122+50) CSM AT (04650) PRIME MERIDIAN LIFT-OFF
P52 (122+28+11) (122+40)DIRECTION OF (03640)ORBITAL MOTION IS
CLOCKWISE
(18012150)I NERTIAL YAWKLINERTIAL PITCH
ORDEAL PITCH EARTHINERTIAL ROLL
FIGURE 2-2
MISSION G LUNAR ORBIT RENDEZVOUS ATTITUDE TIME HISTORY
FOR THE LM
LM TPF (126+00+00) (01302920)
LM LMC2PLANE CHANGELMPI+30) (123+54+25)
(TPI+30) (0560)(0782400) 7 SUN
P20
(TPI+15) P3
P33(0532480) COMP
---- _ (124+12--- ---
LM TPI (125+02+46) L D (026 627650) (124+24+25)
(0980)
FINAL
DIRECTION OF COMP ORBITAL MOTION IS (124+50)
CLOCKWISE
(18012150)
LL INERTIAL YAW NERTIAL PITCH
ORDEAL PITCH EARTH INERTIAL ROLL
FIGURE 2-3
3-1
30 DISCUSSION OF MAJOR EVENTS
31 Concentric Sequence Initiation
Immediately following Insertion the LM navigated vector will be downlinked to Mission Control Center-Houston this state vector is then uplinked to the CSM The LM commander will perform a Proqram 52 fine alignment to REFSMMAT at approxishymately 12240
The digital autopilot is configured to wide deadband Program P20 is called and an automatic pitch maneuver is initiated to the preferred track attitude At 122 55 CSI targeting parameters are loaded in the PGNS and AGS A period of rendezvous radar marking will then take place from 122-57 to 12315 Upon completion of tracking the LM will obtain an out-of-plane velocity from the CSM to be vectored with the in-plane component of the CSI delta V The CSMs estishymate of out-of-plane velocity is alleged to be better than the LMs estimate (Reference 74)
At approximately 123 20 the LM will voice its CSI solution to the CSM the AGS is updated aligned and targeted in external delta-V with the CDH solution to be excuted Program P41 will then be called and the automatic pitch maneuver bypassed since the burn isto be executed with Z-Axis thrusting The CSI burn occurs nominally at 123 26 27 After verification of the LM CSI burn the CSM will incorporate the LM burn parameters in its CMC LM state vector
32 Constant Delta Height and Plane Change
At 12330 approximately three minutes after the LM CSI burn the W matrix will be set to (200025) and the LM targeting paramters are loaded in both the PGNS and AGS for the CDH maneuver Out-of-plane velocity will then be computed and voiced to the LM from the CSM Program P30 is loaded with the targeting parameters for the LM Plane Change maneuver which will be accomplished in Program P41 30 minutes prior to the CDH maneuver Following the burn the target delta V parameters are voice to the CSM and incorporated into the CMC LM state vector At 12356 the CDH targeting parameters are loaded in both the PGNS and AGS for 1242425 A CDH chart solution is calculated 7 minutes prior to TIG The AGS is updated aligned and targeted in external delta V with the CDH solution to be executed The RCS Thrust Program P41 is called at 12418 and the burn attitude is bypassed since the LM executes CDH by thrusting out individual components of delta V while maintaining radar lock-on
3-2
3 3 Terminal Phase Initiation
Radar tracking is initiated after the CDH maneuver and updating of the LGC continued At 12426 approximately two minutes after the LM CDH burn targeting parameters are loaded in both the PGNS and AGS for the TPI maneuver which will be targeted for a node at intercept Backup measurements are made at the appropriate times The AGS is updated aligned and targeted in external delta V with the TPI solution to be executed The RCS Thrust Program P41 is called at 12456 and the burn attitude is bypassed since the LM is burning along the plus Z-axis with the thrust direction established with the COAS
3 4 Midcourse Corrections
Immediately after TPI the Midcourse Prethrust Program P35 will be called and radar tracking reinitiated Backup measshyurements are made and midcourse corrections chart solutions obtained The MCCl burn will nominally be performed at TPI plus 15 minutes (1251746) If MCCI is to be excuted Program P41 will be called and the burn attitude maneuver is bypassed since the plus Z-axis will remain boresighted at the CSM until docking
Following MCCI Program P35 will be called and targeted for MCC2 at TPI plus 30 minutes (1253246) and executed identishycally to MCCI
3 5 Braking
In preparation for braking the DAP is configured in narrow deadband Program P20 is terminated at 18000 feet but the radar is kept in auto track to provide radar range and range rate displayed on the tapemeter Average G is called by Program P47 prior to braking and attitude hold is selected The braking schedule is followed as contained in Section 4
4-1
40 NOMINAL MISSION PROCEDURES
The procedures included in this section do not specify which crewmember Commander or LM Pilot performs each task These need not be specified since the following basic rules define which crewmember performs each task
41 Commander Tasks
1 All attitude changes whether manual or automatic will be accomplished by the CDR
2 The operation of the DSKY during thrust programs (P40 P41 P42 P47) will be done by the CDR Actual manipulation of the TTCA need not be always done by the CDR but in most cases will be
3 Operation of the rendezvous and landing radar will be done by the CDR
4 The CDR will operate all other systems accessible to only his crew station
42 LM Pilot Tasks
1 AGS operation 2 DSKY operation will be done by the LMP except when keyboard
entries affect the control of spacecraft attitude or thrustshying
3 Backup data logging and chart calculations 4 All logging of maneuver solutions and systems performance 5 The LMP will operate all other systems accessible to only
his crew station
These general rules are guidelines only and may be deviated from by the LM crew if they develop more efficient Task assignments
43 ABBREVIATIONS
The abbreviations used herein are consistant with those in the AOH However in order to condense and simplify the procedures so that they are representative of onboard data a number of addshyitional shorthand conventions have been used To allow the unshyfamiliar reader to understand the procedures contained in this section the following explanations are included
1 AGS - A single asterisk is employed to denote those procedures involving operations to be performed on the DEDA The three number group following an asterisk specifies DEDA address An Rfollowing the address group indicates the address is to be read out A five digit group behind the Rindicates a nominal or expected display If the three number address group is followed by a plus or minus sign a data load is indicated When a single digit follows the plus addition of four zeros behind this digit is assumed Once used these conventions are easily handled and save considerable space
4-2
2 PGNS - The verb-noun addresses in the PGNS are indicated to the left of the procedures column An F is used to indicate a flashing display or absence of an F a static display To the right of the verb-noun on the same line are the contents of the three data registers If numeric quantities appear the DSKY should be correspondingly made to agree by executing a V21 V22 or V23 and performing a data load The procedure of blanking and loading registers is not included since it is repeated often and is highly familiar to the crews
EXAMPLE F 06 33 125-02 46 TIG OF TPI
Expanded this means Load flashing verb 06 noun 33 with the quantity 125 hours 2 minutes and 46 seconds the time of ignition of the RCS engine TPI maneuver Procedurally this is done by keying verb 25 enter loading +000125 in register 1 +00002 in register 2 and +04600 in register 3
If numberic quantities do not follow the verb-noun it is indicated that a computed or information quantity is being displayed via the DSKY If nominal values are listed for possible comparison they appear in parentheses
EXAMPLE- F 06 42 HA HP V
Expanded this means Flashing verb 06 noun 42 has computed height of apogee in register 1 height of perigee in regshyister 2 and velocity to be gained in register 3
3 TIME - The numbers in the left hand column preceded by a plus or minus indicate event timer time referenced to an event Minus indicates event timer counting down to a future event Periodically this same column contains the nominal mission ground elapsed times in parentheses Asterisks following the event time indicate a time critical event which should be accomplished to the nearest second
4-3
4 4 Nominal PGNS Procedures
ASSUMPTIONS
AFTER INSERTION
1 INSERTION COMPLETE (RESIOUALS NULLED) VERIFY V82E (ORBIT) 3 RNDZ RDR LOCKED ON IN MODE II 4 LGC AT FLASHING VERB 37 5 PROPER INITIAL W MATRIX LOADED IN LGC
GUID CONT-PGNS ATTITUDE MON-PGNS(CDR) RATE ERR MON-CMPTR(LMP) ATTITUDE MON-AGS(LMP) SHFTTRUN-+5 DEG X-POINTER-HI MULT RADAR TEST SW-OFF ENG ARM-OFF X-TRANSL-2JETS DEAD BAND-MIN PGNS MODE CONT-AUTO THROTJET-JET CBPGNS IMU OPR-CLOSE RR MODE-LGC TTCATRANSL-ENABLE(COR)
BAL CPL-ON MODE SEL-AGS
RNGALT MON-RNGRNGRT RATE ERR MON-RNDZ RORICOR) ATT CONT-PULSE(3)
AGS MODE CONT-ATT HOLD ACA4JET-DISABLE(CDRJ TTCATRANSL-DISABLE(LMP)
ACA4JET-DISABLE(LMPI
KEY ODE (PO0)
(DOWNLINK LM STATE VECTOR)
KEY V63E (RR SELF TEST)
4-4
F 04 12 00004 00001 PRO
F 16 72 TRUN SHFT PRO
F 16 78 R ROOT VERIFY TAPE METER WITH DSKY
+2 VERIFY INSERTION VELOCITY WITH RNDZ ROR WHERE RANGE = 2642 NM RANGE RATE = -4251 FPS
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
KEY V34E (TERMINATE) KEY V48E (LOAD DAP)
F 01 46 11002 PRO
F 06 47 LMWT CMWT PRO
KEY V56E (KILL AUTO TRACK ENABLE)
+3 KEY V41N72E (COARSE ALIGN RR) F 21 73 +000OOTRUN -077OOSHFT F 04 12 00006 00002 (CONTINUOUS DESIGNATE)
PRO 41 (COARSE ALIGN VERB)
KEY VI6N72E 16 72 MONITOR TRUNSHFT ANGLES
CB PGNS RNDZ RDR-OPEN CB AC BUS A RNDZ RDR-OPEN KEY V44E (TERMINATE RR DESIGNATE)
KEY V83E F 16 54 R ROOT THETA
SET ORDEAL PRO
CS HEATER AOT-CLOSE
CB AOT LAMP-CLOSE
+5 KEY V37E52E (IMU REALIGN)
4-5
410+1 CSI ROUTINE 373+02065 CS TIME 275+03028 TPI TIME
605400777 COTANGENT OF LOS TO-CSM 416+1 (ONE-HALF bRBITAL PERIOD) 411+0 RCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT 310R TIME TO CS
267R VELOCITY TO BE GAINED CSI
402R DELTA H
371R DELTA V CDH
372R _ DELTA T CSICDH
F 04 06 00001 00003 -(REFSMMAT) PRO -
F 50 25 00015 SELECT 1ST STAR ENTR
F 01 70 O02DE LOAD 1ST STAR PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FOAl ANGLES (AUTO MNVRI)
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVR)
F 01 71 002DE
KEY V76E PGNS MODE CONT-ATT HOLD
PRO +10 F 54 71 MARK 1ST STAR
PRO F 01 70 O02DE LOAD 2ND STAR
PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FDA ANGLES -(AUTO MNVRV
F 50 18 FDAI ANGLES (REQUEST PNVRt ENTR (BYPASS MNVR
F 01 71 002DE PGNS MODE CONT-ATT HOLD PRO
-35
4-6
+14 F 54 71 MARK 2ND STAR PRO
F 06 05 STAR ANGLE DIFFERENCE PRO
F 06 93 GYRO TORQUE ANGLES PRO
F 50 25 00014
PRO (CHECK ALIGNMENT IF TIME WILL PERMIT)
F 50 25 00015 SELECT 3RD STAR ENTR
F 01 70 OO2DE LOAD 3RD STAR PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FDAI ANGLES (AUTO MNVR)
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVR)
VERIFY ALIGNMENT VIA AOT
KEY V34E (TERMINATE) F 37 BB
V48E (LOAD DAP) F 01 46 11012
PRO F 06 47 LMWT CMWT
+17 PRO
CB AOT LAMP-OPEN
RESET ET (310R)
(12253) CB AC BUS A RNDZ RDR-CLOSE (WAIT 30 SEC) CB PGNS RNDZ RDR-CLOSE
RR MODE-LGC KEY V37E20E (ACQUIRE RADAR)
PGNS MODE CONT-AUTO F 50 18 FDA ANGLES (REQUEST MNVRJ
PRO (AUTO MNVR) 06 18 FDAI ANGLES (AUTO MNVR)
AGS MODE CONT-AUTO RATEERR MON-CMPTR (LMP)
F 50 18 FDAI ANGLES (REQUEST MNVR)
4-7
ENTR (BYPASS MNVR) NO TRK LT-OFF
F 50 72 RR TRUNSHFT VERIFY RR LOCK ON PRO
DSKY BLANKS
KEY V93E (BEFORE 1ST MARK REINIT W MATRIXI KEY V80E (UPDATE LM SV)
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (i20OOZOO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
400+3 AGS ALIGNshy400R (00000 COMPLETE) 507+0 Z-AXIS BORESIGHT 400+2 ACQUISITION STEERING
CS
(122amp55) KEY V37E32E (CSI)
F 06 11 1 S LOAD TIG CSI FROM DATA PAD (NOM 123S26- 271 PRO
F 06 55 +O000IN +02660E +13000 OMEGAT (CDH 180 DEG AFTER CSI PRO
F 06 37 LOAD TIG TPI FROM DATA PAD (NOM 1251021761 PRO
F 16 45 MKS TFI -00001
-30 COPY RDOT FOR 1ST CSI BU
31OR TIME TO CSI
267R VELOCITY TO BE GAINED CSI
402R DELTA H
371R DELTA V CDH
-22
4-8
372R _ DELTA T CSICDH
KEY V32E (MARKS=5
F 06 75 DELTA H DELTA T CSICDH DELTA T CDHTPI PRO
F 06 81 DELTA VOS-LV (CS) (NOM 501 DELTA VX)
CSI(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (CDH)
(NOM 60 DELTA VX) CDH(82)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
KEY V32E (MARKS=1C)
F 06 75 DELTA H DELTA TCSICDH DELTA TCDHTPI PRD
F 06 81 DELTA VS-LV (CSI) CSI(N811
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 82 DELTA VIS-LV(CDH)
CDH(82)
DELTA VX(LVI
DELTA VY(LV)
DELTA VZ(LV)
-12
4-9
-20 COPY RDOT FOR 2ND CSI BU
F 16 45
F 06 75
F 06 81
F 06 16
F 06 90
PRO MKS TFI -00001
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS NON SEL - PRPLNT A + B TEMP IND 40DEG TO lOODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + 8 PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4v 2 3 (120 - 190 DEG F
(LOS OF MSFN ) S-BAND - SLEW TO P = +90 Y a 0 S-BAND - FWD (OR AFT) S-BAND - DN VOICE BU BIOMED OFF
PRO (FINAL COMP)
267R - VELOCITY TO BE GAINED CSI
402R DELTA H
372R TIME CSICDHL
371R PREDICTED VEL TO BE GAINED CDH
263R OUT-OF-PLANE
DELTA H DELTA TCSICDH DELTA TCDHTPI PRO DELTA VS-LV (CSI)
KEY V9OE (OUT-OF-PLANED
0 LOAD TIG CSI FROM DATA PAD (NOM 12302627) PRO Y YDOT PSI
N90 CSM
YDOT
PRO
-7
4-10
F 06 81 DELTA VS-LV(CSI)
COPY YDOT FROM CSM AND LOAD NEGATIVE IN R2 CSIIN81I
DELTA VX(LV)
DELTA VYILV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (COH)
CDH(82)
DELTA VX(LV)
- DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RANGE AND RDOT FOR 3RD CS BU
COMPUTE CSI BU
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (i2000OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
(TRANSMIT CSI DATA TO CSMI VHF A XMTR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF TELEMETY PCM - LO
KEY VB3E F 16 54 R ROOT THETA
SET ORDEAL PRO
317R RANGE
440R RANGE RATE
4-11
400+3 AGS ALIGN t40OR (00000 COMPLETE)
277R THETA
PRO F 37 BB
-6 KEY 41E (RCS THRUSTING) F 50 18 FDAI-ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTAV 400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTAV 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA RF
TRANSMIT TGT DELTA VS TO CSM AND SYNC COUNTDOWN
16 85 DELTA VS-BODY
502R DELTA VZ (NOM 5Ql)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTAVS-BODY
(123t26t27) BURN +Z
NULL DELTA VS
4-12
VERIFY AGS RESIDUALS 50OR 501R 502R DELTA VX _ DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
CDH
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
KEY V67E (RESET W MATRIX) F 06 99 +0200E +O0020E +00005E
PRO
507+0 Z-AXIS BORESIGHT
(VHF RANGING WITH CSM) VHF A XMTR - VOICERNG VHF B XMTR - OFF VHF B RCVR - ON TELEMETRY PCM - HI
(12331) KEY V37E33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 a TIG CDH (NOM 1242425) -120 amp00 10 (AGS 0 TIME)
(CONVERT TO MINUTES)
411+0 THRUST ALONG Z-BODY AXIS ENTER IF YOU DONT TARGET CSI
373R (NOM 26443 310R TIME TO CDH
4-13
423R DESIRED ALT RATE AT CDH
402R DELTA Hshy
450R DELTA VX
452R DELTA VZ
623+0 Z-AXIS PARALLEL TO CSM PLANE
IPRO F 16 45 MKS TFI -00001
-52 RESET ET
KEY V93E (REINIT W MATRIX WHEN MARKS =4)
KEY V32E (MARKS = 3)
F 06 75 DELTA HCDH DELTA TCDHTPI DELTA TTPI PRO
F 06 81 DELTA VCDH-LV CDH(N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
-47 KEY VSOE (OUT-OF-PLANE)
_ TIG CDH (NOM 124t24t25) -3000 TIME FROM CDH
F 06 16 l1 LOAD TIG PLANE CHANGE (NOM 123amp54-253 PRO
F 06 90 Y YDOT PSI N90 CSM
VYDOT PRO
-42 KEY V32E (MARKS=1O)
F 06 75 DELTA HCDH DELTA TCDIHTPI DELTA TTPITPI PRO
F 06 81 DELTA VCDH-LV
4-14
CDH (NS1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -OO1
KEY V34E (TERMINATE) F 37 B8
PLANE CHANGE
KEY 30E (EXTERNAL DELTA V)
TIG CDH (NOM 124124t25) -3000 TIME FROM CDH
F 06 33 LOAD TIG PLANE CHANGE (NOM 123154T25) PRO
F 06 81 DELTA VS-LV (NOM 00)
-36 COPY RDOT FOR 1ST CDH BU
KEY V90E (OUT-OF-PLANE)
F 06 16 1 1 LOAD TIG PLANE CHANGE (NOM 1231543251 PRO
F 06 90 Y YOOT PSI N90 CSM
YDOT
PRO
F 06 81 DELTA VS-LV(NOM 00)
COPY YDOT AND LOAD NEGATIVE IN R2 PRO
F 06 42 HA HP DELTA V PRO
F 16 45 MKS TFI MGA
PRO
F 37 BB
KEY 41E (RCS THRUSTING)
-30
4-15
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVRI
410+5 EXTERNAL DELTA V 450+0 451-YDOT 452+0 (LOAD CSM -YDOT)
407+0 ROTATE EXTERNAL DELTA V RF
16 95 DELTA VS-BODY
-3035 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATTVHOLD 407+1 FREEZE EXTERNAL DELTAV
F 16 85 DELTA VS-BODY -
NULL DELTA VIS
PRO F 37BB
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
507+0 Z-AXIS BORESIGHT
(12356) KEY 33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 TIG CDH (NOM 124t24t25) -120 OO ZOO (AGS 0 TIME)
(CONVERT TO MINUTES)
373R _ (NOM 2644) 310R TIME TO CDH
423R DESIRED ALT RATE AT CDH
(ADS OF MSFN) S-BAND - SLEW TOP = ACQUIRE HGA LOCK ON VOICE - BUVOICE -- VOICE VERIFY VOICE TLM BIOMED - LEFT (OR RIGHT)
402R DELTAH
4-16
F 16 45
-25
-23
F 06 75
F 06 81
F 16 45
-12
F 06 75
F 06 81
450R DELTA VX
452R DELTA VZ
PRO MKS TFI -00001
KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
COPY ROOT FOR 2ND CDH BU
KEY v32E (MARKS = 5)
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40DEG TO 1OODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + B PRESS IND PSIA
A QUANTITY IND _ PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING a TEMP MON SEL RCS QUAD 1 4 2 3 (120 - 190 DEG F)i
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
CDH(NB1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO MKS TFI -00001
PRO (FINAL COMP)
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
KEY V9OE (OUT-OF-PLANE)
-7
4-17
F 06 16 jj LOAD TIG CDH FROM DATA PAD (NOM 12424251 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT PRO
COPY YOOT FROM CSM AND LOAD NEGATIVE IN R2
CDH(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RDOT FOR 3RD CDH BU
COMPUTE CDH BU
TRANSMIT TGT DELTA VOS TO CSM AND SYNC COUNTDOWN
KEY V47E (INITIALIZE AGS F 06 16 GET OF AGS 0 TIME 120O00OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
KEY V83E F 16 54 R RDOT THETA
SET ORDEAL PRO
317R _ RANGE
440R RANGE RATE 400+3 AGS ALIGN 40OR (00000 COMPLETE)
277R THETA
-6
4-18
PRO F 3 BB
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY V06N86E F 06 86 DELTA VIS-LV
AGS(N86) CHART
DELTA VX(LVD
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
16 85 DELTA VS-BODY
50OR DELTA VX (NOM -0O3)
502R DELTA VZ (NOM 60)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD 407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS BODY
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS 5OOR 50IR 502R DELTA VX -DELTA VY DELTA VZ-
VERIFY PGNS RESIDUALS N85
DELTA VX(LM)
4-19
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
TPI
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO 507+0 Z-AXIS BORESIGHT
(12426) KEY 34E (TPI)
-36 RESET ET
F 06 37 - amp LOAD TIG TPI FROM DATA PAD (NOM 1250246) PRO
F 06 55 +00000 +02660E +13000 OMEGAT PRO
F 16 45 MARKS TFI -00001
-32 KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
-29 KEY V32E (MARKS = 3)
F 06 37 __ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
RESET ET
410+3 TPI SEARCH ROUTINE 307+04300 DELTA T TRANSFER
4-20
-26 310+02600 TFI TPI
303R THETA AT TPI
267R DELTA VTPI
371R DELTA VTPI + DELTA VTPF
KEY V32E (MARKS = 10)
F 06 37 _ _ _ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VIS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
TEMPIPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40ODEG TO IGODEG F A + B PRESS IND 181 +-3 PSIA
TEMPIPRESS MON SEL - HEL
A + B PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD I 4 2 3 (120 - 190 DEG F)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
RESET ET
-13 310+01300 TFI TPI
303R THETA AT TPI
-12 PRO (FINAL COMP) F 06 37 Z TIG TPIj__
4-21
TRANSMIT TIG OF TPI TO CSM-
PRO F 06 58 HP DELTA VTPI DELTA VTRF
PRO F 06 81 DELTA VS-LV
KEY V9OE (OUT-OF-PLANE)
F 06 16 1 LOAD TIG TPI FROM DATA PAD (NOM 12502461 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT
PRO F 06 81 DELTA VS-LV
COPY CSM YDOT AND LOAD NEGATIVE IN R2 N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 59 DELTA VS LOS
N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI MGA
RESET ET
PRO F 37 BB
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (12000t600)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE)
-10
-6
4-22
F 50 16 DOWNLINK COMPLETE PRO (UPDATE COMPLETE)
400+3 AGS ALIGN 400R (00000 COMPLETE)
-9 277R COPY TGT LOS ANGLE
310+00800
303R THETA AT TPI 410+4 DIRECT TRANSFER AT ET=-8 404+0 405+0 406+0 (MONITOR 470 471 4721
373R TIG TPI
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
KEY 41E (RCS THRUSTING) F 50 18 FOAl ANGLES (REQUEST MNVRI
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
-5 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUS
400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
COMPUTE TPI BU
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
4-23
1685 DELTA VS-BODY
50OR DELTA VX(NOM -115)
502R DELTA VZ(NOM 229)
-Z35 OSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS-BODY
(1250246) BURN +Z
VERIFY AGS RESIDUALS 500R 501R 502R DELTAVX DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
MCC1
KEY V76E (PGNS PULSE) PGNSMODECONT-AUTO
KEY V93E (BEFORE 1ST MARK REINITW MATRIX)
+2 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
4-24
(LOS OF MSFN) S-BAND - SLEW TO P = 90 Y = 0 S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
404+0 405+0 406+0
(MONITOR 470 471 4721
+9 277R COPY TGT LOS ANGLE
+12 PRO (COMPUTE MCC FOR TPI+15I F 06 81 DELTA VS-LV
PRO F 06 59 DELTA VS-LOS
PRO F 16 45 MKS TFI MGA
+13 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUOS
COMPUTE MCC1 BU
PRO F 37 BB
+14 KEY 41E (RCS THRUSTING) F 50 18 FOAL ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+1425 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+15 F 16 85 NULL DELTA VS
PRO F 37 BB
MCC2
KEY V76E (PGNS PULSE)
4-25
PGNS MODE CONT-AUTO
KEY V93E (BEFORE 1ST MARK REINIT W MATRIX)
+16 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
404+0 405+0 406+0 (MONITOR 470 471 47)shy
+24 277R COPY TGT LOS ANGLE
+27 PRO (COMPUTE MCC FORTPI+30) F 06 81 DELTA VS-LV
PRO F 06 59 DELIA VPS-LOS
PRO F 16 45 MKS TFI MGA
+28 277R COPY TGT LOS ANGLE
COPY R RDOT FROM TAPEMETER FOR BUS
COMPUTE MCC2 BU
F 37 BB PRO
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+2925 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+30 F 16 85 NULL DELTA VS
PRO F 37 BB
KEY OOE (P001
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
4-26
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT KEY V34E (TERMINATE)
KEY V37E47E (AVE G) F 16 83 DELTA VIS
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT VERIFY TAPE METER WITH DSKY
BRAKING GATE 30 FPS - 6000 FT 20 FPS - 3000 FT 10 FPS - 1500 FT 5 FPS - 600 FT
RENDEZVOUS
STATION KEEPING
5-1
50 ABORT PROCEDURE
This is a specific AGS nominal abort procedure due to a PGNS failure between insertion and station keeping
51
5-2
Nominal AGS Procedures
ASSUMPTIONS
AFTER INSERTION
I INSERTION COMPLETE (RFSIDUALS NULLED) g PGNS FAILURE BEFORE INSERTION 3 RAUAR NOT LOCKED ON
(UI CoNT-AGS ATlI[uUE MON-AGS(CDR) RATE ERR MON-CNPTR(LMP) ATTITUDE MON-AGS(LMP) SHFITRUN-+5 DEG X-POINTER-HI MULT RADAR IEST Sw-OFF LNb GMbL-OFF ENG ARM-OFF X-IRANSL-2 JETS DEAD BAND-MAX PGNS MODE CONT-OFF THROTJET-JET CB IMU OIR-ON HH MOVE-AUTO rRACK TTCATNANSL-ENABLE(CDR)
AL CPL-ON MODE SL-AGS RNGAL1 MON-RNbRNGRT RAIE ERR MON-RNDZ HDR(CDR) AVl CoNT(3)-PULSE AGS MODE CONT-AUTO ACA4JET-DISABLE(CDR) TTCATRANSL-DISABLE(LMP) ACA4JET-DISABLE(LMP)
bO7+U Z-AXIS BOPESIGHT 400+2 Z-AXIS STEERING PULSE TO NULL AGS ERRORS POINT Z-AXIS IN DIRECTION OF CSM MODE CONT-ATT HOLD ATT CONT(3)-MODE CONTROL O unnr - ZirF
5-3
SLEW PATE - LO
SLEW RR ANT TO OqON FUAI VERIFY MAX SIGNAL STRENGTH RH MOOE-AUTO TRACK NO TRACK LIGHT OFF -
ATT CONT(3h-PULSE
CHECK INSERTION VELOCITY WITH TAPEMETER COMPARE EAPEMETER WITH AGS STATE VECTOR DATA I
17R RANGE(NOM 2642)
440R RANGE RATE(NOM -425l)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
cSI
+3 417+1 (RADAR FILTER INITIALIZED) 41b+l (NO BOHESIGHT) b03-XXXXX RANGE RATE
+5 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGF
41b+1 CSI ROUTINE 373+o2065 CSi TIME 275+03028 TPI TIME 605+0077 COTANGENT OF LOS TO CSM 41b+1 (ONE-HALF OFBITAL-PERIOD) 411+0 HCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT
610R TIME TO CST
43 RESET ET
267R VELOCITY TO BE GAINED CSI
402R FLTA H
371R DFLTA V CDH
5-4
372R DFLTA T CSICDH
-42 415+1 (No BORESIGHT) bO6-xXXXX RANGE RATE
-40 415+1 (NO BORESIGHT)503-XXXXX RANGE RATE dORESIGHT ON CSM
415+1 316+XXXXX RANGE
-37 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE
-15 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE UORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-2 415+1 (No BOHESIGHT) bO3-XXXXX RANGF RATE
i1uR TIME TO CS
RESEF ET
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-30 COPY ROOT FOR 1ST CSI 81J
BORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-t7 415+1 (NO BORFSIGHT) 50-XXxXx RANGF RATE
267R VELOCITY TO HE GAINED CSI
402R LELTA H
371R OFLTA V COH
372R OELTA T CSICDH
-5 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 blb+XXXXX RANGE
-i2 415+1 (No BORESIGHT) 5n3-XXXXX RANGE RATE
415+1 (NO BORESIGHT)
5-5
503-XXXXX RANGF RATE
COPY Roor FOR 2NO CSI BU
bORESIGHT ON CSM 415+1 316+XXXXX RANGE
TEMPPRESS MON SEL - FUEL MAN
A AND 8 PRESS 181 +-3 PIG TEMPPRESS MON SEL - PRPLNT
A AND B TEMP IND 4ODEG 0 IOODEG F A AND B PRFSS IND 181 +-3 PSIA
tEMPPRESS MON SEL - HEL
A AND 8 PRESS IND PSIA
A QUANTITY IND- -- PERCENT RFMAINING
8 QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4p 2 3 (120 - 190 DFG F)
415+1 (NO BORESIGHT)-17 503-XXXXX RANGE RATE
-15 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
(LOS OF MSFN) S-BAND - SLEW 10 P = +90t Y U S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
-12 415+1 (No 8ORESIGHT)
503-XXXXX RANGE RATE
267R VFLOCITY TU BE GAINED CSI
402R OFLTA H
372R TIME CSICH
371R PREDICTED VEL 10 RE GAINED COH
263R OLT-OF-PLANE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATL
-10 COPY RANGE AND ROOT FOR 3RD CSI 8U
SORESIGH ON CSM 41b+1
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
MISSION G LUNAR ORBIT RENDEZVOUS ATTITUDE TIME HISTORY
FOR THE LM
LM TPF (126+00+00) (01302920)
LM LMC2PLANE CHANGELMPI+30) (123+54+25)
(TPI+30) (0560)(0782400) 7 SUN
P20
(TPI+15) P3
P33(0532480) COMP
---- _ (124+12--- ---
LM TPI (125+02+46) L D (026 627650) (124+24+25)
(0980)
FINAL
DIRECTION OF COMP ORBITAL MOTION IS (124+50)
CLOCKWISE
(18012150)
LL INERTIAL YAW NERTIAL PITCH
ORDEAL PITCH EARTH INERTIAL ROLL
FIGURE 2-3
3-1
30 DISCUSSION OF MAJOR EVENTS
31 Concentric Sequence Initiation
Immediately following Insertion the LM navigated vector will be downlinked to Mission Control Center-Houston this state vector is then uplinked to the CSM The LM commander will perform a Proqram 52 fine alignment to REFSMMAT at approxishymately 12240
The digital autopilot is configured to wide deadband Program P20 is called and an automatic pitch maneuver is initiated to the preferred track attitude At 122 55 CSI targeting parameters are loaded in the PGNS and AGS A period of rendezvous radar marking will then take place from 122-57 to 12315 Upon completion of tracking the LM will obtain an out-of-plane velocity from the CSM to be vectored with the in-plane component of the CSI delta V The CSMs estishymate of out-of-plane velocity is alleged to be better than the LMs estimate (Reference 74)
At approximately 123 20 the LM will voice its CSI solution to the CSM the AGS is updated aligned and targeted in external delta-V with the CDH solution to be excuted Program P41 will then be called and the automatic pitch maneuver bypassed since the burn isto be executed with Z-Axis thrusting The CSI burn occurs nominally at 123 26 27 After verification of the LM CSI burn the CSM will incorporate the LM burn parameters in its CMC LM state vector
32 Constant Delta Height and Plane Change
At 12330 approximately three minutes after the LM CSI burn the W matrix will be set to (200025) and the LM targeting paramters are loaded in both the PGNS and AGS for the CDH maneuver Out-of-plane velocity will then be computed and voiced to the LM from the CSM Program P30 is loaded with the targeting parameters for the LM Plane Change maneuver which will be accomplished in Program P41 30 minutes prior to the CDH maneuver Following the burn the target delta V parameters are voice to the CSM and incorporated into the CMC LM state vector At 12356 the CDH targeting parameters are loaded in both the PGNS and AGS for 1242425 A CDH chart solution is calculated 7 minutes prior to TIG The AGS is updated aligned and targeted in external delta V with the CDH solution to be executed The RCS Thrust Program P41 is called at 12418 and the burn attitude is bypassed since the LM executes CDH by thrusting out individual components of delta V while maintaining radar lock-on
3-2
3 3 Terminal Phase Initiation
Radar tracking is initiated after the CDH maneuver and updating of the LGC continued At 12426 approximately two minutes after the LM CDH burn targeting parameters are loaded in both the PGNS and AGS for the TPI maneuver which will be targeted for a node at intercept Backup measurements are made at the appropriate times The AGS is updated aligned and targeted in external delta V with the TPI solution to be executed The RCS Thrust Program P41 is called at 12456 and the burn attitude is bypassed since the LM is burning along the plus Z-axis with the thrust direction established with the COAS
3 4 Midcourse Corrections
Immediately after TPI the Midcourse Prethrust Program P35 will be called and radar tracking reinitiated Backup measshyurements are made and midcourse corrections chart solutions obtained The MCCl burn will nominally be performed at TPI plus 15 minutes (1251746) If MCCI is to be excuted Program P41 will be called and the burn attitude maneuver is bypassed since the plus Z-axis will remain boresighted at the CSM until docking
Following MCCI Program P35 will be called and targeted for MCC2 at TPI plus 30 minutes (1253246) and executed identishycally to MCCI
3 5 Braking
In preparation for braking the DAP is configured in narrow deadband Program P20 is terminated at 18000 feet but the radar is kept in auto track to provide radar range and range rate displayed on the tapemeter Average G is called by Program P47 prior to braking and attitude hold is selected The braking schedule is followed as contained in Section 4
4-1
40 NOMINAL MISSION PROCEDURES
The procedures included in this section do not specify which crewmember Commander or LM Pilot performs each task These need not be specified since the following basic rules define which crewmember performs each task
41 Commander Tasks
1 All attitude changes whether manual or automatic will be accomplished by the CDR
2 The operation of the DSKY during thrust programs (P40 P41 P42 P47) will be done by the CDR Actual manipulation of the TTCA need not be always done by the CDR but in most cases will be
3 Operation of the rendezvous and landing radar will be done by the CDR
4 The CDR will operate all other systems accessible to only his crew station
42 LM Pilot Tasks
1 AGS operation 2 DSKY operation will be done by the LMP except when keyboard
entries affect the control of spacecraft attitude or thrustshying
3 Backup data logging and chart calculations 4 All logging of maneuver solutions and systems performance 5 The LMP will operate all other systems accessible to only
his crew station
These general rules are guidelines only and may be deviated from by the LM crew if they develop more efficient Task assignments
43 ABBREVIATIONS
The abbreviations used herein are consistant with those in the AOH However in order to condense and simplify the procedures so that they are representative of onboard data a number of addshyitional shorthand conventions have been used To allow the unshyfamiliar reader to understand the procedures contained in this section the following explanations are included
1 AGS - A single asterisk is employed to denote those procedures involving operations to be performed on the DEDA The three number group following an asterisk specifies DEDA address An Rfollowing the address group indicates the address is to be read out A five digit group behind the Rindicates a nominal or expected display If the three number address group is followed by a plus or minus sign a data load is indicated When a single digit follows the plus addition of four zeros behind this digit is assumed Once used these conventions are easily handled and save considerable space
4-2
2 PGNS - The verb-noun addresses in the PGNS are indicated to the left of the procedures column An F is used to indicate a flashing display or absence of an F a static display To the right of the verb-noun on the same line are the contents of the three data registers If numeric quantities appear the DSKY should be correspondingly made to agree by executing a V21 V22 or V23 and performing a data load The procedure of blanking and loading registers is not included since it is repeated often and is highly familiar to the crews
EXAMPLE F 06 33 125-02 46 TIG OF TPI
Expanded this means Load flashing verb 06 noun 33 with the quantity 125 hours 2 minutes and 46 seconds the time of ignition of the RCS engine TPI maneuver Procedurally this is done by keying verb 25 enter loading +000125 in register 1 +00002 in register 2 and +04600 in register 3
If numberic quantities do not follow the verb-noun it is indicated that a computed or information quantity is being displayed via the DSKY If nominal values are listed for possible comparison they appear in parentheses
EXAMPLE- F 06 42 HA HP V
Expanded this means Flashing verb 06 noun 42 has computed height of apogee in register 1 height of perigee in regshyister 2 and velocity to be gained in register 3
3 TIME - The numbers in the left hand column preceded by a plus or minus indicate event timer time referenced to an event Minus indicates event timer counting down to a future event Periodically this same column contains the nominal mission ground elapsed times in parentheses Asterisks following the event time indicate a time critical event which should be accomplished to the nearest second
4-3
4 4 Nominal PGNS Procedures
ASSUMPTIONS
AFTER INSERTION
1 INSERTION COMPLETE (RESIOUALS NULLED) VERIFY V82E (ORBIT) 3 RNDZ RDR LOCKED ON IN MODE II 4 LGC AT FLASHING VERB 37 5 PROPER INITIAL W MATRIX LOADED IN LGC
GUID CONT-PGNS ATTITUDE MON-PGNS(CDR) RATE ERR MON-CMPTR(LMP) ATTITUDE MON-AGS(LMP) SHFTTRUN-+5 DEG X-POINTER-HI MULT RADAR TEST SW-OFF ENG ARM-OFF X-TRANSL-2JETS DEAD BAND-MIN PGNS MODE CONT-AUTO THROTJET-JET CBPGNS IMU OPR-CLOSE RR MODE-LGC TTCATRANSL-ENABLE(COR)
BAL CPL-ON MODE SEL-AGS
RNGALT MON-RNGRNGRT RATE ERR MON-RNDZ RORICOR) ATT CONT-PULSE(3)
AGS MODE CONT-ATT HOLD ACA4JET-DISABLE(CDRJ TTCATRANSL-DISABLE(LMP)
ACA4JET-DISABLE(LMPI
KEY ODE (PO0)
(DOWNLINK LM STATE VECTOR)
KEY V63E (RR SELF TEST)
4-4
F 04 12 00004 00001 PRO
F 16 72 TRUN SHFT PRO
F 16 78 R ROOT VERIFY TAPE METER WITH DSKY
+2 VERIFY INSERTION VELOCITY WITH RNDZ ROR WHERE RANGE = 2642 NM RANGE RATE = -4251 FPS
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
KEY V34E (TERMINATE) KEY V48E (LOAD DAP)
F 01 46 11002 PRO
F 06 47 LMWT CMWT PRO
KEY V56E (KILL AUTO TRACK ENABLE)
+3 KEY V41N72E (COARSE ALIGN RR) F 21 73 +000OOTRUN -077OOSHFT F 04 12 00006 00002 (CONTINUOUS DESIGNATE)
PRO 41 (COARSE ALIGN VERB)
KEY VI6N72E 16 72 MONITOR TRUNSHFT ANGLES
CB PGNS RNDZ RDR-OPEN CB AC BUS A RNDZ RDR-OPEN KEY V44E (TERMINATE RR DESIGNATE)
KEY V83E F 16 54 R ROOT THETA
SET ORDEAL PRO
CS HEATER AOT-CLOSE
CB AOT LAMP-CLOSE
+5 KEY V37E52E (IMU REALIGN)
4-5
410+1 CSI ROUTINE 373+02065 CS TIME 275+03028 TPI TIME
605400777 COTANGENT OF LOS TO-CSM 416+1 (ONE-HALF bRBITAL PERIOD) 411+0 RCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT 310R TIME TO CS
267R VELOCITY TO BE GAINED CSI
402R DELTA H
371R DELTA V CDH
372R _ DELTA T CSICDH
F 04 06 00001 00003 -(REFSMMAT) PRO -
F 50 25 00015 SELECT 1ST STAR ENTR
F 01 70 O02DE LOAD 1ST STAR PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FOAl ANGLES (AUTO MNVRI)
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVR)
F 01 71 002DE
KEY V76E PGNS MODE CONT-ATT HOLD
PRO +10 F 54 71 MARK 1ST STAR
PRO F 01 70 O02DE LOAD 2ND STAR
PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FDA ANGLES -(AUTO MNVRV
F 50 18 FDAI ANGLES (REQUEST PNVRt ENTR (BYPASS MNVR
F 01 71 002DE PGNS MODE CONT-ATT HOLD PRO
-35
4-6
+14 F 54 71 MARK 2ND STAR PRO
F 06 05 STAR ANGLE DIFFERENCE PRO
F 06 93 GYRO TORQUE ANGLES PRO
F 50 25 00014
PRO (CHECK ALIGNMENT IF TIME WILL PERMIT)
F 50 25 00015 SELECT 3RD STAR ENTR
F 01 70 OO2DE LOAD 3RD STAR PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FDAI ANGLES (AUTO MNVR)
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVR)
VERIFY ALIGNMENT VIA AOT
KEY V34E (TERMINATE) F 37 BB
V48E (LOAD DAP) F 01 46 11012
PRO F 06 47 LMWT CMWT
+17 PRO
CB AOT LAMP-OPEN
RESET ET (310R)
(12253) CB AC BUS A RNDZ RDR-CLOSE (WAIT 30 SEC) CB PGNS RNDZ RDR-CLOSE
RR MODE-LGC KEY V37E20E (ACQUIRE RADAR)
PGNS MODE CONT-AUTO F 50 18 FDA ANGLES (REQUEST MNVRJ
PRO (AUTO MNVR) 06 18 FDAI ANGLES (AUTO MNVR)
AGS MODE CONT-AUTO RATEERR MON-CMPTR (LMP)
F 50 18 FDAI ANGLES (REQUEST MNVR)
4-7
ENTR (BYPASS MNVR) NO TRK LT-OFF
F 50 72 RR TRUNSHFT VERIFY RR LOCK ON PRO
DSKY BLANKS
KEY V93E (BEFORE 1ST MARK REINIT W MATRIXI KEY V80E (UPDATE LM SV)
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (i20OOZOO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
400+3 AGS ALIGNshy400R (00000 COMPLETE) 507+0 Z-AXIS BORESIGHT 400+2 ACQUISITION STEERING
CS
(122amp55) KEY V37E32E (CSI)
F 06 11 1 S LOAD TIG CSI FROM DATA PAD (NOM 123S26- 271 PRO
F 06 55 +O000IN +02660E +13000 OMEGAT (CDH 180 DEG AFTER CSI PRO
F 06 37 LOAD TIG TPI FROM DATA PAD (NOM 1251021761 PRO
F 16 45 MKS TFI -00001
-30 COPY RDOT FOR 1ST CSI BU
31OR TIME TO CSI
267R VELOCITY TO BE GAINED CSI
402R DELTA H
371R DELTA V CDH
-22
4-8
372R _ DELTA T CSICDH
KEY V32E (MARKS=5
F 06 75 DELTA H DELTA T CSICDH DELTA T CDHTPI PRO
F 06 81 DELTA VOS-LV (CS) (NOM 501 DELTA VX)
CSI(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (CDH)
(NOM 60 DELTA VX) CDH(82)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
KEY V32E (MARKS=1C)
F 06 75 DELTA H DELTA TCSICDH DELTA TCDHTPI PRD
F 06 81 DELTA VS-LV (CSI) CSI(N811
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 82 DELTA VIS-LV(CDH)
CDH(82)
DELTA VX(LVI
DELTA VY(LV)
DELTA VZ(LV)
-12
4-9
-20 COPY RDOT FOR 2ND CSI BU
F 16 45
F 06 75
F 06 81
F 06 16
F 06 90
PRO MKS TFI -00001
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS NON SEL - PRPLNT A + B TEMP IND 40DEG TO lOODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + 8 PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4v 2 3 (120 - 190 DEG F
(LOS OF MSFN ) S-BAND - SLEW TO P = +90 Y a 0 S-BAND - FWD (OR AFT) S-BAND - DN VOICE BU BIOMED OFF
PRO (FINAL COMP)
267R - VELOCITY TO BE GAINED CSI
402R DELTA H
372R TIME CSICDHL
371R PREDICTED VEL TO BE GAINED CDH
263R OUT-OF-PLANE
DELTA H DELTA TCSICDH DELTA TCDHTPI PRO DELTA VS-LV (CSI)
KEY V9OE (OUT-OF-PLANED
0 LOAD TIG CSI FROM DATA PAD (NOM 12302627) PRO Y YDOT PSI
N90 CSM
YDOT
PRO
-7
4-10
F 06 81 DELTA VS-LV(CSI)
COPY YDOT FROM CSM AND LOAD NEGATIVE IN R2 CSIIN81I
DELTA VX(LV)
DELTA VYILV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (COH)
CDH(82)
DELTA VX(LV)
- DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RANGE AND RDOT FOR 3RD CS BU
COMPUTE CSI BU
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (i2000OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
(TRANSMIT CSI DATA TO CSMI VHF A XMTR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF TELEMETY PCM - LO
KEY VB3E F 16 54 R ROOT THETA
SET ORDEAL PRO
317R RANGE
440R RANGE RATE
4-11
400+3 AGS ALIGN t40OR (00000 COMPLETE)
277R THETA
PRO F 37 BB
-6 KEY 41E (RCS THRUSTING) F 50 18 FDAI-ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTAV 400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTAV 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA RF
TRANSMIT TGT DELTA VS TO CSM AND SYNC COUNTDOWN
16 85 DELTA VS-BODY
502R DELTA VZ (NOM 5Ql)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTAVS-BODY
(123t26t27) BURN +Z
NULL DELTA VS
4-12
VERIFY AGS RESIDUALS 50OR 501R 502R DELTA VX _ DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
CDH
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
KEY V67E (RESET W MATRIX) F 06 99 +0200E +O0020E +00005E
PRO
507+0 Z-AXIS BORESIGHT
(VHF RANGING WITH CSM) VHF A XMTR - VOICERNG VHF B XMTR - OFF VHF B RCVR - ON TELEMETRY PCM - HI
(12331) KEY V37E33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 a TIG CDH (NOM 1242425) -120 amp00 10 (AGS 0 TIME)
(CONVERT TO MINUTES)
411+0 THRUST ALONG Z-BODY AXIS ENTER IF YOU DONT TARGET CSI
373R (NOM 26443 310R TIME TO CDH
4-13
423R DESIRED ALT RATE AT CDH
402R DELTA Hshy
450R DELTA VX
452R DELTA VZ
623+0 Z-AXIS PARALLEL TO CSM PLANE
IPRO F 16 45 MKS TFI -00001
-52 RESET ET
KEY V93E (REINIT W MATRIX WHEN MARKS =4)
KEY V32E (MARKS = 3)
F 06 75 DELTA HCDH DELTA TCDHTPI DELTA TTPI PRO
F 06 81 DELTA VCDH-LV CDH(N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
-47 KEY VSOE (OUT-OF-PLANE)
_ TIG CDH (NOM 124t24t25) -3000 TIME FROM CDH
F 06 16 l1 LOAD TIG PLANE CHANGE (NOM 123amp54-253 PRO
F 06 90 Y YDOT PSI N90 CSM
VYDOT PRO
-42 KEY V32E (MARKS=1O)
F 06 75 DELTA HCDH DELTA TCDIHTPI DELTA TTPITPI PRO
F 06 81 DELTA VCDH-LV
4-14
CDH (NS1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -OO1
KEY V34E (TERMINATE) F 37 B8
PLANE CHANGE
KEY 30E (EXTERNAL DELTA V)
TIG CDH (NOM 124124t25) -3000 TIME FROM CDH
F 06 33 LOAD TIG PLANE CHANGE (NOM 123154T25) PRO
F 06 81 DELTA VS-LV (NOM 00)
-36 COPY RDOT FOR 1ST CDH BU
KEY V90E (OUT-OF-PLANE)
F 06 16 1 1 LOAD TIG PLANE CHANGE (NOM 1231543251 PRO
F 06 90 Y YOOT PSI N90 CSM
YDOT
PRO
F 06 81 DELTA VS-LV(NOM 00)
COPY YDOT AND LOAD NEGATIVE IN R2 PRO
F 06 42 HA HP DELTA V PRO
F 16 45 MKS TFI MGA
PRO
F 37 BB
KEY 41E (RCS THRUSTING)
-30
4-15
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVRI
410+5 EXTERNAL DELTA V 450+0 451-YDOT 452+0 (LOAD CSM -YDOT)
407+0 ROTATE EXTERNAL DELTA V RF
16 95 DELTA VS-BODY
-3035 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATTVHOLD 407+1 FREEZE EXTERNAL DELTAV
F 16 85 DELTA VS-BODY -
NULL DELTA VIS
PRO F 37BB
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
507+0 Z-AXIS BORESIGHT
(12356) KEY 33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 TIG CDH (NOM 124t24t25) -120 OO ZOO (AGS 0 TIME)
(CONVERT TO MINUTES)
373R _ (NOM 2644) 310R TIME TO CDH
423R DESIRED ALT RATE AT CDH
(ADS OF MSFN) S-BAND - SLEW TOP = ACQUIRE HGA LOCK ON VOICE - BUVOICE -- VOICE VERIFY VOICE TLM BIOMED - LEFT (OR RIGHT)
402R DELTAH
4-16
F 16 45
-25
-23
F 06 75
F 06 81
F 16 45
-12
F 06 75
F 06 81
450R DELTA VX
452R DELTA VZ
PRO MKS TFI -00001
KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
COPY ROOT FOR 2ND CDH BU
KEY v32E (MARKS = 5)
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40DEG TO 1OODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + B PRESS IND PSIA
A QUANTITY IND _ PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING a TEMP MON SEL RCS QUAD 1 4 2 3 (120 - 190 DEG F)i
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
CDH(NB1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO MKS TFI -00001
PRO (FINAL COMP)
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
KEY V9OE (OUT-OF-PLANE)
-7
4-17
F 06 16 jj LOAD TIG CDH FROM DATA PAD (NOM 12424251 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT PRO
COPY YOOT FROM CSM AND LOAD NEGATIVE IN R2
CDH(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RDOT FOR 3RD CDH BU
COMPUTE CDH BU
TRANSMIT TGT DELTA VOS TO CSM AND SYNC COUNTDOWN
KEY V47E (INITIALIZE AGS F 06 16 GET OF AGS 0 TIME 120O00OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
KEY V83E F 16 54 R RDOT THETA
SET ORDEAL PRO
317R _ RANGE
440R RANGE RATE 400+3 AGS ALIGN 40OR (00000 COMPLETE)
277R THETA
-6
4-18
PRO F 3 BB
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY V06N86E F 06 86 DELTA VIS-LV
AGS(N86) CHART
DELTA VX(LVD
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
16 85 DELTA VS-BODY
50OR DELTA VX (NOM -0O3)
502R DELTA VZ (NOM 60)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD 407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS BODY
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS 5OOR 50IR 502R DELTA VX -DELTA VY DELTA VZ-
VERIFY PGNS RESIDUALS N85
DELTA VX(LM)
4-19
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
TPI
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO 507+0 Z-AXIS BORESIGHT
(12426) KEY 34E (TPI)
-36 RESET ET
F 06 37 - amp LOAD TIG TPI FROM DATA PAD (NOM 1250246) PRO
F 06 55 +00000 +02660E +13000 OMEGAT PRO
F 16 45 MARKS TFI -00001
-32 KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
-29 KEY V32E (MARKS = 3)
F 06 37 __ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
RESET ET
410+3 TPI SEARCH ROUTINE 307+04300 DELTA T TRANSFER
4-20
-26 310+02600 TFI TPI
303R THETA AT TPI
267R DELTA VTPI
371R DELTA VTPI + DELTA VTPF
KEY V32E (MARKS = 10)
F 06 37 _ _ _ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VIS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
TEMPIPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40ODEG TO IGODEG F A + B PRESS IND 181 +-3 PSIA
TEMPIPRESS MON SEL - HEL
A + B PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD I 4 2 3 (120 - 190 DEG F)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
RESET ET
-13 310+01300 TFI TPI
303R THETA AT TPI
-12 PRO (FINAL COMP) F 06 37 Z TIG TPIj__
4-21
TRANSMIT TIG OF TPI TO CSM-
PRO F 06 58 HP DELTA VTPI DELTA VTRF
PRO F 06 81 DELTA VS-LV
KEY V9OE (OUT-OF-PLANE)
F 06 16 1 LOAD TIG TPI FROM DATA PAD (NOM 12502461 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT
PRO F 06 81 DELTA VS-LV
COPY CSM YDOT AND LOAD NEGATIVE IN R2 N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 59 DELTA VS LOS
N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI MGA
RESET ET
PRO F 37 BB
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (12000t600)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE)
-10
-6
4-22
F 50 16 DOWNLINK COMPLETE PRO (UPDATE COMPLETE)
400+3 AGS ALIGN 400R (00000 COMPLETE)
-9 277R COPY TGT LOS ANGLE
310+00800
303R THETA AT TPI 410+4 DIRECT TRANSFER AT ET=-8 404+0 405+0 406+0 (MONITOR 470 471 4721
373R TIG TPI
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
KEY 41E (RCS THRUSTING) F 50 18 FOAl ANGLES (REQUEST MNVRI
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
-5 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUS
400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
COMPUTE TPI BU
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
4-23
1685 DELTA VS-BODY
50OR DELTA VX(NOM -115)
502R DELTA VZ(NOM 229)
-Z35 OSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS-BODY
(1250246) BURN +Z
VERIFY AGS RESIDUALS 500R 501R 502R DELTAVX DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
MCC1
KEY V76E (PGNS PULSE) PGNSMODECONT-AUTO
KEY V93E (BEFORE 1ST MARK REINITW MATRIX)
+2 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
4-24
(LOS OF MSFN) S-BAND - SLEW TO P = 90 Y = 0 S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
404+0 405+0 406+0
(MONITOR 470 471 4721
+9 277R COPY TGT LOS ANGLE
+12 PRO (COMPUTE MCC FOR TPI+15I F 06 81 DELTA VS-LV
PRO F 06 59 DELTA VS-LOS
PRO F 16 45 MKS TFI MGA
+13 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUOS
COMPUTE MCC1 BU
PRO F 37 BB
+14 KEY 41E (RCS THRUSTING) F 50 18 FOAL ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+1425 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+15 F 16 85 NULL DELTA VS
PRO F 37 BB
MCC2
KEY V76E (PGNS PULSE)
4-25
PGNS MODE CONT-AUTO
KEY V93E (BEFORE 1ST MARK REINIT W MATRIX)
+16 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
404+0 405+0 406+0 (MONITOR 470 471 47)shy
+24 277R COPY TGT LOS ANGLE
+27 PRO (COMPUTE MCC FORTPI+30) F 06 81 DELTA VS-LV
PRO F 06 59 DELIA VPS-LOS
PRO F 16 45 MKS TFI MGA
+28 277R COPY TGT LOS ANGLE
COPY R RDOT FROM TAPEMETER FOR BUS
COMPUTE MCC2 BU
F 37 BB PRO
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+2925 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+30 F 16 85 NULL DELTA VS
PRO F 37 BB
KEY OOE (P001
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
4-26
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT KEY V34E (TERMINATE)
KEY V37E47E (AVE G) F 16 83 DELTA VIS
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT VERIFY TAPE METER WITH DSKY
BRAKING GATE 30 FPS - 6000 FT 20 FPS - 3000 FT 10 FPS - 1500 FT 5 FPS - 600 FT
RENDEZVOUS
STATION KEEPING
5-1
50 ABORT PROCEDURE
This is a specific AGS nominal abort procedure due to a PGNS failure between insertion and station keeping
51
5-2
Nominal AGS Procedures
ASSUMPTIONS
AFTER INSERTION
I INSERTION COMPLETE (RFSIDUALS NULLED) g PGNS FAILURE BEFORE INSERTION 3 RAUAR NOT LOCKED ON
(UI CoNT-AGS ATlI[uUE MON-AGS(CDR) RATE ERR MON-CNPTR(LMP) ATTITUDE MON-AGS(LMP) SHFITRUN-+5 DEG X-POINTER-HI MULT RADAR IEST Sw-OFF LNb GMbL-OFF ENG ARM-OFF X-IRANSL-2 JETS DEAD BAND-MAX PGNS MODE CONT-OFF THROTJET-JET CB IMU OIR-ON HH MOVE-AUTO rRACK TTCATNANSL-ENABLE(CDR)
AL CPL-ON MODE SL-AGS RNGAL1 MON-RNbRNGRT RAIE ERR MON-RNDZ HDR(CDR) AVl CoNT(3)-PULSE AGS MODE CONT-AUTO ACA4JET-DISABLE(CDR) TTCATRANSL-DISABLE(LMP) ACA4JET-DISABLE(LMP)
bO7+U Z-AXIS BOPESIGHT 400+2 Z-AXIS STEERING PULSE TO NULL AGS ERRORS POINT Z-AXIS IN DIRECTION OF CSM MODE CONT-ATT HOLD ATT CONT(3)-MODE CONTROL O unnr - ZirF
5-3
SLEW PATE - LO
SLEW RR ANT TO OqON FUAI VERIFY MAX SIGNAL STRENGTH RH MOOE-AUTO TRACK NO TRACK LIGHT OFF -
ATT CONT(3h-PULSE
CHECK INSERTION VELOCITY WITH TAPEMETER COMPARE EAPEMETER WITH AGS STATE VECTOR DATA I
17R RANGE(NOM 2642)
440R RANGE RATE(NOM -425l)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
cSI
+3 417+1 (RADAR FILTER INITIALIZED) 41b+l (NO BOHESIGHT) b03-XXXXX RANGE RATE
+5 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGF
41b+1 CSI ROUTINE 373+o2065 CSi TIME 275+03028 TPI TIME 605+0077 COTANGENT OF LOS TO CSM 41b+1 (ONE-HALF OFBITAL-PERIOD) 411+0 HCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT
610R TIME TO CST
43 RESET ET
267R VELOCITY TO BE GAINED CSI
402R FLTA H
371R DFLTA V CDH
5-4
372R DFLTA T CSICDH
-42 415+1 (No BORESIGHT) bO6-xXXXX RANGE RATE
-40 415+1 (NO BORESIGHT)503-XXXXX RANGE RATE dORESIGHT ON CSM
415+1 316+XXXXX RANGE
-37 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE
-15 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE UORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-2 415+1 (No BOHESIGHT) bO3-XXXXX RANGF RATE
i1uR TIME TO CS
RESEF ET
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-30 COPY ROOT FOR 1ST CSI 81J
BORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-t7 415+1 (NO BORFSIGHT) 50-XXxXx RANGF RATE
267R VELOCITY TO HE GAINED CSI
402R LELTA H
371R OFLTA V COH
372R OELTA T CSICDH
-5 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 blb+XXXXX RANGE
-i2 415+1 (No BORESIGHT) 5n3-XXXXX RANGE RATE
415+1 (NO BORESIGHT)
5-5
503-XXXXX RANGF RATE
COPY Roor FOR 2NO CSI BU
bORESIGHT ON CSM 415+1 316+XXXXX RANGE
TEMPPRESS MON SEL - FUEL MAN
A AND 8 PRESS 181 +-3 PIG TEMPPRESS MON SEL - PRPLNT
A AND B TEMP IND 4ODEG 0 IOODEG F A AND B PRFSS IND 181 +-3 PSIA
tEMPPRESS MON SEL - HEL
A AND 8 PRESS IND PSIA
A QUANTITY IND- -- PERCENT RFMAINING
8 QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4p 2 3 (120 - 190 DFG F)
415+1 (NO BORESIGHT)-17 503-XXXXX RANGE RATE
-15 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
(LOS OF MSFN) S-BAND - SLEW 10 P = +90t Y U S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
-12 415+1 (No 8ORESIGHT)
503-XXXXX RANGE RATE
267R VFLOCITY TU BE GAINED CSI
402R OFLTA H
372R TIME CSICH
371R PREDICTED VEL 10 RE GAINED COH
263R OLT-OF-PLANE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATL
-10 COPY RANGE AND ROOT FOR 3RD CSI 8U
SORESIGH ON CSM 41b+1
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
3-1
30 DISCUSSION OF MAJOR EVENTS
31 Concentric Sequence Initiation
Immediately following Insertion the LM navigated vector will be downlinked to Mission Control Center-Houston this state vector is then uplinked to the CSM The LM commander will perform a Proqram 52 fine alignment to REFSMMAT at approxishymately 12240
The digital autopilot is configured to wide deadband Program P20 is called and an automatic pitch maneuver is initiated to the preferred track attitude At 122 55 CSI targeting parameters are loaded in the PGNS and AGS A period of rendezvous radar marking will then take place from 122-57 to 12315 Upon completion of tracking the LM will obtain an out-of-plane velocity from the CSM to be vectored with the in-plane component of the CSI delta V The CSMs estishymate of out-of-plane velocity is alleged to be better than the LMs estimate (Reference 74)
At approximately 123 20 the LM will voice its CSI solution to the CSM the AGS is updated aligned and targeted in external delta-V with the CDH solution to be excuted Program P41 will then be called and the automatic pitch maneuver bypassed since the burn isto be executed with Z-Axis thrusting The CSI burn occurs nominally at 123 26 27 After verification of the LM CSI burn the CSM will incorporate the LM burn parameters in its CMC LM state vector
32 Constant Delta Height and Plane Change
At 12330 approximately three minutes after the LM CSI burn the W matrix will be set to (200025) and the LM targeting paramters are loaded in both the PGNS and AGS for the CDH maneuver Out-of-plane velocity will then be computed and voiced to the LM from the CSM Program P30 is loaded with the targeting parameters for the LM Plane Change maneuver which will be accomplished in Program P41 30 minutes prior to the CDH maneuver Following the burn the target delta V parameters are voice to the CSM and incorporated into the CMC LM state vector At 12356 the CDH targeting parameters are loaded in both the PGNS and AGS for 1242425 A CDH chart solution is calculated 7 minutes prior to TIG The AGS is updated aligned and targeted in external delta V with the CDH solution to be executed The RCS Thrust Program P41 is called at 12418 and the burn attitude is bypassed since the LM executes CDH by thrusting out individual components of delta V while maintaining radar lock-on
3-2
3 3 Terminal Phase Initiation
Radar tracking is initiated after the CDH maneuver and updating of the LGC continued At 12426 approximately two minutes after the LM CDH burn targeting parameters are loaded in both the PGNS and AGS for the TPI maneuver which will be targeted for a node at intercept Backup measurements are made at the appropriate times The AGS is updated aligned and targeted in external delta V with the TPI solution to be executed The RCS Thrust Program P41 is called at 12456 and the burn attitude is bypassed since the LM is burning along the plus Z-axis with the thrust direction established with the COAS
3 4 Midcourse Corrections
Immediately after TPI the Midcourse Prethrust Program P35 will be called and radar tracking reinitiated Backup measshyurements are made and midcourse corrections chart solutions obtained The MCCl burn will nominally be performed at TPI plus 15 minutes (1251746) If MCCI is to be excuted Program P41 will be called and the burn attitude maneuver is bypassed since the plus Z-axis will remain boresighted at the CSM until docking
Following MCCI Program P35 will be called and targeted for MCC2 at TPI plus 30 minutes (1253246) and executed identishycally to MCCI
3 5 Braking
In preparation for braking the DAP is configured in narrow deadband Program P20 is terminated at 18000 feet but the radar is kept in auto track to provide radar range and range rate displayed on the tapemeter Average G is called by Program P47 prior to braking and attitude hold is selected The braking schedule is followed as contained in Section 4
4-1
40 NOMINAL MISSION PROCEDURES
The procedures included in this section do not specify which crewmember Commander or LM Pilot performs each task These need not be specified since the following basic rules define which crewmember performs each task
41 Commander Tasks
1 All attitude changes whether manual or automatic will be accomplished by the CDR
2 The operation of the DSKY during thrust programs (P40 P41 P42 P47) will be done by the CDR Actual manipulation of the TTCA need not be always done by the CDR but in most cases will be
3 Operation of the rendezvous and landing radar will be done by the CDR
4 The CDR will operate all other systems accessible to only his crew station
42 LM Pilot Tasks
1 AGS operation 2 DSKY operation will be done by the LMP except when keyboard
entries affect the control of spacecraft attitude or thrustshying
3 Backup data logging and chart calculations 4 All logging of maneuver solutions and systems performance 5 The LMP will operate all other systems accessible to only
his crew station
These general rules are guidelines only and may be deviated from by the LM crew if they develop more efficient Task assignments
43 ABBREVIATIONS
The abbreviations used herein are consistant with those in the AOH However in order to condense and simplify the procedures so that they are representative of onboard data a number of addshyitional shorthand conventions have been used To allow the unshyfamiliar reader to understand the procedures contained in this section the following explanations are included
1 AGS - A single asterisk is employed to denote those procedures involving operations to be performed on the DEDA The three number group following an asterisk specifies DEDA address An Rfollowing the address group indicates the address is to be read out A five digit group behind the Rindicates a nominal or expected display If the three number address group is followed by a plus or minus sign a data load is indicated When a single digit follows the plus addition of four zeros behind this digit is assumed Once used these conventions are easily handled and save considerable space
4-2
2 PGNS - The verb-noun addresses in the PGNS are indicated to the left of the procedures column An F is used to indicate a flashing display or absence of an F a static display To the right of the verb-noun on the same line are the contents of the three data registers If numeric quantities appear the DSKY should be correspondingly made to agree by executing a V21 V22 or V23 and performing a data load The procedure of blanking and loading registers is not included since it is repeated often and is highly familiar to the crews
EXAMPLE F 06 33 125-02 46 TIG OF TPI
Expanded this means Load flashing verb 06 noun 33 with the quantity 125 hours 2 minutes and 46 seconds the time of ignition of the RCS engine TPI maneuver Procedurally this is done by keying verb 25 enter loading +000125 in register 1 +00002 in register 2 and +04600 in register 3
If numberic quantities do not follow the verb-noun it is indicated that a computed or information quantity is being displayed via the DSKY If nominal values are listed for possible comparison they appear in parentheses
EXAMPLE- F 06 42 HA HP V
Expanded this means Flashing verb 06 noun 42 has computed height of apogee in register 1 height of perigee in regshyister 2 and velocity to be gained in register 3
3 TIME - The numbers in the left hand column preceded by a plus or minus indicate event timer time referenced to an event Minus indicates event timer counting down to a future event Periodically this same column contains the nominal mission ground elapsed times in parentheses Asterisks following the event time indicate a time critical event which should be accomplished to the nearest second
4-3
4 4 Nominal PGNS Procedures
ASSUMPTIONS
AFTER INSERTION
1 INSERTION COMPLETE (RESIOUALS NULLED) VERIFY V82E (ORBIT) 3 RNDZ RDR LOCKED ON IN MODE II 4 LGC AT FLASHING VERB 37 5 PROPER INITIAL W MATRIX LOADED IN LGC
GUID CONT-PGNS ATTITUDE MON-PGNS(CDR) RATE ERR MON-CMPTR(LMP) ATTITUDE MON-AGS(LMP) SHFTTRUN-+5 DEG X-POINTER-HI MULT RADAR TEST SW-OFF ENG ARM-OFF X-TRANSL-2JETS DEAD BAND-MIN PGNS MODE CONT-AUTO THROTJET-JET CBPGNS IMU OPR-CLOSE RR MODE-LGC TTCATRANSL-ENABLE(COR)
BAL CPL-ON MODE SEL-AGS
RNGALT MON-RNGRNGRT RATE ERR MON-RNDZ RORICOR) ATT CONT-PULSE(3)
AGS MODE CONT-ATT HOLD ACA4JET-DISABLE(CDRJ TTCATRANSL-DISABLE(LMP)
ACA4JET-DISABLE(LMPI
KEY ODE (PO0)
(DOWNLINK LM STATE VECTOR)
KEY V63E (RR SELF TEST)
4-4
F 04 12 00004 00001 PRO
F 16 72 TRUN SHFT PRO
F 16 78 R ROOT VERIFY TAPE METER WITH DSKY
+2 VERIFY INSERTION VELOCITY WITH RNDZ ROR WHERE RANGE = 2642 NM RANGE RATE = -4251 FPS
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
KEY V34E (TERMINATE) KEY V48E (LOAD DAP)
F 01 46 11002 PRO
F 06 47 LMWT CMWT PRO
KEY V56E (KILL AUTO TRACK ENABLE)
+3 KEY V41N72E (COARSE ALIGN RR) F 21 73 +000OOTRUN -077OOSHFT F 04 12 00006 00002 (CONTINUOUS DESIGNATE)
PRO 41 (COARSE ALIGN VERB)
KEY VI6N72E 16 72 MONITOR TRUNSHFT ANGLES
CB PGNS RNDZ RDR-OPEN CB AC BUS A RNDZ RDR-OPEN KEY V44E (TERMINATE RR DESIGNATE)
KEY V83E F 16 54 R ROOT THETA
SET ORDEAL PRO
CS HEATER AOT-CLOSE
CB AOT LAMP-CLOSE
+5 KEY V37E52E (IMU REALIGN)
4-5
410+1 CSI ROUTINE 373+02065 CS TIME 275+03028 TPI TIME
605400777 COTANGENT OF LOS TO-CSM 416+1 (ONE-HALF bRBITAL PERIOD) 411+0 RCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT 310R TIME TO CS
267R VELOCITY TO BE GAINED CSI
402R DELTA H
371R DELTA V CDH
372R _ DELTA T CSICDH
F 04 06 00001 00003 -(REFSMMAT) PRO -
F 50 25 00015 SELECT 1ST STAR ENTR
F 01 70 O02DE LOAD 1ST STAR PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FOAl ANGLES (AUTO MNVRI)
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVR)
F 01 71 002DE
KEY V76E PGNS MODE CONT-ATT HOLD
PRO +10 F 54 71 MARK 1ST STAR
PRO F 01 70 O02DE LOAD 2ND STAR
PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FDA ANGLES -(AUTO MNVRV
F 50 18 FDAI ANGLES (REQUEST PNVRt ENTR (BYPASS MNVR
F 01 71 002DE PGNS MODE CONT-ATT HOLD PRO
-35
4-6
+14 F 54 71 MARK 2ND STAR PRO
F 06 05 STAR ANGLE DIFFERENCE PRO
F 06 93 GYRO TORQUE ANGLES PRO
F 50 25 00014
PRO (CHECK ALIGNMENT IF TIME WILL PERMIT)
F 50 25 00015 SELECT 3RD STAR ENTR
F 01 70 OO2DE LOAD 3RD STAR PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FDAI ANGLES (AUTO MNVR)
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVR)
VERIFY ALIGNMENT VIA AOT
KEY V34E (TERMINATE) F 37 BB
V48E (LOAD DAP) F 01 46 11012
PRO F 06 47 LMWT CMWT
+17 PRO
CB AOT LAMP-OPEN
RESET ET (310R)
(12253) CB AC BUS A RNDZ RDR-CLOSE (WAIT 30 SEC) CB PGNS RNDZ RDR-CLOSE
RR MODE-LGC KEY V37E20E (ACQUIRE RADAR)
PGNS MODE CONT-AUTO F 50 18 FDA ANGLES (REQUEST MNVRJ
PRO (AUTO MNVR) 06 18 FDAI ANGLES (AUTO MNVR)
AGS MODE CONT-AUTO RATEERR MON-CMPTR (LMP)
F 50 18 FDAI ANGLES (REQUEST MNVR)
4-7
ENTR (BYPASS MNVR) NO TRK LT-OFF
F 50 72 RR TRUNSHFT VERIFY RR LOCK ON PRO
DSKY BLANKS
KEY V93E (BEFORE 1ST MARK REINIT W MATRIXI KEY V80E (UPDATE LM SV)
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (i20OOZOO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
400+3 AGS ALIGNshy400R (00000 COMPLETE) 507+0 Z-AXIS BORESIGHT 400+2 ACQUISITION STEERING
CS
(122amp55) KEY V37E32E (CSI)
F 06 11 1 S LOAD TIG CSI FROM DATA PAD (NOM 123S26- 271 PRO
F 06 55 +O000IN +02660E +13000 OMEGAT (CDH 180 DEG AFTER CSI PRO
F 06 37 LOAD TIG TPI FROM DATA PAD (NOM 1251021761 PRO
F 16 45 MKS TFI -00001
-30 COPY RDOT FOR 1ST CSI BU
31OR TIME TO CSI
267R VELOCITY TO BE GAINED CSI
402R DELTA H
371R DELTA V CDH
-22
4-8
372R _ DELTA T CSICDH
KEY V32E (MARKS=5
F 06 75 DELTA H DELTA T CSICDH DELTA T CDHTPI PRO
F 06 81 DELTA VOS-LV (CS) (NOM 501 DELTA VX)
CSI(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (CDH)
(NOM 60 DELTA VX) CDH(82)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
KEY V32E (MARKS=1C)
F 06 75 DELTA H DELTA TCSICDH DELTA TCDHTPI PRD
F 06 81 DELTA VS-LV (CSI) CSI(N811
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 82 DELTA VIS-LV(CDH)
CDH(82)
DELTA VX(LVI
DELTA VY(LV)
DELTA VZ(LV)
-12
4-9
-20 COPY RDOT FOR 2ND CSI BU
F 16 45
F 06 75
F 06 81
F 06 16
F 06 90
PRO MKS TFI -00001
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS NON SEL - PRPLNT A + B TEMP IND 40DEG TO lOODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + 8 PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4v 2 3 (120 - 190 DEG F
(LOS OF MSFN ) S-BAND - SLEW TO P = +90 Y a 0 S-BAND - FWD (OR AFT) S-BAND - DN VOICE BU BIOMED OFF
PRO (FINAL COMP)
267R - VELOCITY TO BE GAINED CSI
402R DELTA H
372R TIME CSICDHL
371R PREDICTED VEL TO BE GAINED CDH
263R OUT-OF-PLANE
DELTA H DELTA TCSICDH DELTA TCDHTPI PRO DELTA VS-LV (CSI)
KEY V9OE (OUT-OF-PLANED
0 LOAD TIG CSI FROM DATA PAD (NOM 12302627) PRO Y YDOT PSI
N90 CSM
YDOT
PRO
-7
4-10
F 06 81 DELTA VS-LV(CSI)
COPY YDOT FROM CSM AND LOAD NEGATIVE IN R2 CSIIN81I
DELTA VX(LV)
DELTA VYILV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (COH)
CDH(82)
DELTA VX(LV)
- DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RANGE AND RDOT FOR 3RD CS BU
COMPUTE CSI BU
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (i2000OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
(TRANSMIT CSI DATA TO CSMI VHF A XMTR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF TELEMETY PCM - LO
KEY VB3E F 16 54 R ROOT THETA
SET ORDEAL PRO
317R RANGE
440R RANGE RATE
4-11
400+3 AGS ALIGN t40OR (00000 COMPLETE)
277R THETA
PRO F 37 BB
-6 KEY 41E (RCS THRUSTING) F 50 18 FDAI-ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTAV 400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTAV 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA RF
TRANSMIT TGT DELTA VS TO CSM AND SYNC COUNTDOWN
16 85 DELTA VS-BODY
502R DELTA VZ (NOM 5Ql)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTAVS-BODY
(123t26t27) BURN +Z
NULL DELTA VS
4-12
VERIFY AGS RESIDUALS 50OR 501R 502R DELTA VX _ DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
CDH
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
KEY V67E (RESET W MATRIX) F 06 99 +0200E +O0020E +00005E
PRO
507+0 Z-AXIS BORESIGHT
(VHF RANGING WITH CSM) VHF A XMTR - VOICERNG VHF B XMTR - OFF VHF B RCVR - ON TELEMETRY PCM - HI
(12331) KEY V37E33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 a TIG CDH (NOM 1242425) -120 amp00 10 (AGS 0 TIME)
(CONVERT TO MINUTES)
411+0 THRUST ALONG Z-BODY AXIS ENTER IF YOU DONT TARGET CSI
373R (NOM 26443 310R TIME TO CDH
4-13
423R DESIRED ALT RATE AT CDH
402R DELTA Hshy
450R DELTA VX
452R DELTA VZ
623+0 Z-AXIS PARALLEL TO CSM PLANE
IPRO F 16 45 MKS TFI -00001
-52 RESET ET
KEY V93E (REINIT W MATRIX WHEN MARKS =4)
KEY V32E (MARKS = 3)
F 06 75 DELTA HCDH DELTA TCDHTPI DELTA TTPI PRO
F 06 81 DELTA VCDH-LV CDH(N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
-47 KEY VSOE (OUT-OF-PLANE)
_ TIG CDH (NOM 124t24t25) -3000 TIME FROM CDH
F 06 16 l1 LOAD TIG PLANE CHANGE (NOM 123amp54-253 PRO
F 06 90 Y YDOT PSI N90 CSM
VYDOT PRO
-42 KEY V32E (MARKS=1O)
F 06 75 DELTA HCDH DELTA TCDIHTPI DELTA TTPITPI PRO
F 06 81 DELTA VCDH-LV
4-14
CDH (NS1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -OO1
KEY V34E (TERMINATE) F 37 B8
PLANE CHANGE
KEY 30E (EXTERNAL DELTA V)
TIG CDH (NOM 124124t25) -3000 TIME FROM CDH
F 06 33 LOAD TIG PLANE CHANGE (NOM 123154T25) PRO
F 06 81 DELTA VS-LV (NOM 00)
-36 COPY RDOT FOR 1ST CDH BU
KEY V90E (OUT-OF-PLANE)
F 06 16 1 1 LOAD TIG PLANE CHANGE (NOM 1231543251 PRO
F 06 90 Y YOOT PSI N90 CSM
YDOT
PRO
F 06 81 DELTA VS-LV(NOM 00)
COPY YDOT AND LOAD NEGATIVE IN R2 PRO
F 06 42 HA HP DELTA V PRO
F 16 45 MKS TFI MGA
PRO
F 37 BB
KEY 41E (RCS THRUSTING)
-30
4-15
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVRI
410+5 EXTERNAL DELTA V 450+0 451-YDOT 452+0 (LOAD CSM -YDOT)
407+0 ROTATE EXTERNAL DELTA V RF
16 95 DELTA VS-BODY
-3035 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATTVHOLD 407+1 FREEZE EXTERNAL DELTAV
F 16 85 DELTA VS-BODY -
NULL DELTA VIS
PRO F 37BB
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
507+0 Z-AXIS BORESIGHT
(12356) KEY 33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 TIG CDH (NOM 124t24t25) -120 OO ZOO (AGS 0 TIME)
(CONVERT TO MINUTES)
373R _ (NOM 2644) 310R TIME TO CDH
423R DESIRED ALT RATE AT CDH
(ADS OF MSFN) S-BAND - SLEW TOP = ACQUIRE HGA LOCK ON VOICE - BUVOICE -- VOICE VERIFY VOICE TLM BIOMED - LEFT (OR RIGHT)
402R DELTAH
4-16
F 16 45
-25
-23
F 06 75
F 06 81
F 16 45
-12
F 06 75
F 06 81
450R DELTA VX
452R DELTA VZ
PRO MKS TFI -00001
KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
COPY ROOT FOR 2ND CDH BU
KEY v32E (MARKS = 5)
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40DEG TO 1OODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + B PRESS IND PSIA
A QUANTITY IND _ PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING a TEMP MON SEL RCS QUAD 1 4 2 3 (120 - 190 DEG F)i
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
CDH(NB1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO MKS TFI -00001
PRO (FINAL COMP)
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
KEY V9OE (OUT-OF-PLANE)
-7
4-17
F 06 16 jj LOAD TIG CDH FROM DATA PAD (NOM 12424251 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT PRO
COPY YOOT FROM CSM AND LOAD NEGATIVE IN R2
CDH(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RDOT FOR 3RD CDH BU
COMPUTE CDH BU
TRANSMIT TGT DELTA VOS TO CSM AND SYNC COUNTDOWN
KEY V47E (INITIALIZE AGS F 06 16 GET OF AGS 0 TIME 120O00OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
KEY V83E F 16 54 R RDOT THETA
SET ORDEAL PRO
317R _ RANGE
440R RANGE RATE 400+3 AGS ALIGN 40OR (00000 COMPLETE)
277R THETA
-6
4-18
PRO F 3 BB
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY V06N86E F 06 86 DELTA VIS-LV
AGS(N86) CHART
DELTA VX(LVD
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
16 85 DELTA VS-BODY
50OR DELTA VX (NOM -0O3)
502R DELTA VZ (NOM 60)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD 407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS BODY
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS 5OOR 50IR 502R DELTA VX -DELTA VY DELTA VZ-
VERIFY PGNS RESIDUALS N85
DELTA VX(LM)
4-19
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
TPI
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO 507+0 Z-AXIS BORESIGHT
(12426) KEY 34E (TPI)
-36 RESET ET
F 06 37 - amp LOAD TIG TPI FROM DATA PAD (NOM 1250246) PRO
F 06 55 +00000 +02660E +13000 OMEGAT PRO
F 16 45 MARKS TFI -00001
-32 KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
-29 KEY V32E (MARKS = 3)
F 06 37 __ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
RESET ET
410+3 TPI SEARCH ROUTINE 307+04300 DELTA T TRANSFER
4-20
-26 310+02600 TFI TPI
303R THETA AT TPI
267R DELTA VTPI
371R DELTA VTPI + DELTA VTPF
KEY V32E (MARKS = 10)
F 06 37 _ _ _ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VIS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
TEMPIPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40ODEG TO IGODEG F A + B PRESS IND 181 +-3 PSIA
TEMPIPRESS MON SEL - HEL
A + B PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD I 4 2 3 (120 - 190 DEG F)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
RESET ET
-13 310+01300 TFI TPI
303R THETA AT TPI
-12 PRO (FINAL COMP) F 06 37 Z TIG TPIj__
4-21
TRANSMIT TIG OF TPI TO CSM-
PRO F 06 58 HP DELTA VTPI DELTA VTRF
PRO F 06 81 DELTA VS-LV
KEY V9OE (OUT-OF-PLANE)
F 06 16 1 LOAD TIG TPI FROM DATA PAD (NOM 12502461 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT
PRO F 06 81 DELTA VS-LV
COPY CSM YDOT AND LOAD NEGATIVE IN R2 N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 59 DELTA VS LOS
N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI MGA
RESET ET
PRO F 37 BB
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (12000t600)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE)
-10
-6
4-22
F 50 16 DOWNLINK COMPLETE PRO (UPDATE COMPLETE)
400+3 AGS ALIGN 400R (00000 COMPLETE)
-9 277R COPY TGT LOS ANGLE
310+00800
303R THETA AT TPI 410+4 DIRECT TRANSFER AT ET=-8 404+0 405+0 406+0 (MONITOR 470 471 4721
373R TIG TPI
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
KEY 41E (RCS THRUSTING) F 50 18 FOAl ANGLES (REQUEST MNVRI
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
-5 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUS
400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
COMPUTE TPI BU
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
4-23
1685 DELTA VS-BODY
50OR DELTA VX(NOM -115)
502R DELTA VZ(NOM 229)
-Z35 OSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS-BODY
(1250246) BURN +Z
VERIFY AGS RESIDUALS 500R 501R 502R DELTAVX DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
MCC1
KEY V76E (PGNS PULSE) PGNSMODECONT-AUTO
KEY V93E (BEFORE 1ST MARK REINITW MATRIX)
+2 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
4-24
(LOS OF MSFN) S-BAND - SLEW TO P = 90 Y = 0 S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
404+0 405+0 406+0
(MONITOR 470 471 4721
+9 277R COPY TGT LOS ANGLE
+12 PRO (COMPUTE MCC FOR TPI+15I F 06 81 DELTA VS-LV
PRO F 06 59 DELTA VS-LOS
PRO F 16 45 MKS TFI MGA
+13 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUOS
COMPUTE MCC1 BU
PRO F 37 BB
+14 KEY 41E (RCS THRUSTING) F 50 18 FOAL ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+1425 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+15 F 16 85 NULL DELTA VS
PRO F 37 BB
MCC2
KEY V76E (PGNS PULSE)
4-25
PGNS MODE CONT-AUTO
KEY V93E (BEFORE 1ST MARK REINIT W MATRIX)
+16 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
404+0 405+0 406+0 (MONITOR 470 471 47)shy
+24 277R COPY TGT LOS ANGLE
+27 PRO (COMPUTE MCC FORTPI+30) F 06 81 DELTA VS-LV
PRO F 06 59 DELIA VPS-LOS
PRO F 16 45 MKS TFI MGA
+28 277R COPY TGT LOS ANGLE
COPY R RDOT FROM TAPEMETER FOR BUS
COMPUTE MCC2 BU
F 37 BB PRO
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+2925 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+30 F 16 85 NULL DELTA VS
PRO F 37 BB
KEY OOE (P001
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
4-26
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT KEY V34E (TERMINATE)
KEY V37E47E (AVE G) F 16 83 DELTA VIS
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT VERIFY TAPE METER WITH DSKY
BRAKING GATE 30 FPS - 6000 FT 20 FPS - 3000 FT 10 FPS - 1500 FT 5 FPS - 600 FT
RENDEZVOUS
STATION KEEPING
5-1
50 ABORT PROCEDURE
This is a specific AGS nominal abort procedure due to a PGNS failure between insertion and station keeping
51
5-2
Nominal AGS Procedures
ASSUMPTIONS
AFTER INSERTION
I INSERTION COMPLETE (RFSIDUALS NULLED) g PGNS FAILURE BEFORE INSERTION 3 RAUAR NOT LOCKED ON
(UI CoNT-AGS ATlI[uUE MON-AGS(CDR) RATE ERR MON-CNPTR(LMP) ATTITUDE MON-AGS(LMP) SHFITRUN-+5 DEG X-POINTER-HI MULT RADAR IEST Sw-OFF LNb GMbL-OFF ENG ARM-OFF X-IRANSL-2 JETS DEAD BAND-MAX PGNS MODE CONT-OFF THROTJET-JET CB IMU OIR-ON HH MOVE-AUTO rRACK TTCATNANSL-ENABLE(CDR)
AL CPL-ON MODE SL-AGS RNGAL1 MON-RNbRNGRT RAIE ERR MON-RNDZ HDR(CDR) AVl CoNT(3)-PULSE AGS MODE CONT-AUTO ACA4JET-DISABLE(CDR) TTCATRANSL-DISABLE(LMP) ACA4JET-DISABLE(LMP)
bO7+U Z-AXIS BOPESIGHT 400+2 Z-AXIS STEERING PULSE TO NULL AGS ERRORS POINT Z-AXIS IN DIRECTION OF CSM MODE CONT-ATT HOLD ATT CONT(3)-MODE CONTROL O unnr - ZirF
5-3
SLEW PATE - LO
SLEW RR ANT TO OqON FUAI VERIFY MAX SIGNAL STRENGTH RH MOOE-AUTO TRACK NO TRACK LIGHT OFF -
ATT CONT(3h-PULSE
CHECK INSERTION VELOCITY WITH TAPEMETER COMPARE EAPEMETER WITH AGS STATE VECTOR DATA I
17R RANGE(NOM 2642)
440R RANGE RATE(NOM -425l)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
cSI
+3 417+1 (RADAR FILTER INITIALIZED) 41b+l (NO BOHESIGHT) b03-XXXXX RANGE RATE
+5 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGF
41b+1 CSI ROUTINE 373+o2065 CSi TIME 275+03028 TPI TIME 605+0077 COTANGENT OF LOS TO CSM 41b+1 (ONE-HALF OFBITAL-PERIOD) 411+0 HCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT
610R TIME TO CST
43 RESET ET
267R VELOCITY TO BE GAINED CSI
402R FLTA H
371R DFLTA V CDH
5-4
372R DFLTA T CSICDH
-42 415+1 (No BORESIGHT) bO6-xXXXX RANGE RATE
-40 415+1 (NO BORESIGHT)503-XXXXX RANGE RATE dORESIGHT ON CSM
415+1 316+XXXXX RANGE
-37 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE
-15 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE UORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-2 415+1 (No BOHESIGHT) bO3-XXXXX RANGF RATE
i1uR TIME TO CS
RESEF ET
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-30 COPY ROOT FOR 1ST CSI 81J
BORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-t7 415+1 (NO BORFSIGHT) 50-XXxXx RANGF RATE
267R VELOCITY TO HE GAINED CSI
402R LELTA H
371R OFLTA V COH
372R OELTA T CSICDH
-5 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 blb+XXXXX RANGE
-i2 415+1 (No BORESIGHT) 5n3-XXXXX RANGE RATE
415+1 (NO BORESIGHT)
5-5
503-XXXXX RANGF RATE
COPY Roor FOR 2NO CSI BU
bORESIGHT ON CSM 415+1 316+XXXXX RANGE
TEMPPRESS MON SEL - FUEL MAN
A AND 8 PRESS 181 +-3 PIG TEMPPRESS MON SEL - PRPLNT
A AND B TEMP IND 4ODEG 0 IOODEG F A AND B PRFSS IND 181 +-3 PSIA
tEMPPRESS MON SEL - HEL
A AND 8 PRESS IND PSIA
A QUANTITY IND- -- PERCENT RFMAINING
8 QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4p 2 3 (120 - 190 DFG F)
415+1 (NO BORESIGHT)-17 503-XXXXX RANGE RATE
-15 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
(LOS OF MSFN) S-BAND - SLEW 10 P = +90t Y U S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
-12 415+1 (No 8ORESIGHT)
503-XXXXX RANGE RATE
267R VFLOCITY TU BE GAINED CSI
402R OFLTA H
372R TIME CSICH
371R PREDICTED VEL 10 RE GAINED COH
263R OLT-OF-PLANE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATL
-10 COPY RANGE AND ROOT FOR 3RD CSI 8U
SORESIGH ON CSM 41b+1
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
3-2
3 3 Terminal Phase Initiation
Radar tracking is initiated after the CDH maneuver and updating of the LGC continued At 12426 approximately two minutes after the LM CDH burn targeting parameters are loaded in both the PGNS and AGS for the TPI maneuver which will be targeted for a node at intercept Backup measurements are made at the appropriate times The AGS is updated aligned and targeted in external delta V with the TPI solution to be executed The RCS Thrust Program P41 is called at 12456 and the burn attitude is bypassed since the LM is burning along the plus Z-axis with the thrust direction established with the COAS
3 4 Midcourse Corrections
Immediately after TPI the Midcourse Prethrust Program P35 will be called and radar tracking reinitiated Backup measshyurements are made and midcourse corrections chart solutions obtained The MCCl burn will nominally be performed at TPI plus 15 minutes (1251746) If MCCI is to be excuted Program P41 will be called and the burn attitude maneuver is bypassed since the plus Z-axis will remain boresighted at the CSM until docking
Following MCCI Program P35 will be called and targeted for MCC2 at TPI plus 30 minutes (1253246) and executed identishycally to MCCI
3 5 Braking
In preparation for braking the DAP is configured in narrow deadband Program P20 is terminated at 18000 feet but the radar is kept in auto track to provide radar range and range rate displayed on the tapemeter Average G is called by Program P47 prior to braking and attitude hold is selected The braking schedule is followed as contained in Section 4
4-1
40 NOMINAL MISSION PROCEDURES
The procedures included in this section do not specify which crewmember Commander or LM Pilot performs each task These need not be specified since the following basic rules define which crewmember performs each task
41 Commander Tasks
1 All attitude changes whether manual or automatic will be accomplished by the CDR
2 The operation of the DSKY during thrust programs (P40 P41 P42 P47) will be done by the CDR Actual manipulation of the TTCA need not be always done by the CDR but in most cases will be
3 Operation of the rendezvous and landing radar will be done by the CDR
4 The CDR will operate all other systems accessible to only his crew station
42 LM Pilot Tasks
1 AGS operation 2 DSKY operation will be done by the LMP except when keyboard
entries affect the control of spacecraft attitude or thrustshying
3 Backup data logging and chart calculations 4 All logging of maneuver solutions and systems performance 5 The LMP will operate all other systems accessible to only
his crew station
These general rules are guidelines only and may be deviated from by the LM crew if they develop more efficient Task assignments
43 ABBREVIATIONS
The abbreviations used herein are consistant with those in the AOH However in order to condense and simplify the procedures so that they are representative of onboard data a number of addshyitional shorthand conventions have been used To allow the unshyfamiliar reader to understand the procedures contained in this section the following explanations are included
1 AGS - A single asterisk is employed to denote those procedures involving operations to be performed on the DEDA The three number group following an asterisk specifies DEDA address An Rfollowing the address group indicates the address is to be read out A five digit group behind the Rindicates a nominal or expected display If the three number address group is followed by a plus or minus sign a data load is indicated When a single digit follows the plus addition of four zeros behind this digit is assumed Once used these conventions are easily handled and save considerable space
4-2
2 PGNS - The verb-noun addresses in the PGNS are indicated to the left of the procedures column An F is used to indicate a flashing display or absence of an F a static display To the right of the verb-noun on the same line are the contents of the three data registers If numeric quantities appear the DSKY should be correspondingly made to agree by executing a V21 V22 or V23 and performing a data load The procedure of blanking and loading registers is not included since it is repeated often and is highly familiar to the crews
EXAMPLE F 06 33 125-02 46 TIG OF TPI
Expanded this means Load flashing verb 06 noun 33 with the quantity 125 hours 2 minutes and 46 seconds the time of ignition of the RCS engine TPI maneuver Procedurally this is done by keying verb 25 enter loading +000125 in register 1 +00002 in register 2 and +04600 in register 3
If numberic quantities do not follow the verb-noun it is indicated that a computed or information quantity is being displayed via the DSKY If nominal values are listed for possible comparison they appear in parentheses
EXAMPLE- F 06 42 HA HP V
Expanded this means Flashing verb 06 noun 42 has computed height of apogee in register 1 height of perigee in regshyister 2 and velocity to be gained in register 3
3 TIME - The numbers in the left hand column preceded by a plus or minus indicate event timer time referenced to an event Minus indicates event timer counting down to a future event Periodically this same column contains the nominal mission ground elapsed times in parentheses Asterisks following the event time indicate a time critical event which should be accomplished to the nearest second
4-3
4 4 Nominal PGNS Procedures
ASSUMPTIONS
AFTER INSERTION
1 INSERTION COMPLETE (RESIOUALS NULLED) VERIFY V82E (ORBIT) 3 RNDZ RDR LOCKED ON IN MODE II 4 LGC AT FLASHING VERB 37 5 PROPER INITIAL W MATRIX LOADED IN LGC
GUID CONT-PGNS ATTITUDE MON-PGNS(CDR) RATE ERR MON-CMPTR(LMP) ATTITUDE MON-AGS(LMP) SHFTTRUN-+5 DEG X-POINTER-HI MULT RADAR TEST SW-OFF ENG ARM-OFF X-TRANSL-2JETS DEAD BAND-MIN PGNS MODE CONT-AUTO THROTJET-JET CBPGNS IMU OPR-CLOSE RR MODE-LGC TTCATRANSL-ENABLE(COR)
BAL CPL-ON MODE SEL-AGS
RNGALT MON-RNGRNGRT RATE ERR MON-RNDZ RORICOR) ATT CONT-PULSE(3)
AGS MODE CONT-ATT HOLD ACA4JET-DISABLE(CDRJ TTCATRANSL-DISABLE(LMP)
ACA4JET-DISABLE(LMPI
KEY ODE (PO0)
(DOWNLINK LM STATE VECTOR)
KEY V63E (RR SELF TEST)
4-4
F 04 12 00004 00001 PRO
F 16 72 TRUN SHFT PRO
F 16 78 R ROOT VERIFY TAPE METER WITH DSKY
+2 VERIFY INSERTION VELOCITY WITH RNDZ ROR WHERE RANGE = 2642 NM RANGE RATE = -4251 FPS
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
KEY V34E (TERMINATE) KEY V48E (LOAD DAP)
F 01 46 11002 PRO
F 06 47 LMWT CMWT PRO
KEY V56E (KILL AUTO TRACK ENABLE)
+3 KEY V41N72E (COARSE ALIGN RR) F 21 73 +000OOTRUN -077OOSHFT F 04 12 00006 00002 (CONTINUOUS DESIGNATE)
PRO 41 (COARSE ALIGN VERB)
KEY VI6N72E 16 72 MONITOR TRUNSHFT ANGLES
CB PGNS RNDZ RDR-OPEN CB AC BUS A RNDZ RDR-OPEN KEY V44E (TERMINATE RR DESIGNATE)
KEY V83E F 16 54 R ROOT THETA
SET ORDEAL PRO
CS HEATER AOT-CLOSE
CB AOT LAMP-CLOSE
+5 KEY V37E52E (IMU REALIGN)
4-5
410+1 CSI ROUTINE 373+02065 CS TIME 275+03028 TPI TIME
605400777 COTANGENT OF LOS TO-CSM 416+1 (ONE-HALF bRBITAL PERIOD) 411+0 RCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT 310R TIME TO CS
267R VELOCITY TO BE GAINED CSI
402R DELTA H
371R DELTA V CDH
372R _ DELTA T CSICDH
F 04 06 00001 00003 -(REFSMMAT) PRO -
F 50 25 00015 SELECT 1ST STAR ENTR
F 01 70 O02DE LOAD 1ST STAR PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FOAl ANGLES (AUTO MNVRI)
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVR)
F 01 71 002DE
KEY V76E PGNS MODE CONT-ATT HOLD
PRO +10 F 54 71 MARK 1ST STAR
PRO F 01 70 O02DE LOAD 2ND STAR
PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FDA ANGLES -(AUTO MNVRV
F 50 18 FDAI ANGLES (REQUEST PNVRt ENTR (BYPASS MNVR
F 01 71 002DE PGNS MODE CONT-ATT HOLD PRO
-35
4-6
+14 F 54 71 MARK 2ND STAR PRO
F 06 05 STAR ANGLE DIFFERENCE PRO
F 06 93 GYRO TORQUE ANGLES PRO
F 50 25 00014
PRO (CHECK ALIGNMENT IF TIME WILL PERMIT)
F 50 25 00015 SELECT 3RD STAR ENTR
F 01 70 OO2DE LOAD 3RD STAR PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FDAI ANGLES (AUTO MNVR)
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVR)
VERIFY ALIGNMENT VIA AOT
KEY V34E (TERMINATE) F 37 BB
V48E (LOAD DAP) F 01 46 11012
PRO F 06 47 LMWT CMWT
+17 PRO
CB AOT LAMP-OPEN
RESET ET (310R)
(12253) CB AC BUS A RNDZ RDR-CLOSE (WAIT 30 SEC) CB PGNS RNDZ RDR-CLOSE
RR MODE-LGC KEY V37E20E (ACQUIRE RADAR)
PGNS MODE CONT-AUTO F 50 18 FDA ANGLES (REQUEST MNVRJ
PRO (AUTO MNVR) 06 18 FDAI ANGLES (AUTO MNVR)
AGS MODE CONT-AUTO RATEERR MON-CMPTR (LMP)
F 50 18 FDAI ANGLES (REQUEST MNVR)
4-7
ENTR (BYPASS MNVR) NO TRK LT-OFF
F 50 72 RR TRUNSHFT VERIFY RR LOCK ON PRO
DSKY BLANKS
KEY V93E (BEFORE 1ST MARK REINIT W MATRIXI KEY V80E (UPDATE LM SV)
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (i20OOZOO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
400+3 AGS ALIGNshy400R (00000 COMPLETE) 507+0 Z-AXIS BORESIGHT 400+2 ACQUISITION STEERING
CS
(122amp55) KEY V37E32E (CSI)
F 06 11 1 S LOAD TIG CSI FROM DATA PAD (NOM 123S26- 271 PRO
F 06 55 +O000IN +02660E +13000 OMEGAT (CDH 180 DEG AFTER CSI PRO
F 06 37 LOAD TIG TPI FROM DATA PAD (NOM 1251021761 PRO
F 16 45 MKS TFI -00001
-30 COPY RDOT FOR 1ST CSI BU
31OR TIME TO CSI
267R VELOCITY TO BE GAINED CSI
402R DELTA H
371R DELTA V CDH
-22
4-8
372R _ DELTA T CSICDH
KEY V32E (MARKS=5
F 06 75 DELTA H DELTA T CSICDH DELTA T CDHTPI PRO
F 06 81 DELTA VOS-LV (CS) (NOM 501 DELTA VX)
CSI(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (CDH)
(NOM 60 DELTA VX) CDH(82)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
KEY V32E (MARKS=1C)
F 06 75 DELTA H DELTA TCSICDH DELTA TCDHTPI PRD
F 06 81 DELTA VS-LV (CSI) CSI(N811
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 82 DELTA VIS-LV(CDH)
CDH(82)
DELTA VX(LVI
DELTA VY(LV)
DELTA VZ(LV)
-12
4-9
-20 COPY RDOT FOR 2ND CSI BU
F 16 45
F 06 75
F 06 81
F 06 16
F 06 90
PRO MKS TFI -00001
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS NON SEL - PRPLNT A + B TEMP IND 40DEG TO lOODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + 8 PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4v 2 3 (120 - 190 DEG F
(LOS OF MSFN ) S-BAND - SLEW TO P = +90 Y a 0 S-BAND - FWD (OR AFT) S-BAND - DN VOICE BU BIOMED OFF
PRO (FINAL COMP)
267R - VELOCITY TO BE GAINED CSI
402R DELTA H
372R TIME CSICDHL
371R PREDICTED VEL TO BE GAINED CDH
263R OUT-OF-PLANE
DELTA H DELTA TCSICDH DELTA TCDHTPI PRO DELTA VS-LV (CSI)
KEY V9OE (OUT-OF-PLANED
0 LOAD TIG CSI FROM DATA PAD (NOM 12302627) PRO Y YDOT PSI
N90 CSM
YDOT
PRO
-7
4-10
F 06 81 DELTA VS-LV(CSI)
COPY YDOT FROM CSM AND LOAD NEGATIVE IN R2 CSIIN81I
DELTA VX(LV)
DELTA VYILV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (COH)
CDH(82)
DELTA VX(LV)
- DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RANGE AND RDOT FOR 3RD CS BU
COMPUTE CSI BU
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (i2000OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
(TRANSMIT CSI DATA TO CSMI VHF A XMTR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF TELEMETY PCM - LO
KEY VB3E F 16 54 R ROOT THETA
SET ORDEAL PRO
317R RANGE
440R RANGE RATE
4-11
400+3 AGS ALIGN t40OR (00000 COMPLETE)
277R THETA
PRO F 37 BB
-6 KEY 41E (RCS THRUSTING) F 50 18 FDAI-ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTAV 400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTAV 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA RF
TRANSMIT TGT DELTA VS TO CSM AND SYNC COUNTDOWN
16 85 DELTA VS-BODY
502R DELTA VZ (NOM 5Ql)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTAVS-BODY
(123t26t27) BURN +Z
NULL DELTA VS
4-12
VERIFY AGS RESIDUALS 50OR 501R 502R DELTA VX _ DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
CDH
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
KEY V67E (RESET W MATRIX) F 06 99 +0200E +O0020E +00005E
PRO
507+0 Z-AXIS BORESIGHT
(VHF RANGING WITH CSM) VHF A XMTR - VOICERNG VHF B XMTR - OFF VHF B RCVR - ON TELEMETRY PCM - HI
(12331) KEY V37E33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 a TIG CDH (NOM 1242425) -120 amp00 10 (AGS 0 TIME)
(CONVERT TO MINUTES)
411+0 THRUST ALONG Z-BODY AXIS ENTER IF YOU DONT TARGET CSI
373R (NOM 26443 310R TIME TO CDH
4-13
423R DESIRED ALT RATE AT CDH
402R DELTA Hshy
450R DELTA VX
452R DELTA VZ
623+0 Z-AXIS PARALLEL TO CSM PLANE
IPRO F 16 45 MKS TFI -00001
-52 RESET ET
KEY V93E (REINIT W MATRIX WHEN MARKS =4)
KEY V32E (MARKS = 3)
F 06 75 DELTA HCDH DELTA TCDHTPI DELTA TTPI PRO
F 06 81 DELTA VCDH-LV CDH(N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
-47 KEY VSOE (OUT-OF-PLANE)
_ TIG CDH (NOM 124t24t25) -3000 TIME FROM CDH
F 06 16 l1 LOAD TIG PLANE CHANGE (NOM 123amp54-253 PRO
F 06 90 Y YDOT PSI N90 CSM
VYDOT PRO
-42 KEY V32E (MARKS=1O)
F 06 75 DELTA HCDH DELTA TCDIHTPI DELTA TTPITPI PRO
F 06 81 DELTA VCDH-LV
4-14
CDH (NS1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -OO1
KEY V34E (TERMINATE) F 37 B8
PLANE CHANGE
KEY 30E (EXTERNAL DELTA V)
TIG CDH (NOM 124124t25) -3000 TIME FROM CDH
F 06 33 LOAD TIG PLANE CHANGE (NOM 123154T25) PRO
F 06 81 DELTA VS-LV (NOM 00)
-36 COPY RDOT FOR 1ST CDH BU
KEY V90E (OUT-OF-PLANE)
F 06 16 1 1 LOAD TIG PLANE CHANGE (NOM 1231543251 PRO
F 06 90 Y YOOT PSI N90 CSM
YDOT
PRO
F 06 81 DELTA VS-LV(NOM 00)
COPY YDOT AND LOAD NEGATIVE IN R2 PRO
F 06 42 HA HP DELTA V PRO
F 16 45 MKS TFI MGA
PRO
F 37 BB
KEY 41E (RCS THRUSTING)
-30
4-15
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVRI
410+5 EXTERNAL DELTA V 450+0 451-YDOT 452+0 (LOAD CSM -YDOT)
407+0 ROTATE EXTERNAL DELTA V RF
16 95 DELTA VS-BODY
-3035 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATTVHOLD 407+1 FREEZE EXTERNAL DELTAV
F 16 85 DELTA VS-BODY -
NULL DELTA VIS
PRO F 37BB
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
507+0 Z-AXIS BORESIGHT
(12356) KEY 33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 TIG CDH (NOM 124t24t25) -120 OO ZOO (AGS 0 TIME)
(CONVERT TO MINUTES)
373R _ (NOM 2644) 310R TIME TO CDH
423R DESIRED ALT RATE AT CDH
(ADS OF MSFN) S-BAND - SLEW TOP = ACQUIRE HGA LOCK ON VOICE - BUVOICE -- VOICE VERIFY VOICE TLM BIOMED - LEFT (OR RIGHT)
402R DELTAH
4-16
F 16 45
-25
-23
F 06 75
F 06 81
F 16 45
-12
F 06 75
F 06 81
450R DELTA VX
452R DELTA VZ
PRO MKS TFI -00001
KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
COPY ROOT FOR 2ND CDH BU
KEY v32E (MARKS = 5)
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40DEG TO 1OODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + B PRESS IND PSIA
A QUANTITY IND _ PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING a TEMP MON SEL RCS QUAD 1 4 2 3 (120 - 190 DEG F)i
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
CDH(NB1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO MKS TFI -00001
PRO (FINAL COMP)
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
KEY V9OE (OUT-OF-PLANE)
-7
4-17
F 06 16 jj LOAD TIG CDH FROM DATA PAD (NOM 12424251 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT PRO
COPY YOOT FROM CSM AND LOAD NEGATIVE IN R2
CDH(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RDOT FOR 3RD CDH BU
COMPUTE CDH BU
TRANSMIT TGT DELTA VOS TO CSM AND SYNC COUNTDOWN
KEY V47E (INITIALIZE AGS F 06 16 GET OF AGS 0 TIME 120O00OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
KEY V83E F 16 54 R RDOT THETA
SET ORDEAL PRO
317R _ RANGE
440R RANGE RATE 400+3 AGS ALIGN 40OR (00000 COMPLETE)
277R THETA
-6
4-18
PRO F 3 BB
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY V06N86E F 06 86 DELTA VIS-LV
AGS(N86) CHART
DELTA VX(LVD
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
16 85 DELTA VS-BODY
50OR DELTA VX (NOM -0O3)
502R DELTA VZ (NOM 60)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD 407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS BODY
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS 5OOR 50IR 502R DELTA VX -DELTA VY DELTA VZ-
VERIFY PGNS RESIDUALS N85
DELTA VX(LM)
4-19
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
TPI
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO 507+0 Z-AXIS BORESIGHT
(12426) KEY 34E (TPI)
-36 RESET ET
F 06 37 - amp LOAD TIG TPI FROM DATA PAD (NOM 1250246) PRO
F 06 55 +00000 +02660E +13000 OMEGAT PRO
F 16 45 MARKS TFI -00001
-32 KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
-29 KEY V32E (MARKS = 3)
F 06 37 __ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
RESET ET
410+3 TPI SEARCH ROUTINE 307+04300 DELTA T TRANSFER
4-20
-26 310+02600 TFI TPI
303R THETA AT TPI
267R DELTA VTPI
371R DELTA VTPI + DELTA VTPF
KEY V32E (MARKS = 10)
F 06 37 _ _ _ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VIS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
TEMPIPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40ODEG TO IGODEG F A + B PRESS IND 181 +-3 PSIA
TEMPIPRESS MON SEL - HEL
A + B PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD I 4 2 3 (120 - 190 DEG F)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
RESET ET
-13 310+01300 TFI TPI
303R THETA AT TPI
-12 PRO (FINAL COMP) F 06 37 Z TIG TPIj__
4-21
TRANSMIT TIG OF TPI TO CSM-
PRO F 06 58 HP DELTA VTPI DELTA VTRF
PRO F 06 81 DELTA VS-LV
KEY V9OE (OUT-OF-PLANE)
F 06 16 1 LOAD TIG TPI FROM DATA PAD (NOM 12502461 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT
PRO F 06 81 DELTA VS-LV
COPY CSM YDOT AND LOAD NEGATIVE IN R2 N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 59 DELTA VS LOS
N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI MGA
RESET ET
PRO F 37 BB
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (12000t600)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE)
-10
-6
4-22
F 50 16 DOWNLINK COMPLETE PRO (UPDATE COMPLETE)
400+3 AGS ALIGN 400R (00000 COMPLETE)
-9 277R COPY TGT LOS ANGLE
310+00800
303R THETA AT TPI 410+4 DIRECT TRANSFER AT ET=-8 404+0 405+0 406+0 (MONITOR 470 471 4721
373R TIG TPI
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
KEY 41E (RCS THRUSTING) F 50 18 FOAl ANGLES (REQUEST MNVRI
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
-5 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUS
400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
COMPUTE TPI BU
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
4-23
1685 DELTA VS-BODY
50OR DELTA VX(NOM -115)
502R DELTA VZ(NOM 229)
-Z35 OSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS-BODY
(1250246) BURN +Z
VERIFY AGS RESIDUALS 500R 501R 502R DELTAVX DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
MCC1
KEY V76E (PGNS PULSE) PGNSMODECONT-AUTO
KEY V93E (BEFORE 1ST MARK REINITW MATRIX)
+2 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
4-24
(LOS OF MSFN) S-BAND - SLEW TO P = 90 Y = 0 S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
404+0 405+0 406+0
(MONITOR 470 471 4721
+9 277R COPY TGT LOS ANGLE
+12 PRO (COMPUTE MCC FOR TPI+15I F 06 81 DELTA VS-LV
PRO F 06 59 DELTA VS-LOS
PRO F 16 45 MKS TFI MGA
+13 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUOS
COMPUTE MCC1 BU
PRO F 37 BB
+14 KEY 41E (RCS THRUSTING) F 50 18 FOAL ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+1425 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+15 F 16 85 NULL DELTA VS
PRO F 37 BB
MCC2
KEY V76E (PGNS PULSE)
4-25
PGNS MODE CONT-AUTO
KEY V93E (BEFORE 1ST MARK REINIT W MATRIX)
+16 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
404+0 405+0 406+0 (MONITOR 470 471 47)shy
+24 277R COPY TGT LOS ANGLE
+27 PRO (COMPUTE MCC FORTPI+30) F 06 81 DELTA VS-LV
PRO F 06 59 DELIA VPS-LOS
PRO F 16 45 MKS TFI MGA
+28 277R COPY TGT LOS ANGLE
COPY R RDOT FROM TAPEMETER FOR BUS
COMPUTE MCC2 BU
F 37 BB PRO
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+2925 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+30 F 16 85 NULL DELTA VS
PRO F 37 BB
KEY OOE (P001
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
4-26
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT KEY V34E (TERMINATE)
KEY V37E47E (AVE G) F 16 83 DELTA VIS
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT VERIFY TAPE METER WITH DSKY
BRAKING GATE 30 FPS - 6000 FT 20 FPS - 3000 FT 10 FPS - 1500 FT 5 FPS - 600 FT
RENDEZVOUS
STATION KEEPING
5-1
50 ABORT PROCEDURE
This is a specific AGS nominal abort procedure due to a PGNS failure between insertion and station keeping
51
5-2
Nominal AGS Procedures
ASSUMPTIONS
AFTER INSERTION
I INSERTION COMPLETE (RFSIDUALS NULLED) g PGNS FAILURE BEFORE INSERTION 3 RAUAR NOT LOCKED ON
(UI CoNT-AGS ATlI[uUE MON-AGS(CDR) RATE ERR MON-CNPTR(LMP) ATTITUDE MON-AGS(LMP) SHFITRUN-+5 DEG X-POINTER-HI MULT RADAR IEST Sw-OFF LNb GMbL-OFF ENG ARM-OFF X-IRANSL-2 JETS DEAD BAND-MAX PGNS MODE CONT-OFF THROTJET-JET CB IMU OIR-ON HH MOVE-AUTO rRACK TTCATNANSL-ENABLE(CDR)
AL CPL-ON MODE SL-AGS RNGAL1 MON-RNbRNGRT RAIE ERR MON-RNDZ HDR(CDR) AVl CoNT(3)-PULSE AGS MODE CONT-AUTO ACA4JET-DISABLE(CDR) TTCATRANSL-DISABLE(LMP) ACA4JET-DISABLE(LMP)
bO7+U Z-AXIS BOPESIGHT 400+2 Z-AXIS STEERING PULSE TO NULL AGS ERRORS POINT Z-AXIS IN DIRECTION OF CSM MODE CONT-ATT HOLD ATT CONT(3)-MODE CONTROL O unnr - ZirF
5-3
SLEW PATE - LO
SLEW RR ANT TO OqON FUAI VERIFY MAX SIGNAL STRENGTH RH MOOE-AUTO TRACK NO TRACK LIGHT OFF -
ATT CONT(3h-PULSE
CHECK INSERTION VELOCITY WITH TAPEMETER COMPARE EAPEMETER WITH AGS STATE VECTOR DATA I
17R RANGE(NOM 2642)
440R RANGE RATE(NOM -425l)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
cSI
+3 417+1 (RADAR FILTER INITIALIZED) 41b+l (NO BOHESIGHT) b03-XXXXX RANGE RATE
+5 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGF
41b+1 CSI ROUTINE 373+o2065 CSi TIME 275+03028 TPI TIME 605+0077 COTANGENT OF LOS TO CSM 41b+1 (ONE-HALF OFBITAL-PERIOD) 411+0 HCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT
610R TIME TO CST
43 RESET ET
267R VELOCITY TO BE GAINED CSI
402R FLTA H
371R DFLTA V CDH
5-4
372R DFLTA T CSICDH
-42 415+1 (No BORESIGHT) bO6-xXXXX RANGE RATE
-40 415+1 (NO BORESIGHT)503-XXXXX RANGE RATE dORESIGHT ON CSM
415+1 316+XXXXX RANGE
-37 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE
-15 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE UORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-2 415+1 (No BOHESIGHT) bO3-XXXXX RANGF RATE
i1uR TIME TO CS
RESEF ET
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-30 COPY ROOT FOR 1ST CSI 81J
BORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-t7 415+1 (NO BORFSIGHT) 50-XXxXx RANGF RATE
267R VELOCITY TO HE GAINED CSI
402R LELTA H
371R OFLTA V COH
372R OELTA T CSICDH
-5 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 blb+XXXXX RANGE
-i2 415+1 (No BORESIGHT) 5n3-XXXXX RANGE RATE
415+1 (NO BORESIGHT)
5-5
503-XXXXX RANGF RATE
COPY Roor FOR 2NO CSI BU
bORESIGHT ON CSM 415+1 316+XXXXX RANGE
TEMPPRESS MON SEL - FUEL MAN
A AND 8 PRESS 181 +-3 PIG TEMPPRESS MON SEL - PRPLNT
A AND B TEMP IND 4ODEG 0 IOODEG F A AND B PRFSS IND 181 +-3 PSIA
tEMPPRESS MON SEL - HEL
A AND 8 PRESS IND PSIA
A QUANTITY IND- -- PERCENT RFMAINING
8 QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4p 2 3 (120 - 190 DFG F)
415+1 (NO BORESIGHT)-17 503-XXXXX RANGE RATE
-15 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
(LOS OF MSFN) S-BAND - SLEW 10 P = +90t Y U S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
-12 415+1 (No 8ORESIGHT)
503-XXXXX RANGE RATE
267R VFLOCITY TU BE GAINED CSI
402R OFLTA H
372R TIME CSICH
371R PREDICTED VEL 10 RE GAINED COH
263R OLT-OF-PLANE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATL
-10 COPY RANGE AND ROOT FOR 3RD CSI 8U
SORESIGH ON CSM 41b+1
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
4-1
40 NOMINAL MISSION PROCEDURES
The procedures included in this section do not specify which crewmember Commander or LM Pilot performs each task These need not be specified since the following basic rules define which crewmember performs each task
41 Commander Tasks
1 All attitude changes whether manual or automatic will be accomplished by the CDR
2 The operation of the DSKY during thrust programs (P40 P41 P42 P47) will be done by the CDR Actual manipulation of the TTCA need not be always done by the CDR but in most cases will be
3 Operation of the rendezvous and landing radar will be done by the CDR
4 The CDR will operate all other systems accessible to only his crew station
42 LM Pilot Tasks
1 AGS operation 2 DSKY operation will be done by the LMP except when keyboard
entries affect the control of spacecraft attitude or thrustshying
3 Backup data logging and chart calculations 4 All logging of maneuver solutions and systems performance 5 The LMP will operate all other systems accessible to only
his crew station
These general rules are guidelines only and may be deviated from by the LM crew if they develop more efficient Task assignments
43 ABBREVIATIONS
The abbreviations used herein are consistant with those in the AOH However in order to condense and simplify the procedures so that they are representative of onboard data a number of addshyitional shorthand conventions have been used To allow the unshyfamiliar reader to understand the procedures contained in this section the following explanations are included
1 AGS - A single asterisk is employed to denote those procedures involving operations to be performed on the DEDA The three number group following an asterisk specifies DEDA address An Rfollowing the address group indicates the address is to be read out A five digit group behind the Rindicates a nominal or expected display If the three number address group is followed by a plus or minus sign a data load is indicated When a single digit follows the plus addition of four zeros behind this digit is assumed Once used these conventions are easily handled and save considerable space
4-2
2 PGNS - The verb-noun addresses in the PGNS are indicated to the left of the procedures column An F is used to indicate a flashing display or absence of an F a static display To the right of the verb-noun on the same line are the contents of the three data registers If numeric quantities appear the DSKY should be correspondingly made to agree by executing a V21 V22 or V23 and performing a data load The procedure of blanking and loading registers is not included since it is repeated often and is highly familiar to the crews
EXAMPLE F 06 33 125-02 46 TIG OF TPI
Expanded this means Load flashing verb 06 noun 33 with the quantity 125 hours 2 minutes and 46 seconds the time of ignition of the RCS engine TPI maneuver Procedurally this is done by keying verb 25 enter loading +000125 in register 1 +00002 in register 2 and +04600 in register 3
If numberic quantities do not follow the verb-noun it is indicated that a computed or information quantity is being displayed via the DSKY If nominal values are listed for possible comparison they appear in parentheses
EXAMPLE- F 06 42 HA HP V
Expanded this means Flashing verb 06 noun 42 has computed height of apogee in register 1 height of perigee in regshyister 2 and velocity to be gained in register 3
3 TIME - The numbers in the left hand column preceded by a plus or minus indicate event timer time referenced to an event Minus indicates event timer counting down to a future event Periodically this same column contains the nominal mission ground elapsed times in parentheses Asterisks following the event time indicate a time critical event which should be accomplished to the nearest second
4-3
4 4 Nominal PGNS Procedures
ASSUMPTIONS
AFTER INSERTION
1 INSERTION COMPLETE (RESIOUALS NULLED) VERIFY V82E (ORBIT) 3 RNDZ RDR LOCKED ON IN MODE II 4 LGC AT FLASHING VERB 37 5 PROPER INITIAL W MATRIX LOADED IN LGC
GUID CONT-PGNS ATTITUDE MON-PGNS(CDR) RATE ERR MON-CMPTR(LMP) ATTITUDE MON-AGS(LMP) SHFTTRUN-+5 DEG X-POINTER-HI MULT RADAR TEST SW-OFF ENG ARM-OFF X-TRANSL-2JETS DEAD BAND-MIN PGNS MODE CONT-AUTO THROTJET-JET CBPGNS IMU OPR-CLOSE RR MODE-LGC TTCATRANSL-ENABLE(COR)
BAL CPL-ON MODE SEL-AGS
RNGALT MON-RNGRNGRT RATE ERR MON-RNDZ RORICOR) ATT CONT-PULSE(3)
AGS MODE CONT-ATT HOLD ACA4JET-DISABLE(CDRJ TTCATRANSL-DISABLE(LMP)
ACA4JET-DISABLE(LMPI
KEY ODE (PO0)
(DOWNLINK LM STATE VECTOR)
KEY V63E (RR SELF TEST)
4-4
F 04 12 00004 00001 PRO
F 16 72 TRUN SHFT PRO
F 16 78 R ROOT VERIFY TAPE METER WITH DSKY
+2 VERIFY INSERTION VELOCITY WITH RNDZ ROR WHERE RANGE = 2642 NM RANGE RATE = -4251 FPS
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
KEY V34E (TERMINATE) KEY V48E (LOAD DAP)
F 01 46 11002 PRO
F 06 47 LMWT CMWT PRO
KEY V56E (KILL AUTO TRACK ENABLE)
+3 KEY V41N72E (COARSE ALIGN RR) F 21 73 +000OOTRUN -077OOSHFT F 04 12 00006 00002 (CONTINUOUS DESIGNATE)
PRO 41 (COARSE ALIGN VERB)
KEY VI6N72E 16 72 MONITOR TRUNSHFT ANGLES
CB PGNS RNDZ RDR-OPEN CB AC BUS A RNDZ RDR-OPEN KEY V44E (TERMINATE RR DESIGNATE)
KEY V83E F 16 54 R ROOT THETA
SET ORDEAL PRO
CS HEATER AOT-CLOSE
CB AOT LAMP-CLOSE
+5 KEY V37E52E (IMU REALIGN)
4-5
410+1 CSI ROUTINE 373+02065 CS TIME 275+03028 TPI TIME
605400777 COTANGENT OF LOS TO-CSM 416+1 (ONE-HALF bRBITAL PERIOD) 411+0 RCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT 310R TIME TO CS
267R VELOCITY TO BE GAINED CSI
402R DELTA H
371R DELTA V CDH
372R _ DELTA T CSICDH
F 04 06 00001 00003 -(REFSMMAT) PRO -
F 50 25 00015 SELECT 1ST STAR ENTR
F 01 70 O02DE LOAD 1ST STAR PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FOAl ANGLES (AUTO MNVRI)
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVR)
F 01 71 002DE
KEY V76E PGNS MODE CONT-ATT HOLD
PRO +10 F 54 71 MARK 1ST STAR
PRO F 01 70 O02DE LOAD 2ND STAR
PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FDA ANGLES -(AUTO MNVRV
F 50 18 FDAI ANGLES (REQUEST PNVRt ENTR (BYPASS MNVR
F 01 71 002DE PGNS MODE CONT-ATT HOLD PRO
-35
4-6
+14 F 54 71 MARK 2ND STAR PRO
F 06 05 STAR ANGLE DIFFERENCE PRO
F 06 93 GYRO TORQUE ANGLES PRO
F 50 25 00014
PRO (CHECK ALIGNMENT IF TIME WILL PERMIT)
F 50 25 00015 SELECT 3RD STAR ENTR
F 01 70 OO2DE LOAD 3RD STAR PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FDAI ANGLES (AUTO MNVR)
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVR)
VERIFY ALIGNMENT VIA AOT
KEY V34E (TERMINATE) F 37 BB
V48E (LOAD DAP) F 01 46 11012
PRO F 06 47 LMWT CMWT
+17 PRO
CB AOT LAMP-OPEN
RESET ET (310R)
(12253) CB AC BUS A RNDZ RDR-CLOSE (WAIT 30 SEC) CB PGNS RNDZ RDR-CLOSE
RR MODE-LGC KEY V37E20E (ACQUIRE RADAR)
PGNS MODE CONT-AUTO F 50 18 FDA ANGLES (REQUEST MNVRJ
PRO (AUTO MNVR) 06 18 FDAI ANGLES (AUTO MNVR)
AGS MODE CONT-AUTO RATEERR MON-CMPTR (LMP)
F 50 18 FDAI ANGLES (REQUEST MNVR)
4-7
ENTR (BYPASS MNVR) NO TRK LT-OFF
F 50 72 RR TRUNSHFT VERIFY RR LOCK ON PRO
DSKY BLANKS
KEY V93E (BEFORE 1ST MARK REINIT W MATRIXI KEY V80E (UPDATE LM SV)
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (i20OOZOO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
400+3 AGS ALIGNshy400R (00000 COMPLETE) 507+0 Z-AXIS BORESIGHT 400+2 ACQUISITION STEERING
CS
(122amp55) KEY V37E32E (CSI)
F 06 11 1 S LOAD TIG CSI FROM DATA PAD (NOM 123S26- 271 PRO
F 06 55 +O000IN +02660E +13000 OMEGAT (CDH 180 DEG AFTER CSI PRO
F 06 37 LOAD TIG TPI FROM DATA PAD (NOM 1251021761 PRO
F 16 45 MKS TFI -00001
-30 COPY RDOT FOR 1ST CSI BU
31OR TIME TO CSI
267R VELOCITY TO BE GAINED CSI
402R DELTA H
371R DELTA V CDH
-22
4-8
372R _ DELTA T CSICDH
KEY V32E (MARKS=5
F 06 75 DELTA H DELTA T CSICDH DELTA T CDHTPI PRO
F 06 81 DELTA VOS-LV (CS) (NOM 501 DELTA VX)
CSI(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (CDH)
(NOM 60 DELTA VX) CDH(82)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
KEY V32E (MARKS=1C)
F 06 75 DELTA H DELTA TCSICDH DELTA TCDHTPI PRD
F 06 81 DELTA VS-LV (CSI) CSI(N811
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 82 DELTA VIS-LV(CDH)
CDH(82)
DELTA VX(LVI
DELTA VY(LV)
DELTA VZ(LV)
-12
4-9
-20 COPY RDOT FOR 2ND CSI BU
F 16 45
F 06 75
F 06 81
F 06 16
F 06 90
PRO MKS TFI -00001
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS NON SEL - PRPLNT A + B TEMP IND 40DEG TO lOODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + 8 PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4v 2 3 (120 - 190 DEG F
(LOS OF MSFN ) S-BAND - SLEW TO P = +90 Y a 0 S-BAND - FWD (OR AFT) S-BAND - DN VOICE BU BIOMED OFF
PRO (FINAL COMP)
267R - VELOCITY TO BE GAINED CSI
402R DELTA H
372R TIME CSICDHL
371R PREDICTED VEL TO BE GAINED CDH
263R OUT-OF-PLANE
DELTA H DELTA TCSICDH DELTA TCDHTPI PRO DELTA VS-LV (CSI)
KEY V9OE (OUT-OF-PLANED
0 LOAD TIG CSI FROM DATA PAD (NOM 12302627) PRO Y YDOT PSI
N90 CSM
YDOT
PRO
-7
4-10
F 06 81 DELTA VS-LV(CSI)
COPY YDOT FROM CSM AND LOAD NEGATIVE IN R2 CSIIN81I
DELTA VX(LV)
DELTA VYILV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (COH)
CDH(82)
DELTA VX(LV)
- DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RANGE AND RDOT FOR 3RD CS BU
COMPUTE CSI BU
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (i2000OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
(TRANSMIT CSI DATA TO CSMI VHF A XMTR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF TELEMETY PCM - LO
KEY VB3E F 16 54 R ROOT THETA
SET ORDEAL PRO
317R RANGE
440R RANGE RATE
4-11
400+3 AGS ALIGN t40OR (00000 COMPLETE)
277R THETA
PRO F 37 BB
-6 KEY 41E (RCS THRUSTING) F 50 18 FDAI-ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTAV 400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTAV 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA RF
TRANSMIT TGT DELTA VS TO CSM AND SYNC COUNTDOWN
16 85 DELTA VS-BODY
502R DELTA VZ (NOM 5Ql)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTAVS-BODY
(123t26t27) BURN +Z
NULL DELTA VS
4-12
VERIFY AGS RESIDUALS 50OR 501R 502R DELTA VX _ DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
CDH
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
KEY V67E (RESET W MATRIX) F 06 99 +0200E +O0020E +00005E
PRO
507+0 Z-AXIS BORESIGHT
(VHF RANGING WITH CSM) VHF A XMTR - VOICERNG VHF B XMTR - OFF VHF B RCVR - ON TELEMETRY PCM - HI
(12331) KEY V37E33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 a TIG CDH (NOM 1242425) -120 amp00 10 (AGS 0 TIME)
(CONVERT TO MINUTES)
411+0 THRUST ALONG Z-BODY AXIS ENTER IF YOU DONT TARGET CSI
373R (NOM 26443 310R TIME TO CDH
4-13
423R DESIRED ALT RATE AT CDH
402R DELTA Hshy
450R DELTA VX
452R DELTA VZ
623+0 Z-AXIS PARALLEL TO CSM PLANE
IPRO F 16 45 MKS TFI -00001
-52 RESET ET
KEY V93E (REINIT W MATRIX WHEN MARKS =4)
KEY V32E (MARKS = 3)
F 06 75 DELTA HCDH DELTA TCDHTPI DELTA TTPI PRO
F 06 81 DELTA VCDH-LV CDH(N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
-47 KEY VSOE (OUT-OF-PLANE)
_ TIG CDH (NOM 124t24t25) -3000 TIME FROM CDH
F 06 16 l1 LOAD TIG PLANE CHANGE (NOM 123amp54-253 PRO
F 06 90 Y YDOT PSI N90 CSM
VYDOT PRO
-42 KEY V32E (MARKS=1O)
F 06 75 DELTA HCDH DELTA TCDIHTPI DELTA TTPITPI PRO
F 06 81 DELTA VCDH-LV
4-14
CDH (NS1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -OO1
KEY V34E (TERMINATE) F 37 B8
PLANE CHANGE
KEY 30E (EXTERNAL DELTA V)
TIG CDH (NOM 124124t25) -3000 TIME FROM CDH
F 06 33 LOAD TIG PLANE CHANGE (NOM 123154T25) PRO
F 06 81 DELTA VS-LV (NOM 00)
-36 COPY RDOT FOR 1ST CDH BU
KEY V90E (OUT-OF-PLANE)
F 06 16 1 1 LOAD TIG PLANE CHANGE (NOM 1231543251 PRO
F 06 90 Y YOOT PSI N90 CSM
YDOT
PRO
F 06 81 DELTA VS-LV(NOM 00)
COPY YDOT AND LOAD NEGATIVE IN R2 PRO
F 06 42 HA HP DELTA V PRO
F 16 45 MKS TFI MGA
PRO
F 37 BB
KEY 41E (RCS THRUSTING)
-30
4-15
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVRI
410+5 EXTERNAL DELTA V 450+0 451-YDOT 452+0 (LOAD CSM -YDOT)
407+0 ROTATE EXTERNAL DELTA V RF
16 95 DELTA VS-BODY
-3035 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATTVHOLD 407+1 FREEZE EXTERNAL DELTAV
F 16 85 DELTA VS-BODY -
NULL DELTA VIS
PRO F 37BB
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
507+0 Z-AXIS BORESIGHT
(12356) KEY 33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 TIG CDH (NOM 124t24t25) -120 OO ZOO (AGS 0 TIME)
(CONVERT TO MINUTES)
373R _ (NOM 2644) 310R TIME TO CDH
423R DESIRED ALT RATE AT CDH
(ADS OF MSFN) S-BAND - SLEW TOP = ACQUIRE HGA LOCK ON VOICE - BUVOICE -- VOICE VERIFY VOICE TLM BIOMED - LEFT (OR RIGHT)
402R DELTAH
4-16
F 16 45
-25
-23
F 06 75
F 06 81
F 16 45
-12
F 06 75
F 06 81
450R DELTA VX
452R DELTA VZ
PRO MKS TFI -00001
KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
COPY ROOT FOR 2ND CDH BU
KEY v32E (MARKS = 5)
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40DEG TO 1OODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + B PRESS IND PSIA
A QUANTITY IND _ PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING a TEMP MON SEL RCS QUAD 1 4 2 3 (120 - 190 DEG F)i
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
CDH(NB1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO MKS TFI -00001
PRO (FINAL COMP)
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
KEY V9OE (OUT-OF-PLANE)
-7
4-17
F 06 16 jj LOAD TIG CDH FROM DATA PAD (NOM 12424251 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT PRO
COPY YOOT FROM CSM AND LOAD NEGATIVE IN R2
CDH(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RDOT FOR 3RD CDH BU
COMPUTE CDH BU
TRANSMIT TGT DELTA VOS TO CSM AND SYNC COUNTDOWN
KEY V47E (INITIALIZE AGS F 06 16 GET OF AGS 0 TIME 120O00OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
KEY V83E F 16 54 R RDOT THETA
SET ORDEAL PRO
317R _ RANGE
440R RANGE RATE 400+3 AGS ALIGN 40OR (00000 COMPLETE)
277R THETA
-6
4-18
PRO F 3 BB
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY V06N86E F 06 86 DELTA VIS-LV
AGS(N86) CHART
DELTA VX(LVD
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
16 85 DELTA VS-BODY
50OR DELTA VX (NOM -0O3)
502R DELTA VZ (NOM 60)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD 407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS BODY
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS 5OOR 50IR 502R DELTA VX -DELTA VY DELTA VZ-
VERIFY PGNS RESIDUALS N85
DELTA VX(LM)
4-19
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
TPI
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO 507+0 Z-AXIS BORESIGHT
(12426) KEY 34E (TPI)
-36 RESET ET
F 06 37 - amp LOAD TIG TPI FROM DATA PAD (NOM 1250246) PRO
F 06 55 +00000 +02660E +13000 OMEGAT PRO
F 16 45 MARKS TFI -00001
-32 KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
-29 KEY V32E (MARKS = 3)
F 06 37 __ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
RESET ET
410+3 TPI SEARCH ROUTINE 307+04300 DELTA T TRANSFER
4-20
-26 310+02600 TFI TPI
303R THETA AT TPI
267R DELTA VTPI
371R DELTA VTPI + DELTA VTPF
KEY V32E (MARKS = 10)
F 06 37 _ _ _ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VIS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
TEMPIPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40ODEG TO IGODEG F A + B PRESS IND 181 +-3 PSIA
TEMPIPRESS MON SEL - HEL
A + B PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD I 4 2 3 (120 - 190 DEG F)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
RESET ET
-13 310+01300 TFI TPI
303R THETA AT TPI
-12 PRO (FINAL COMP) F 06 37 Z TIG TPIj__
4-21
TRANSMIT TIG OF TPI TO CSM-
PRO F 06 58 HP DELTA VTPI DELTA VTRF
PRO F 06 81 DELTA VS-LV
KEY V9OE (OUT-OF-PLANE)
F 06 16 1 LOAD TIG TPI FROM DATA PAD (NOM 12502461 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT
PRO F 06 81 DELTA VS-LV
COPY CSM YDOT AND LOAD NEGATIVE IN R2 N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 59 DELTA VS LOS
N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI MGA
RESET ET
PRO F 37 BB
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (12000t600)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE)
-10
-6
4-22
F 50 16 DOWNLINK COMPLETE PRO (UPDATE COMPLETE)
400+3 AGS ALIGN 400R (00000 COMPLETE)
-9 277R COPY TGT LOS ANGLE
310+00800
303R THETA AT TPI 410+4 DIRECT TRANSFER AT ET=-8 404+0 405+0 406+0 (MONITOR 470 471 4721
373R TIG TPI
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
KEY 41E (RCS THRUSTING) F 50 18 FOAl ANGLES (REQUEST MNVRI
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
-5 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUS
400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
COMPUTE TPI BU
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
4-23
1685 DELTA VS-BODY
50OR DELTA VX(NOM -115)
502R DELTA VZ(NOM 229)
-Z35 OSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS-BODY
(1250246) BURN +Z
VERIFY AGS RESIDUALS 500R 501R 502R DELTAVX DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
MCC1
KEY V76E (PGNS PULSE) PGNSMODECONT-AUTO
KEY V93E (BEFORE 1ST MARK REINITW MATRIX)
+2 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
4-24
(LOS OF MSFN) S-BAND - SLEW TO P = 90 Y = 0 S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
404+0 405+0 406+0
(MONITOR 470 471 4721
+9 277R COPY TGT LOS ANGLE
+12 PRO (COMPUTE MCC FOR TPI+15I F 06 81 DELTA VS-LV
PRO F 06 59 DELTA VS-LOS
PRO F 16 45 MKS TFI MGA
+13 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUOS
COMPUTE MCC1 BU
PRO F 37 BB
+14 KEY 41E (RCS THRUSTING) F 50 18 FOAL ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+1425 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+15 F 16 85 NULL DELTA VS
PRO F 37 BB
MCC2
KEY V76E (PGNS PULSE)
4-25
PGNS MODE CONT-AUTO
KEY V93E (BEFORE 1ST MARK REINIT W MATRIX)
+16 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
404+0 405+0 406+0 (MONITOR 470 471 47)shy
+24 277R COPY TGT LOS ANGLE
+27 PRO (COMPUTE MCC FORTPI+30) F 06 81 DELTA VS-LV
PRO F 06 59 DELIA VPS-LOS
PRO F 16 45 MKS TFI MGA
+28 277R COPY TGT LOS ANGLE
COPY R RDOT FROM TAPEMETER FOR BUS
COMPUTE MCC2 BU
F 37 BB PRO
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+2925 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+30 F 16 85 NULL DELTA VS
PRO F 37 BB
KEY OOE (P001
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
4-26
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT KEY V34E (TERMINATE)
KEY V37E47E (AVE G) F 16 83 DELTA VIS
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT VERIFY TAPE METER WITH DSKY
BRAKING GATE 30 FPS - 6000 FT 20 FPS - 3000 FT 10 FPS - 1500 FT 5 FPS - 600 FT
RENDEZVOUS
STATION KEEPING
5-1
50 ABORT PROCEDURE
This is a specific AGS nominal abort procedure due to a PGNS failure between insertion and station keeping
51
5-2
Nominal AGS Procedures
ASSUMPTIONS
AFTER INSERTION
I INSERTION COMPLETE (RFSIDUALS NULLED) g PGNS FAILURE BEFORE INSERTION 3 RAUAR NOT LOCKED ON
(UI CoNT-AGS ATlI[uUE MON-AGS(CDR) RATE ERR MON-CNPTR(LMP) ATTITUDE MON-AGS(LMP) SHFITRUN-+5 DEG X-POINTER-HI MULT RADAR IEST Sw-OFF LNb GMbL-OFF ENG ARM-OFF X-IRANSL-2 JETS DEAD BAND-MAX PGNS MODE CONT-OFF THROTJET-JET CB IMU OIR-ON HH MOVE-AUTO rRACK TTCATNANSL-ENABLE(CDR)
AL CPL-ON MODE SL-AGS RNGAL1 MON-RNbRNGRT RAIE ERR MON-RNDZ HDR(CDR) AVl CoNT(3)-PULSE AGS MODE CONT-AUTO ACA4JET-DISABLE(CDR) TTCATRANSL-DISABLE(LMP) ACA4JET-DISABLE(LMP)
bO7+U Z-AXIS BOPESIGHT 400+2 Z-AXIS STEERING PULSE TO NULL AGS ERRORS POINT Z-AXIS IN DIRECTION OF CSM MODE CONT-ATT HOLD ATT CONT(3)-MODE CONTROL O unnr - ZirF
5-3
SLEW PATE - LO
SLEW RR ANT TO OqON FUAI VERIFY MAX SIGNAL STRENGTH RH MOOE-AUTO TRACK NO TRACK LIGHT OFF -
ATT CONT(3h-PULSE
CHECK INSERTION VELOCITY WITH TAPEMETER COMPARE EAPEMETER WITH AGS STATE VECTOR DATA I
17R RANGE(NOM 2642)
440R RANGE RATE(NOM -425l)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
cSI
+3 417+1 (RADAR FILTER INITIALIZED) 41b+l (NO BOHESIGHT) b03-XXXXX RANGE RATE
+5 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGF
41b+1 CSI ROUTINE 373+o2065 CSi TIME 275+03028 TPI TIME 605+0077 COTANGENT OF LOS TO CSM 41b+1 (ONE-HALF OFBITAL-PERIOD) 411+0 HCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT
610R TIME TO CST
43 RESET ET
267R VELOCITY TO BE GAINED CSI
402R FLTA H
371R DFLTA V CDH
5-4
372R DFLTA T CSICDH
-42 415+1 (No BORESIGHT) bO6-xXXXX RANGE RATE
-40 415+1 (NO BORESIGHT)503-XXXXX RANGE RATE dORESIGHT ON CSM
415+1 316+XXXXX RANGE
-37 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE
-15 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE UORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-2 415+1 (No BOHESIGHT) bO3-XXXXX RANGF RATE
i1uR TIME TO CS
RESEF ET
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-30 COPY ROOT FOR 1ST CSI 81J
BORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-t7 415+1 (NO BORFSIGHT) 50-XXxXx RANGF RATE
267R VELOCITY TO HE GAINED CSI
402R LELTA H
371R OFLTA V COH
372R OELTA T CSICDH
-5 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 blb+XXXXX RANGE
-i2 415+1 (No BORESIGHT) 5n3-XXXXX RANGE RATE
415+1 (NO BORESIGHT)
5-5
503-XXXXX RANGF RATE
COPY Roor FOR 2NO CSI BU
bORESIGHT ON CSM 415+1 316+XXXXX RANGE
TEMPPRESS MON SEL - FUEL MAN
A AND 8 PRESS 181 +-3 PIG TEMPPRESS MON SEL - PRPLNT
A AND B TEMP IND 4ODEG 0 IOODEG F A AND B PRFSS IND 181 +-3 PSIA
tEMPPRESS MON SEL - HEL
A AND 8 PRESS IND PSIA
A QUANTITY IND- -- PERCENT RFMAINING
8 QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4p 2 3 (120 - 190 DFG F)
415+1 (NO BORESIGHT)-17 503-XXXXX RANGE RATE
-15 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
(LOS OF MSFN) S-BAND - SLEW 10 P = +90t Y U S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
-12 415+1 (No 8ORESIGHT)
503-XXXXX RANGE RATE
267R VFLOCITY TU BE GAINED CSI
402R OFLTA H
372R TIME CSICH
371R PREDICTED VEL 10 RE GAINED COH
263R OLT-OF-PLANE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATL
-10 COPY RANGE AND ROOT FOR 3RD CSI 8U
SORESIGH ON CSM 41b+1
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
4-2
2 PGNS - The verb-noun addresses in the PGNS are indicated to the left of the procedures column An F is used to indicate a flashing display or absence of an F a static display To the right of the verb-noun on the same line are the contents of the three data registers If numeric quantities appear the DSKY should be correspondingly made to agree by executing a V21 V22 or V23 and performing a data load The procedure of blanking and loading registers is not included since it is repeated often and is highly familiar to the crews
EXAMPLE F 06 33 125-02 46 TIG OF TPI
Expanded this means Load flashing verb 06 noun 33 with the quantity 125 hours 2 minutes and 46 seconds the time of ignition of the RCS engine TPI maneuver Procedurally this is done by keying verb 25 enter loading +000125 in register 1 +00002 in register 2 and +04600 in register 3
If numberic quantities do not follow the verb-noun it is indicated that a computed or information quantity is being displayed via the DSKY If nominal values are listed for possible comparison they appear in parentheses
EXAMPLE- F 06 42 HA HP V
Expanded this means Flashing verb 06 noun 42 has computed height of apogee in register 1 height of perigee in regshyister 2 and velocity to be gained in register 3
3 TIME - The numbers in the left hand column preceded by a plus or minus indicate event timer time referenced to an event Minus indicates event timer counting down to a future event Periodically this same column contains the nominal mission ground elapsed times in parentheses Asterisks following the event time indicate a time critical event which should be accomplished to the nearest second
4-3
4 4 Nominal PGNS Procedures
ASSUMPTIONS
AFTER INSERTION
1 INSERTION COMPLETE (RESIOUALS NULLED) VERIFY V82E (ORBIT) 3 RNDZ RDR LOCKED ON IN MODE II 4 LGC AT FLASHING VERB 37 5 PROPER INITIAL W MATRIX LOADED IN LGC
GUID CONT-PGNS ATTITUDE MON-PGNS(CDR) RATE ERR MON-CMPTR(LMP) ATTITUDE MON-AGS(LMP) SHFTTRUN-+5 DEG X-POINTER-HI MULT RADAR TEST SW-OFF ENG ARM-OFF X-TRANSL-2JETS DEAD BAND-MIN PGNS MODE CONT-AUTO THROTJET-JET CBPGNS IMU OPR-CLOSE RR MODE-LGC TTCATRANSL-ENABLE(COR)
BAL CPL-ON MODE SEL-AGS
RNGALT MON-RNGRNGRT RATE ERR MON-RNDZ RORICOR) ATT CONT-PULSE(3)
AGS MODE CONT-ATT HOLD ACA4JET-DISABLE(CDRJ TTCATRANSL-DISABLE(LMP)
ACA4JET-DISABLE(LMPI
KEY ODE (PO0)
(DOWNLINK LM STATE VECTOR)
KEY V63E (RR SELF TEST)
4-4
F 04 12 00004 00001 PRO
F 16 72 TRUN SHFT PRO
F 16 78 R ROOT VERIFY TAPE METER WITH DSKY
+2 VERIFY INSERTION VELOCITY WITH RNDZ ROR WHERE RANGE = 2642 NM RANGE RATE = -4251 FPS
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
KEY V34E (TERMINATE) KEY V48E (LOAD DAP)
F 01 46 11002 PRO
F 06 47 LMWT CMWT PRO
KEY V56E (KILL AUTO TRACK ENABLE)
+3 KEY V41N72E (COARSE ALIGN RR) F 21 73 +000OOTRUN -077OOSHFT F 04 12 00006 00002 (CONTINUOUS DESIGNATE)
PRO 41 (COARSE ALIGN VERB)
KEY VI6N72E 16 72 MONITOR TRUNSHFT ANGLES
CB PGNS RNDZ RDR-OPEN CB AC BUS A RNDZ RDR-OPEN KEY V44E (TERMINATE RR DESIGNATE)
KEY V83E F 16 54 R ROOT THETA
SET ORDEAL PRO
CS HEATER AOT-CLOSE
CB AOT LAMP-CLOSE
+5 KEY V37E52E (IMU REALIGN)
4-5
410+1 CSI ROUTINE 373+02065 CS TIME 275+03028 TPI TIME
605400777 COTANGENT OF LOS TO-CSM 416+1 (ONE-HALF bRBITAL PERIOD) 411+0 RCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT 310R TIME TO CS
267R VELOCITY TO BE GAINED CSI
402R DELTA H
371R DELTA V CDH
372R _ DELTA T CSICDH
F 04 06 00001 00003 -(REFSMMAT) PRO -
F 50 25 00015 SELECT 1ST STAR ENTR
F 01 70 O02DE LOAD 1ST STAR PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FOAl ANGLES (AUTO MNVRI)
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVR)
F 01 71 002DE
KEY V76E PGNS MODE CONT-ATT HOLD
PRO +10 F 54 71 MARK 1ST STAR
PRO F 01 70 O02DE LOAD 2ND STAR
PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FDA ANGLES -(AUTO MNVRV
F 50 18 FDAI ANGLES (REQUEST PNVRt ENTR (BYPASS MNVR
F 01 71 002DE PGNS MODE CONT-ATT HOLD PRO
-35
4-6
+14 F 54 71 MARK 2ND STAR PRO
F 06 05 STAR ANGLE DIFFERENCE PRO
F 06 93 GYRO TORQUE ANGLES PRO
F 50 25 00014
PRO (CHECK ALIGNMENT IF TIME WILL PERMIT)
F 50 25 00015 SELECT 3RD STAR ENTR
F 01 70 OO2DE LOAD 3RD STAR PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FDAI ANGLES (AUTO MNVR)
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVR)
VERIFY ALIGNMENT VIA AOT
KEY V34E (TERMINATE) F 37 BB
V48E (LOAD DAP) F 01 46 11012
PRO F 06 47 LMWT CMWT
+17 PRO
CB AOT LAMP-OPEN
RESET ET (310R)
(12253) CB AC BUS A RNDZ RDR-CLOSE (WAIT 30 SEC) CB PGNS RNDZ RDR-CLOSE
RR MODE-LGC KEY V37E20E (ACQUIRE RADAR)
PGNS MODE CONT-AUTO F 50 18 FDA ANGLES (REQUEST MNVRJ
PRO (AUTO MNVR) 06 18 FDAI ANGLES (AUTO MNVR)
AGS MODE CONT-AUTO RATEERR MON-CMPTR (LMP)
F 50 18 FDAI ANGLES (REQUEST MNVR)
4-7
ENTR (BYPASS MNVR) NO TRK LT-OFF
F 50 72 RR TRUNSHFT VERIFY RR LOCK ON PRO
DSKY BLANKS
KEY V93E (BEFORE 1ST MARK REINIT W MATRIXI KEY V80E (UPDATE LM SV)
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (i20OOZOO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
400+3 AGS ALIGNshy400R (00000 COMPLETE) 507+0 Z-AXIS BORESIGHT 400+2 ACQUISITION STEERING
CS
(122amp55) KEY V37E32E (CSI)
F 06 11 1 S LOAD TIG CSI FROM DATA PAD (NOM 123S26- 271 PRO
F 06 55 +O000IN +02660E +13000 OMEGAT (CDH 180 DEG AFTER CSI PRO
F 06 37 LOAD TIG TPI FROM DATA PAD (NOM 1251021761 PRO
F 16 45 MKS TFI -00001
-30 COPY RDOT FOR 1ST CSI BU
31OR TIME TO CSI
267R VELOCITY TO BE GAINED CSI
402R DELTA H
371R DELTA V CDH
-22
4-8
372R _ DELTA T CSICDH
KEY V32E (MARKS=5
F 06 75 DELTA H DELTA T CSICDH DELTA T CDHTPI PRO
F 06 81 DELTA VOS-LV (CS) (NOM 501 DELTA VX)
CSI(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (CDH)
(NOM 60 DELTA VX) CDH(82)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
KEY V32E (MARKS=1C)
F 06 75 DELTA H DELTA TCSICDH DELTA TCDHTPI PRD
F 06 81 DELTA VS-LV (CSI) CSI(N811
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 82 DELTA VIS-LV(CDH)
CDH(82)
DELTA VX(LVI
DELTA VY(LV)
DELTA VZ(LV)
-12
4-9
-20 COPY RDOT FOR 2ND CSI BU
F 16 45
F 06 75
F 06 81
F 06 16
F 06 90
PRO MKS TFI -00001
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS NON SEL - PRPLNT A + B TEMP IND 40DEG TO lOODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + 8 PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4v 2 3 (120 - 190 DEG F
(LOS OF MSFN ) S-BAND - SLEW TO P = +90 Y a 0 S-BAND - FWD (OR AFT) S-BAND - DN VOICE BU BIOMED OFF
PRO (FINAL COMP)
267R - VELOCITY TO BE GAINED CSI
402R DELTA H
372R TIME CSICDHL
371R PREDICTED VEL TO BE GAINED CDH
263R OUT-OF-PLANE
DELTA H DELTA TCSICDH DELTA TCDHTPI PRO DELTA VS-LV (CSI)
KEY V9OE (OUT-OF-PLANED
0 LOAD TIG CSI FROM DATA PAD (NOM 12302627) PRO Y YDOT PSI
N90 CSM
YDOT
PRO
-7
4-10
F 06 81 DELTA VS-LV(CSI)
COPY YDOT FROM CSM AND LOAD NEGATIVE IN R2 CSIIN81I
DELTA VX(LV)
DELTA VYILV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (COH)
CDH(82)
DELTA VX(LV)
- DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RANGE AND RDOT FOR 3RD CS BU
COMPUTE CSI BU
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (i2000OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
(TRANSMIT CSI DATA TO CSMI VHF A XMTR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF TELEMETY PCM - LO
KEY VB3E F 16 54 R ROOT THETA
SET ORDEAL PRO
317R RANGE
440R RANGE RATE
4-11
400+3 AGS ALIGN t40OR (00000 COMPLETE)
277R THETA
PRO F 37 BB
-6 KEY 41E (RCS THRUSTING) F 50 18 FDAI-ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTAV 400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTAV 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA RF
TRANSMIT TGT DELTA VS TO CSM AND SYNC COUNTDOWN
16 85 DELTA VS-BODY
502R DELTA VZ (NOM 5Ql)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTAVS-BODY
(123t26t27) BURN +Z
NULL DELTA VS
4-12
VERIFY AGS RESIDUALS 50OR 501R 502R DELTA VX _ DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
CDH
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
KEY V67E (RESET W MATRIX) F 06 99 +0200E +O0020E +00005E
PRO
507+0 Z-AXIS BORESIGHT
(VHF RANGING WITH CSM) VHF A XMTR - VOICERNG VHF B XMTR - OFF VHF B RCVR - ON TELEMETRY PCM - HI
(12331) KEY V37E33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 a TIG CDH (NOM 1242425) -120 amp00 10 (AGS 0 TIME)
(CONVERT TO MINUTES)
411+0 THRUST ALONG Z-BODY AXIS ENTER IF YOU DONT TARGET CSI
373R (NOM 26443 310R TIME TO CDH
4-13
423R DESIRED ALT RATE AT CDH
402R DELTA Hshy
450R DELTA VX
452R DELTA VZ
623+0 Z-AXIS PARALLEL TO CSM PLANE
IPRO F 16 45 MKS TFI -00001
-52 RESET ET
KEY V93E (REINIT W MATRIX WHEN MARKS =4)
KEY V32E (MARKS = 3)
F 06 75 DELTA HCDH DELTA TCDHTPI DELTA TTPI PRO
F 06 81 DELTA VCDH-LV CDH(N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
-47 KEY VSOE (OUT-OF-PLANE)
_ TIG CDH (NOM 124t24t25) -3000 TIME FROM CDH
F 06 16 l1 LOAD TIG PLANE CHANGE (NOM 123amp54-253 PRO
F 06 90 Y YDOT PSI N90 CSM
VYDOT PRO
-42 KEY V32E (MARKS=1O)
F 06 75 DELTA HCDH DELTA TCDIHTPI DELTA TTPITPI PRO
F 06 81 DELTA VCDH-LV
4-14
CDH (NS1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -OO1
KEY V34E (TERMINATE) F 37 B8
PLANE CHANGE
KEY 30E (EXTERNAL DELTA V)
TIG CDH (NOM 124124t25) -3000 TIME FROM CDH
F 06 33 LOAD TIG PLANE CHANGE (NOM 123154T25) PRO
F 06 81 DELTA VS-LV (NOM 00)
-36 COPY RDOT FOR 1ST CDH BU
KEY V90E (OUT-OF-PLANE)
F 06 16 1 1 LOAD TIG PLANE CHANGE (NOM 1231543251 PRO
F 06 90 Y YOOT PSI N90 CSM
YDOT
PRO
F 06 81 DELTA VS-LV(NOM 00)
COPY YDOT AND LOAD NEGATIVE IN R2 PRO
F 06 42 HA HP DELTA V PRO
F 16 45 MKS TFI MGA
PRO
F 37 BB
KEY 41E (RCS THRUSTING)
-30
4-15
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVRI
410+5 EXTERNAL DELTA V 450+0 451-YDOT 452+0 (LOAD CSM -YDOT)
407+0 ROTATE EXTERNAL DELTA V RF
16 95 DELTA VS-BODY
-3035 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATTVHOLD 407+1 FREEZE EXTERNAL DELTAV
F 16 85 DELTA VS-BODY -
NULL DELTA VIS
PRO F 37BB
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
507+0 Z-AXIS BORESIGHT
(12356) KEY 33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 TIG CDH (NOM 124t24t25) -120 OO ZOO (AGS 0 TIME)
(CONVERT TO MINUTES)
373R _ (NOM 2644) 310R TIME TO CDH
423R DESIRED ALT RATE AT CDH
(ADS OF MSFN) S-BAND - SLEW TOP = ACQUIRE HGA LOCK ON VOICE - BUVOICE -- VOICE VERIFY VOICE TLM BIOMED - LEFT (OR RIGHT)
402R DELTAH
4-16
F 16 45
-25
-23
F 06 75
F 06 81
F 16 45
-12
F 06 75
F 06 81
450R DELTA VX
452R DELTA VZ
PRO MKS TFI -00001
KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
COPY ROOT FOR 2ND CDH BU
KEY v32E (MARKS = 5)
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40DEG TO 1OODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + B PRESS IND PSIA
A QUANTITY IND _ PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING a TEMP MON SEL RCS QUAD 1 4 2 3 (120 - 190 DEG F)i
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
CDH(NB1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO MKS TFI -00001
PRO (FINAL COMP)
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
KEY V9OE (OUT-OF-PLANE)
-7
4-17
F 06 16 jj LOAD TIG CDH FROM DATA PAD (NOM 12424251 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT PRO
COPY YOOT FROM CSM AND LOAD NEGATIVE IN R2
CDH(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RDOT FOR 3RD CDH BU
COMPUTE CDH BU
TRANSMIT TGT DELTA VOS TO CSM AND SYNC COUNTDOWN
KEY V47E (INITIALIZE AGS F 06 16 GET OF AGS 0 TIME 120O00OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
KEY V83E F 16 54 R RDOT THETA
SET ORDEAL PRO
317R _ RANGE
440R RANGE RATE 400+3 AGS ALIGN 40OR (00000 COMPLETE)
277R THETA
-6
4-18
PRO F 3 BB
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY V06N86E F 06 86 DELTA VIS-LV
AGS(N86) CHART
DELTA VX(LVD
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
16 85 DELTA VS-BODY
50OR DELTA VX (NOM -0O3)
502R DELTA VZ (NOM 60)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD 407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS BODY
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS 5OOR 50IR 502R DELTA VX -DELTA VY DELTA VZ-
VERIFY PGNS RESIDUALS N85
DELTA VX(LM)
4-19
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
TPI
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO 507+0 Z-AXIS BORESIGHT
(12426) KEY 34E (TPI)
-36 RESET ET
F 06 37 - amp LOAD TIG TPI FROM DATA PAD (NOM 1250246) PRO
F 06 55 +00000 +02660E +13000 OMEGAT PRO
F 16 45 MARKS TFI -00001
-32 KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
-29 KEY V32E (MARKS = 3)
F 06 37 __ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
RESET ET
410+3 TPI SEARCH ROUTINE 307+04300 DELTA T TRANSFER
4-20
-26 310+02600 TFI TPI
303R THETA AT TPI
267R DELTA VTPI
371R DELTA VTPI + DELTA VTPF
KEY V32E (MARKS = 10)
F 06 37 _ _ _ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VIS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
TEMPIPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40ODEG TO IGODEG F A + B PRESS IND 181 +-3 PSIA
TEMPIPRESS MON SEL - HEL
A + B PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD I 4 2 3 (120 - 190 DEG F)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
RESET ET
-13 310+01300 TFI TPI
303R THETA AT TPI
-12 PRO (FINAL COMP) F 06 37 Z TIG TPIj__
4-21
TRANSMIT TIG OF TPI TO CSM-
PRO F 06 58 HP DELTA VTPI DELTA VTRF
PRO F 06 81 DELTA VS-LV
KEY V9OE (OUT-OF-PLANE)
F 06 16 1 LOAD TIG TPI FROM DATA PAD (NOM 12502461 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT
PRO F 06 81 DELTA VS-LV
COPY CSM YDOT AND LOAD NEGATIVE IN R2 N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 59 DELTA VS LOS
N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI MGA
RESET ET
PRO F 37 BB
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (12000t600)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE)
-10
-6
4-22
F 50 16 DOWNLINK COMPLETE PRO (UPDATE COMPLETE)
400+3 AGS ALIGN 400R (00000 COMPLETE)
-9 277R COPY TGT LOS ANGLE
310+00800
303R THETA AT TPI 410+4 DIRECT TRANSFER AT ET=-8 404+0 405+0 406+0 (MONITOR 470 471 4721
373R TIG TPI
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
KEY 41E (RCS THRUSTING) F 50 18 FOAl ANGLES (REQUEST MNVRI
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
-5 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUS
400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
COMPUTE TPI BU
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
4-23
1685 DELTA VS-BODY
50OR DELTA VX(NOM -115)
502R DELTA VZ(NOM 229)
-Z35 OSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS-BODY
(1250246) BURN +Z
VERIFY AGS RESIDUALS 500R 501R 502R DELTAVX DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
MCC1
KEY V76E (PGNS PULSE) PGNSMODECONT-AUTO
KEY V93E (BEFORE 1ST MARK REINITW MATRIX)
+2 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
4-24
(LOS OF MSFN) S-BAND - SLEW TO P = 90 Y = 0 S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
404+0 405+0 406+0
(MONITOR 470 471 4721
+9 277R COPY TGT LOS ANGLE
+12 PRO (COMPUTE MCC FOR TPI+15I F 06 81 DELTA VS-LV
PRO F 06 59 DELTA VS-LOS
PRO F 16 45 MKS TFI MGA
+13 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUOS
COMPUTE MCC1 BU
PRO F 37 BB
+14 KEY 41E (RCS THRUSTING) F 50 18 FOAL ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+1425 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+15 F 16 85 NULL DELTA VS
PRO F 37 BB
MCC2
KEY V76E (PGNS PULSE)
4-25
PGNS MODE CONT-AUTO
KEY V93E (BEFORE 1ST MARK REINIT W MATRIX)
+16 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
404+0 405+0 406+0 (MONITOR 470 471 47)shy
+24 277R COPY TGT LOS ANGLE
+27 PRO (COMPUTE MCC FORTPI+30) F 06 81 DELTA VS-LV
PRO F 06 59 DELIA VPS-LOS
PRO F 16 45 MKS TFI MGA
+28 277R COPY TGT LOS ANGLE
COPY R RDOT FROM TAPEMETER FOR BUS
COMPUTE MCC2 BU
F 37 BB PRO
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+2925 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+30 F 16 85 NULL DELTA VS
PRO F 37 BB
KEY OOE (P001
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
4-26
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT KEY V34E (TERMINATE)
KEY V37E47E (AVE G) F 16 83 DELTA VIS
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT VERIFY TAPE METER WITH DSKY
BRAKING GATE 30 FPS - 6000 FT 20 FPS - 3000 FT 10 FPS - 1500 FT 5 FPS - 600 FT
RENDEZVOUS
STATION KEEPING
5-1
50 ABORT PROCEDURE
This is a specific AGS nominal abort procedure due to a PGNS failure between insertion and station keeping
51
5-2
Nominal AGS Procedures
ASSUMPTIONS
AFTER INSERTION
I INSERTION COMPLETE (RFSIDUALS NULLED) g PGNS FAILURE BEFORE INSERTION 3 RAUAR NOT LOCKED ON
(UI CoNT-AGS ATlI[uUE MON-AGS(CDR) RATE ERR MON-CNPTR(LMP) ATTITUDE MON-AGS(LMP) SHFITRUN-+5 DEG X-POINTER-HI MULT RADAR IEST Sw-OFF LNb GMbL-OFF ENG ARM-OFF X-IRANSL-2 JETS DEAD BAND-MAX PGNS MODE CONT-OFF THROTJET-JET CB IMU OIR-ON HH MOVE-AUTO rRACK TTCATNANSL-ENABLE(CDR)
AL CPL-ON MODE SL-AGS RNGAL1 MON-RNbRNGRT RAIE ERR MON-RNDZ HDR(CDR) AVl CoNT(3)-PULSE AGS MODE CONT-AUTO ACA4JET-DISABLE(CDR) TTCATRANSL-DISABLE(LMP) ACA4JET-DISABLE(LMP)
bO7+U Z-AXIS BOPESIGHT 400+2 Z-AXIS STEERING PULSE TO NULL AGS ERRORS POINT Z-AXIS IN DIRECTION OF CSM MODE CONT-ATT HOLD ATT CONT(3)-MODE CONTROL O unnr - ZirF
5-3
SLEW PATE - LO
SLEW RR ANT TO OqON FUAI VERIFY MAX SIGNAL STRENGTH RH MOOE-AUTO TRACK NO TRACK LIGHT OFF -
ATT CONT(3h-PULSE
CHECK INSERTION VELOCITY WITH TAPEMETER COMPARE EAPEMETER WITH AGS STATE VECTOR DATA I
17R RANGE(NOM 2642)
440R RANGE RATE(NOM -425l)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
cSI
+3 417+1 (RADAR FILTER INITIALIZED) 41b+l (NO BOHESIGHT) b03-XXXXX RANGE RATE
+5 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGF
41b+1 CSI ROUTINE 373+o2065 CSi TIME 275+03028 TPI TIME 605+0077 COTANGENT OF LOS TO CSM 41b+1 (ONE-HALF OFBITAL-PERIOD) 411+0 HCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT
610R TIME TO CST
43 RESET ET
267R VELOCITY TO BE GAINED CSI
402R FLTA H
371R DFLTA V CDH
5-4
372R DFLTA T CSICDH
-42 415+1 (No BORESIGHT) bO6-xXXXX RANGE RATE
-40 415+1 (NO BORESIGHT)503-XXXXX RANGE RATE dORESIGHT ON CSM
415+1 316+XXXXX RANGE
-37 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE
-15 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE UORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-2 415+1 (No BOHESIGHT) bO3-XXXXX RANGF RATE
i1uR TIME TO CS
RESEF ET
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-30 COPY ROOT FOR 1ST CSI 81J
BORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-t7 415+1 (NO BORFSIGHT) 50-XXxXx RANGF RATE
267R VELOCITY TO HE GAINED CSI
402R LELTA H
371R OFLTA V COH
372R OELTA T CSICDH
-5 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 blb+XXXXX RANGE
-i2 415+1 (No BORESIGHT) 5n3-XXXXX RANGE RATE
415+1 (NO BORESIGHT)
5-5
503-XXXXX RANGF RATE
COPY Roor FOR 2NO CSI BU
bORESIGHT ON CSM 415+1 316+XXXXX RANGE
TEMPPRESS MON SEL - FUEL MAN
A AND 8 PRESS 181 +-3 PIG TEMPPRESS MON SEL - PRPLNT
A AND B TEMP IND 4ODEG 0 IOODEG F A AND B PRFSS IND 181 +-3 PSIA
tEMPPRESS MON SEL - HEL
A AND 8 PRESS IND PSIA
A QUANTITY IND- -- PERCENT RFMAINING
8 QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4p 2 3 (120 - 190 DFG F)
415+1 (NO BORESIGHT)-17 503-XXXXX RANGE RATE
-15 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
(LOS OF MSFN) S-BAND - SLEW 10 P = +90t Y U S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
-12 415+1 (No 8ORESIGHT)
503-XXXXX RANGE RATE
267R VFLOCITY TU BE GAINED CSI
402R OFLTA H
372R TIME CSICH
371R PREDICTED VEL 10 RE GAINED COH
263R OLT-OF-PLANE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATL
-10 COPY RANGE AND ROOT FOR 3RD CSI 8U
SORESIGH ON CSM 41b+1
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
4-3
4 4 Nominal PGNS Procedures
ASSUMPTIONS
AFTER INSERTION
1 INSERTION COMPLETE (RESIOUALS NULLED) VERIFY V82E (ORBIT) 3 RNDZ RDR LOCKED ON IN MODE II 4 LGC AT FLASHING VERB 37 5 PROPER INITIAL W MATRIX LOADED IN LGC
GUID CONT-PGNS ATTITUDE MON-PGNS(CDR) RATE ERR MON-CMPTR(LMP) ATTITUDE MON-AGS(LMP) SHFTTRUN-+5 DEG X-POINTER-HI MULT RADAR TEST SW-OFF ENG ARM-OFF X-TRANSL-2JETS DEAD BAND-MIN PGNS MODE CONT-AUTO THROTJET-JET CBPGNS IMU OPR-CLOSE RR MODE-LGC TTCATRANSL-ENABLE(COR)
BAL CPL-ON MODE SEL-AGS
RNGALT MON-RNGRNGRT RATE ERR MON-RNDZ RORICOR) ATT CONT-PULSE(3)
AGS MODE CONT-ATT HOLD ACA4JET-DISABLE(CDRJ TTCATRANSL-DISABLE(LMP)
ACA4JET-DISABLE(LMPI
KEY ODE (PO0)
(DOWNLINK LM STATE VECTOR)
KEY V63E (RR SELF TEST)
4-4
F 04 12 00004 00001 PRO
F 16 72 TRUN SHFT PRO
F 16 78 R ROOT VERIFY TAPE METER WITH DSKY
+2 VERIFY INSERTION VELOCITY WITH RNDZ ROR WHERE RANGE = 2642 NM RANGE RATE = -4251 FPS
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
KEY V34E (TERMINATE) KEY V48E (LOAD DAP)
F 01 46 11002 PRO
F 06 47 LMWT CMWT PRO
KEY V56E (KILL AUTO TRACK ENABLE)
+3 KEY V41N72E (COARSE ALIGN RR) F 21 73 +000OOTRUN -077OOSHFT F 04 12 00006 00002 (CONTINUOUS DESIGNATE)
PRO 41 (COARSE ALIGN VERB)
KEY VI6N72E 16 72 MONITOR TRUNSHFT ANGLES
CB PGNS RNDZ RDR-OPEN CB AC BUS A RNDZ RDR-OPEN KEY V44E (TERMINATE RR DESIGNATE)
KEY V83E F 16 54 R ROOT THETA
SET ORDEAL PRO
CS HEATER AOT-CLOSE
CB AOT LAMP-CLOSE
+5 KEY V37E52E (IMU REALIGN)
4-5
410+1 CSI ROUTINE 373+02065 CS TIME 275+03028 TPI TIME
605400777 COTANGENT OF LOS TO-CSM 416+1 (ONE-HALF bRBITAL PERIOD) 411+0 RCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT 310R TIME TO CS
267R VELOCITY TO BE GAINED CSI
402R DELTA H
371R DELTA V CDH
372R _ DELTA T CSICDH
F 04 06 00001 00003 -(REFSMMAT) PRO -
F 50 25 00015 SELECT 1ST STAR ENTR
F 01 70 O02DE LOAD 1ST STAR PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FOAl ANGLES (AUTO MNVRI)
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVR)
F 01 71 002DE
KEY V76E PGNS MODE CONT-ATT HOLD
PRO +10 F 54 71 MARK 1ST STAR
PRO F 01 70 O02DE LOAD 2ND STAR
PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FDA ANGLES -(AUTO MNVRV
F 50 18 FDAI ANGLES (REQUEST PNVRt ENTR (BYPASS MNVR
F 01 71 002DE PGNS MODE CONT-ATT HOLD PRO
-35
4-6
+14 F 54 71 MARK 2ND STAR PRO
F 06 05 STAR ANGLE DIFFERENCE PRO
F 06 93 GYRO TORQUE ANGLES PRO
F 50 25 00014
PRO (CHECK ALIGNMENT IF TIME WILL PERMIT)
F 50 25 00015 SELECT 3RD STAR ENTR
F 01 70 OO2DE LOAD 3RD STAR PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FDAI ANGLES (AUTO MNVR)
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVR)
VERIFY ALIGNMENT VIA AOT
KEY V34E (TERMINATE) F 37 BB
V48E (LOAD DAP) F 01 46 11012
PRO F 06 47 LMWT CMWT
+17 PRO
CB AOT LAMP-OPEN
RESET ET (310R)
(12253) CB AC BUS A RNDZ RDR-CLOSE (WAIT 30 SEC) CB PGNS RNDZ RDR-CLOSE
RR MODE-LGC KEY V37E20E (ACQUIRE RADAR)
PGNS MODE CONT-AUTO F 50 18 FDA ANGLES (REQUEST MNVRJ
PRO (AUTO MNVR) 06 18 FDAI ANGLES (AUTO MNVR)
AGS MODE CONT-AUTO RATEERR MON-CMPTR (LMP)
F 50 18 FDAI ANGLES (REQUEST MNVR)
4-7
ENTR (BYPASS MNVR) NO TRK LT-OFF
F 50 72 RR TRUNSHFT VERIFY RR LOCK ON PRO
DSKY BLANKS
KEY V93E (BEFORE 1ST MARK REINIT W MATRIXI KEY V80E (UPDATE LM SV)
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (i20OOZOO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
400+3 AGS ALIGNshy400R (00000 COMPLETE) 507+0 Z-AXIS BORESIGHT 400+2 ACQUISITION STEERING
CS
(122amp55) KEY V37E32E (CSI)
F 06 11 1 S LOAD TIG CSI FROM DATA PAD (NOM 123S26- 271 PRO
F 06 55 +O000IN +02660E +13000 OMEGAT (CDH 180 DEG AFTER CSI PRO
F 06 37 LOAD TIG TPI FROM DATA PAD (NOM 1251021761 PRO
F 16 45 MKS TFI -00001
-30 COPY RDOT FOR 1ST CSI BU
31OR TIME TO CSI
267R VELOCITY TO BE GAINED CSI
402R DELTA H
371R DELTA V CDH
-22
4-8
372R _ DELTA T CSICDH
KEY V32E (MARKS=5
F 06 75 DELTA H DELTA T CSICDH DELTA T CDHTPI PRO
F 06 81 DELTA VOS-LV (CS) (NOM 501 DELTA VX)
CSI(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (CDH)
(NOM 60 DELTA VX) CDH(82)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
KEY V32E (MARKS=1C)
F 06 75 DELTA H DELTA TCSICDH DELTA TCDHTPI PRD
F 06 81 DELTA VS-LV (CSI) CSI(N811
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 82 DELTA VIS-LV(CDH)
CDH(82)
DELTA VX(LVI
DELTA VY(LV)
DELTA VZ(LV)
-12
4-9
-20 COPY RDOT FOR 2ND CSI BU
F 16 45
F 06 75
F 06 81
F 06 16
F 06 90
PRO MKS TFI -00001
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS NON SEL - PRPLNT A + B TEMP IND 40DEG TO lOODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + 8 PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4v 2 3 (120 - 190 DEG F
(LOS OF MSFN ) S-BAND - SLEW TO P = +90 Y a 0 S-BAND - FWD (OR AFT) S-BAND - DN VOICE BU BIOMED OFF
PRO (FINAL COMP)
267R - VELOCITY TO BE GAINED CSI
402R DELTA H
372R TIME CSICDHL
371R PREDICTED VEL TO BE GAINED CDH
263R OUT-OF-PLANE
DELTA H DELTA TCSICDH DELTA TCDHTPI PRO DELTA VS-LV (CSI)
KEY V9OE (OUT-OF-PLANED
0 LOAD TIG CSI FROM DATA PAD (NOM 12302627) PRO Y YDOT PSI
N90 CSM
YDOT
PRO
-7
4-10
F 06 81 DELTA VS-LV(CSI)
COPY YDOT FROM CSM AND LOAD NEGATIVE IN R2 CSIIN81I
DELTA VX(LV)
DELTA VYILV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (COH)
CDH(82)
DELTA VX(LV)
- DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RANGE AND RDOT FOR 3RD CS BU
COMPUTE CSI BU
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (i2000OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
(TRANSMIT CSI DATA TO CSMI VHF A XMTR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF TELEMETY PCM - LO
KEY VB3E F 16 54 R ROOT THETA
SET ORDEAL PRO
317R RANGE
440R RANGE RATE
4-11
400+3 AGS ALIGN t40OR (00000 COMPLETE)
277R THETA
PRO F 37 BB
-6 KEY 41E (RCS THRUSTING) F 50 18 FDAI-ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTAV 400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTAV 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA RF
TRANSMIT TGT DELTA VS TO CSM AND SYNC COUNTDOWN
16 85 DELTA VS-BODY
502R DELTA VZ (NOM 5Ql)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTAVS-BODY
(123t26t27) BURN +Z
NULL DELTA VS
4-12
VERIFY AGS RESIDUALS 50OR 501R 502R DELTA VX _ DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
CDH
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
KEY V67E (RESET W MATRIX) F 06 99 +0200E +O0020E +00005E
PRO
507+0 Z-AXIS BORESIGHT
(VHF RANGING WITH CSM) VHF A XMTR - VOICERNG VHF B XMTR - OFF VHF B RCVR - ON TELEMETRY PCM - HI
(12331) KEY V37E33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 a TIG CDH (NOM 1242425) -120 amp00 10 (AGS 0 TIME)
(CONVERT TO MINUTES)
411+0 THRUST ALONG Z-BODY AXIS ENTER IF YOU DONT TARGET CSI
373R (NOM 26443 310R TIME TO CDH
4-13
423R DESIRED ALT RATE AT CDH
402R DELTA Hshy
450R DELTA VX
452R DELTA VZ
623+0 Z-AXIS PARALLEL TO CSM PLANE
IPRO F 16 45 MKS TFI -00001
-52 RESET ET
KEY V93E (REINIT W MATRIX WHEN MARKS =4)
KEY V32E (MARKS = 3)
F 06 75 DELTA HCDH DELTA TCDHTPI DELTA TTPI PRO
F 06 81 DELTA VCDH-LV CDH(N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
-47 KEY VSOE (OUT-OF-PLANE)
_ TIG CDH (NOM 124t24t25) -3000 TIME FROM CDH
F 06 16 l1 LOAD TIG PLANE CHANGE (NOM 123amp54-253 PRO
F 06 90 Y YDOT PSI N90 CSM
VYDOT PRO
-42 KEY V32E (MARKS=1O)
F 06 75 DELTA HCDH DELTA TCDIHTPI DELTA TTPITPI PRO
F 06 81 DELTA VCDH-LV
4-14
CDH (NS1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -OO1
KEY V34E (TERMINATE) F 37 B8
PLANE CHANGE
KEY 30E (EXTERNAL DELTA V)
TIG CDH (NOM 124124t25) -3000 TIME FROM CDH
F 06 33 LOAD TIG PLANE CHANGE (NOM 123154T25) PRO
F 06 81 DELTA VS-LV (NOM 00)
-36 COPY RDOT FOR 1ST CDH BU
KEY V90E (OUT-OF-PLANE)
F 06 16 1 1 LOAD TIG PLANE CHANGE (NOM 1231543251 PRO
F 06 90 Y YOOT PSI N90 CSM
YDOT
PRO
F 06 81 DELTA VS-LV(NOM 00)
COPY YDOT AND LOAD NEGATIVE IN R2 PRO
F 06 42 HA HP DELTA V PRO
F 16 45 MKS TFI MGA
PRO
F 37 BB
KEY 41E (RCS THRUSTING)
-30
4-15
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVRI
410+5 EXTERNAL DELTA V 450+0 451-YDOT 452+0 (LOAD CSM -YDOT)
407+0 ROTATE EXTERNAL DELTA V RF
16 95 DELTA VS-BODY
-3035 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATTVHOLD 407+1 FREEZE EXTERNAL DELTAV
F 16 85 DELTA VS-BODY -
NULL DELTA VIS
PRO F 37BB
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
507+0 Z-AXIS BORESIGHT
(12356) KEY 33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 TIG CDH (NOM 124t24t25) -120 OO ZOO (AGS 0 TIME)
(CONVERT TO MINUTES)
373R _ (NOM 2644) 310R TIME TO CDH
423R DESIRED ALT RATE AT CDH
(ADS OF MSFN) S-BAND - SLEW TOP = ACQUIRE HGA LOCK ON VOICE - BUVOICE -- VOICE VERIFY VOICE TLM BIOMED - LEFT (OR RIGHT)
402R DELTAH
4-16
F 16 45
-25
-23
F 06 75
F 06 81
F 16 45
-12
F 06 75
F 06 81
450R DELTA VX
452R DELTA VZ
PRO MKS TFI -00001
KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
COPY ROOT FOR 2ND CDH BU
KEY v32E (MARKS = 5)
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40DEG TO 1OODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + B PRESS IND PSIA
A QUANTITY IND _ PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING a TEMP MON SEL RCS QUAD 1 4 2 3 (120 - 190 DEG F)i
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
CDH(NB1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO MKS TFI -00001
PRO (FINAL COMP)
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
KEY V9OE (OUT-OF-PLANE)
-7
4-17
F 06 16 jj LOAD TIG CDH FROM DATA PAD (NOM 12424251 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT PRO
COPY YOOT FROM CSM AND LOAD NEGATIVE IN R2
CDH(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RDOT FOR 3RD CDH BU
COMPUTE CDH BU
TRANSMIT TGT DELTA VOS TO CSM AND SYNC COUNTDOWN
KEY V47E (INITIALIZE AGS F 06 16 GET OF AGS 0 TIME 120O00OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
KEY V83E F 16 54 R RDOT THETA
SET ORDEAL PRO
317R _ RANGE
440R RANGE RATE 400+3 AGS ALIGN 40OR (00000 COMPLETE)
277R THETA
-6
4-18
PRO F 3 BB
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY V06N86E F 06 86 DELTA VIS-LV
AGS(N86) CHART
DELTA VX(LVD
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
16 85 DELTA VS-BODY
50OR DELTA VX (NOM -0O3)
502R DELTA VZ (NOM 60)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD 407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS BODY
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS 5OOR 50IR 502R DELTA VX -DELTA VY DELTA VZ-
VERIFY PGNS RESIDUALS N85
DELTA VX(LM)
4-19
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
TPI
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO 507+0 Z-AXIS BORESIGHT
(12426) KEY 34E (TPI)
-36 RESET ET
F 06 37 - amp LOAD TIG TPI FROM DATA PAD (NOM 1250246) PRO
F 06 55 +00000 +02660E +13000 OMEGAT PRO
F 16 45 MARKS TFI -00001
-32 KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
-29 KEY V32E (MARKS = 3)
F 06 37 __ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
RESET ET
410+3 TPI SEARCH ROUTINE 307+04300 DELTA T TRANSFER
4-20
-26 310+02600 TFI TPI
303R THETA AT TPI
267R DELTA VTPI
371R DELTA VTPI + DELTA VTPF
KEY V32E (MARKS = 10)
F 06 37 _ _ _ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VIS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
TEMPIPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40ODEG TO IGODEG F A + B PRESS IND 181 +-3 PSIA
TEMPIPRESS MON SEL - HEL
A + B PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD I 4 2 3 (120 - 190 DEG F)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
RESET ET
-13 310+01300 TFI TPI
303R THETA AT TPI
-12 PRO (FINAL COMP) F 06 37 Z TIG TPIj__
4-21
TRANSMIT TIG OF TPI TO CSM-
PRO F 06 58 HP DELTA VTPI DELTA VTRF
PRO F 06 81 DELTA VS-LV
KEY V9OE (OUT-OF-PLANE)
F 06 16 1 LOAD TIG TPI FROM DATA PAD (NOM 12502461 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT
PRO F 06 81 DELTA VS-LV
COPY CSM YDOT AND LOAD NEGATIVE IN R2 N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 59 DELTA VS LOS
N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI MGA
RESET ET
PRO F 37 BB
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (12000t600)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE)
-10
-6
4-22
F 50 16 DOWNLINK COMPLETE PRO (UPDATE COMPLETE)
400+3 AGS ALIGN 400R (00000 COMPLETE)
-9 277R COPY TGT LOS ANGLE
310+00800
303R THETA AT TPI 410+4 DIRECT TRANSFER AT ET=-8 404+0 405+0 406+0 (MONITOR 470 471 4721
373R TIG TPI
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
KEY 41E (RCS THRUSTING) F 50 18 FOAl ANGLES (REQUEST MNVRI
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
-5 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUS
400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
COMPUTE TPI BU
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
4-23
1685 DELTA VS-BODY
50OR DELTA VX(NOM -115)
502R DELTA VZ(NOM 229)
-Z35 OSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS-BODY
(1250246) BURN +Z
VERIFY AGS RESIDUALS 500R 501R 502R DELTAVX DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
MCC1
KEY V76E (PGNS PULSE) PGNSMODECONT-AUTO
KEY V93E (BEFORE 1ST MARK REINITW MATRIX)
+2 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
4-24
(LOS OF MSFN) S-BAND - SLEW TO P = 90 Y = 0 S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
404+0 405+0 406+0
(MONITOR 470 471 4721
+9 277R COPY TGT LOS ANGLE
+12 PRO (COMPUTE MCC FOR TPI+15I F 06 81 DELTA VS-LV
PRO F 06 59 DELTA VS-LOS
PRO F 16 45 MKS TFI MGA
+13 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUOS
COMPUTE MCC1 BU
PRO F 37 BB
+14 KEY 41E (RCS THRUSTING) F 50 18 FOAL ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+1425 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+15 F 16 85 NULL DELTA VS
PRO F 37 BB
MCC2
KEY V76E (PGNS PULSE)
4-25
PGNS MODE CONT-AUTO
KEY V93E (BEFORE 1ST MARK REINIT W MATRIX)
+16 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
404+0 405+0 406+0 (MONITOR 470 471 47)shy
+24 277R COPY TGT LOS ANGLE
+27 PRO (COMPUTE MCC FORTPI+30) F 06 81 DELTA VS-LV
PRO F 06 59 DELIA VPS-LOS
PRO F 16 45 MKS TFI MGA
+28 277R COPY TGT LOS ANGLE
COPY R RDOT FROM TAPEMETER FOR BUS
COMPUTE MCC2 BU
F 37 BB PRO
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+2925 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+30 F 16 85 NULL DELTA VS
PRO F 37 BB
KEY OOE (P001
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
4-26
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT KEY V34E (TERMINATE)
KEY V37E47E (AVE G) F 16 83 DELTA VIS
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT VERIFY TAPE METER WITH DSKY
BRAKING GATE 30 FPS - 6000 FT 20 FPS - 3000 FT 10 FPS - 1500 FT 5 FPS - 600 FT
RENDEZVOUS
STATION KEEPING
5-1
50 ABORT PROCEDURE
This is a specific AGS nominal abort procedure due to a PGNS failure between insertion and station keeping
51
5-2
Nominal AGS Procedures
ASSUMPTIONS
AFTER INSERTION
I INSERTION COMPLETE (RFSIDUALS NULLED) g PGNS FAILURE BEFORE INSERTION 3 RAUAR NOT LOCKED ON
(UI CoNT-AGS ATlI[uUE MON-AGS(CDR) RATE ERR MON-CNPTR(LMP) ATTITUDE MON-AGS(LMP) SHFITRUN-+5 DEG X-POINTER-HI MULT RADAR IEST Sw-OFF LNb GMbL-OFF ENG ARM-OFF X-IRANSL-2 JETS DEAD BAND-MAX PGNS MODE CONT-OFF THROTJET-JET CB IMU OIR-ON HH MOVE-AUTO rRACK TTCATNANSL-ENABLE(CDR)
AL CPL-ON MODE SL-AGS RNGAL1 MON-RNbRNGRT RAIE ERR MON-RNDZ HDR(CDR) AVl CoNT(3)-PULSE AGS MODE CONT-AUTO ACA4JET-DISABLE(CDR) TTCATRANSL-DISABLE(LMP) ACA4JET-DISABLE(LMP)
bO7+U Z-AXIS BOPESIGHT 400+2 Z-AXIS STEERING PULSE TO NULL AGS ERRORS POINT Z-AXIS IN DIRECTION OF CSM MODE CONT-ATT HOLD ATT CONT(3)-MODE CONTROL O unnr - ZirF
5-3
SLEW PATE - LO
SLEW RR ANT TO OqON FUAI VERIFY MAX SIGNAL STRENGTH RH MOOE-AUTO TRACK NO TRACK LIGHT OFF -
ATT CONT(3h-PULSE
CHECK INSERTION VELOCITY WITH TAPEMETER COMPARE EAPEMETER WITH AGS STATE VECTOR DATA I
17R RANGE(NOM 2642)
440R RANGE RATE(NOM -425l)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
cSI
+3 417+1 (RADAR FILTER INITIALIZED) 41b+l (NO BOHESIGHT) b03-XXXXX RANGE RATE
+5 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGF
41b+1 CSI ROUTINE 373+o2065 CSi TIME 275+03028 TPI TIME 605+0077 COTANGENT OF LOS TO CSM 41b+1 (ONE-HALF OFBITAL-PERIOD) 411+0 HCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT
610R TIME TO CST
43 RESET ET
267R VELOCITY TO BE GAINED CSI
402R FLTA H
371R DFLTA V CDH
5-4
372R DFLTA T CSICDH
-42 415+1 (No BORESIGHT) bO6-xXXXX RANGE RATE
-40 415+1 (NO BORESIGHT)503-XXXXX RANGE RATE dORESIGHT ON CSM
415+1 316+XXXXX RANGE
-37 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE
-15 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE UORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-2 415+1 (No BOHESIGHT) bO3-XXXXX RANGF RATE
i1uR TIME TO CS
RESEF ET
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-30 COPY ROOT FOR 1ST CSI 81J
BORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-t7 415+1 (NO BORFSIGHT) 50-XXxXx RANGF RATE
267R VELOCITY TO HE GAINED CSI
402R LELTA H
371R OFLTA V COH
372R OELTA T CSICDH
-5 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 blb+XXXXX RANGE
-i2 415+1 (No BORESIGHT) 5n3-XXXXX RANGE RATE
415+1 (NO BORESIGHT)
5-5
503-XXXXX RANGF RATE
COPY Roor FOR 2NO CSI BU
bORESIGHT ON CSM 415+1 316+XXXXX RANGE
TEMPPRESS MON SEL - FUEL MAN
A AND 8 PRESS 181 +-3 PIG TEMPPRESS MON SEL - PRPLNT
A AND B TEMP IND 4ODEG 0 IOODEG F A AND B PRFSS IND 181 +-3 PSIA
tEMPPRESS MON SEL - HEL
A AND 8 PRESS IND PSIA
A QUANTITY IND- -- PERCENT RFMAINING
8 QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4p 2 3 (120 - 190 DFG F)
415+1 (NO BORESIGHT)-17 503-XXXXX RANGE RATE
-15 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
(LOS OF MSFN) S-BAND - SLEW 10 P = +90t Y U S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
-12 415+1 (No 8ORESIGHT)
503-XXXXX RANGE RATE
267R VFLOCITY TU BE GAINED CSI
402R OFLTA H
372R TIME CSICH
371R PREDICTED VEL 10 RE GAINED COH
263R OLT-OF-PLANE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATL
-10 COPY RANGE AND ROOT FOR 3RD CSI 8U
SORESIGH ON CSM 41b+1
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
4-4
F 04 12 00004 00001 PRO
F 16 72 TRUN SHFT PRO
F 16 78 R ROOT VERIFY TAPE METER WITH DSKY
+2 VERIFY INSERTION VELOCITY WITH RNDZ ROR WHERE RANGE = 2642 NM RANGE RATE = -4251 FPS
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
KEY V34E (TERMINATE) KEY V48E (LOAD DAP)
F 01 46 11002 PRO
F 06 47 LMWT CMWT PRO
KEY V56E (KILL AUTO TRACK ENABLE)
+3 KEY V41N72E (COARSE ALIGN RR) F 21 73 +000OOTRUN -077OOSHFT F 04 12 00006 00002 (CONTINUOUS DESIGNATE)
PRO 41 (COARSE ALIGN VERB)
KEY VI6N72E 16 72 MONITOR TRUNSHFT ANGLES
CB PGNS RNDZ RDR-OPEN CB AC BUS A RNDZ RDR-OPEN KEY V44E (TERMINATE RR DESIGNATE)
KEY V83E F 16 54 R ROOT THETA
SET ORDEAL PRO
CS HEATER AOT-CLOSE
CB AOT LAMP-CLOSE
+5 KEY V37E52E (IMU REALIGN)
4-5
410+1 CSI ROUTINE 373+02065 CS TIME 275+03028 TPI TIME
605400777 COTANGENT OF LOS TO-CSM 416+1 (ONE-HALF bRBITAL PERIOD) 411+0 RCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT 310R TIME TO CS
267R VELOCITY TO BE GAINED CSI
402R DELTA H
371R DELTA V CDH
372R _ DELTA T CSICDH
F 04 06 00001 00003 -(REFSMMAT) PRO -
F 50 25 00015 SELECT 1ST STAR ENTR
F 01 70 O02DE LOAD 1ST STAR PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FOAl ANGLES (AUTO MNVRI)
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVR)
F 01 71 002DE
KEY V76E PGNS MODE CONT-ATT HOLD
PRO +10 F 54 71 MARK 1ST STAR
PRO F 01 70 O02DE LOAD 2ND STAR
PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FDA ANGLES -(AUTO MNVRV
F 50 18 FDAI ANGLES (REQUEST PNVRt ENTR (BYPASS MNVR
F 01 71 002DE PGNS MODE CONT-ATT HOLD PRO
-35
4-6
+14 F 54 71 MARK 2ND STAR PRO
F 06 05 STAR ANGLE DIFFERENCE PRO
F 06 93 GYRO TORQUE ANGLES PRO
F 50 25 00014
PRO (CHECK ALIGNMENT IF TIME WILL PERMIT)
F 50 25 00015 SELECT 3RD STAR ENTR
F 01 70 OO2DE LOAD 3RD STAR PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FDAI ANGLES (AUTO MNVR)
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVR)
VERIFY ALIGNMENT VIA AOT
KEY V34E (TERMINATE) F 37 BB
V48E (LOAD DAP) F 01 46 11012
PRO F 06 47 LMWT CMWT
+17 PRO
CB AOT LAMP-OPEN
RESET ET (310R)
(12253) CB AC BUS A RNDZ RDR-CLOSE (WAIT 30 SEC) CB PGNS RNDZ RDR-CLOSE
RR MODE-LGC KEY V37E20E (ACQUIRE RADAR)
PGNS MODE CONT-AUTO F 50 18 FDA ANGLES (REQUEST MNVRJ
PRO (AUTO MNVR) 06 18 FDAI ANGLES (AUTO MNVR)
AGS MODE CONT-AUTO RATEERR MON-CMPTR (LMP)
F 50 18 FDAI ANGLES (REQUEST MNVR)
4-7
ENTR (BYPASS MNVR) NO TRK LT-OFF
F 50 72 RR TRUNSHFT VERIFY RR LOCK ON PRO
DSKY BLANKS
KEY V93E (BEFORE 1ST MARK REINIT W MATRIXI KEY V80E (UPDATE LM SV)
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (i20OOZOO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
400+3 AGS ALIGNshy400R (00000 COMPLETE) 507+0 Z-AXIS BORESIGHT 400+2 ACQUISITION STEERING
CS
(122amp55) KEY V37E32E (CSI)
F 06 11 1 S LOAD TIG CSI FROM DATA PAD (NOM 123S26- 271 PRO
F 06 55 +O000IN +02660E +13000 OMEGAT (CDH 180 DEG AFTER CSI PRO
F 06 37 LOAD TIG TPI FROM DATA PAD (NOM 1251021761 PRO
F 16 45 MKS TFI -00001
-30 COPY RDOT FOR 1ST CSI BU
31OR TIME TO CSI
267R VELOCITY TO BE GAINED CSI
402R DELTA H
371R DELTA V CDH
-22
4-8
372R _ DELTA T CSICDH
KEY V32E (MARKS=5
F 06 75 DELTA H DELTA T CSICDH DELTA T CDHTPI PRO
F 06 81 DELTA VOS-LV (CS) (NOM 501 DELTA VX)
CSI(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (CDH)
(NOM 60 DELTA VX) CDH(82)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
KEY V32E (MARKS=1C)
F 06 75 DELTA H DELTA TCSICDH DELTA TCDHTPI PRD
F 06 81 DELTA VS-LV (CSI) CSI(N811
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 82 DELTA VIS-LV(CDH)
CDH(82)
DELTA VX(LVI
DELTA VY(LV)
DELTA VZ(LV)
-12
4-9
-20 COPY RDOT FOR 2ND CSI BU
F 16 45
F 06 75
F 06 81
F 06 16
F 06 90
PRO MKS TFI -00001
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS NON SEL - PRPLNT A + B TEMP IND 40DEG TO lOODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + 8 PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4v 2 3 (120 - 190 DEG F
(LOS OF MSFN ) S-BAND - SLEW TO P = +90 Y a 0 S-BAND - FWD (OR AFT) S-BAND - DN VOICE BU BIOMED OFF
PRO (FINAL COMP)
267R - VELOCITY TO BE GAINED CSI
402R DELTA H
372R TIME CSICDHL
371R PREDICTED VEL TO BE GAINED CDH
263R OUT-OF-PLANE
DELTA H DELTA TCSICDH DELTA TCDHTPI PRO DELTA VS-LV (CSI)
KEY V9OE (OUT-OF-PLANED
0 LOAD TIG CSI FROM DATA PAD (NOM 12302627) PRO Y YDOT PSI
N90 CSM
YDOT
PRO
-7
4-10
F 06 81 DELTA VS-LV(CSI)
COPY YDOT FROM CSM AND LOAD NEGATIVE IN R2 CSIIN81I
DELTA VX(LV)
DELTA VYILV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (COH)
CDH(82)
DELTA VX(LV)
- DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RANGE AND RDOT FOR 3RD CS BU
COMPUTE CSI BU
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (i2000OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
(TRANSMIT CSI DATA TO CSMI VHF A XMTR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF TELEMETY PCM - LO
KEY VB3E F 16 54 R ROOT THETA
SET ORDEAL PRO
317R RANGE
440R RANGE RATE
4-11
400+3 AGS ALIGN t40OR (00000 COMPLETE)
277R THETA
PRO F 37 BB
-6 KEY 41E (RCS THRUSTING) F 50 18 FDAI-ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTAV 400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTAV 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA RF
TRANSMIT TGT DELTA VS TO CSM AND SYNC COUNTDOWN
16 85 DELTA VS-BODY
502R DELTA VZ (NOM 5Ql)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTAVS-BODY
(123t26t27) BURN +Z
NULL DELTA VS
4-12
VERIFY AGS RESIDUALS 50OR 501R 502R DELTA VX _ DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
CDH
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
KEY V67E (RESET W MATRIX) F 06 99 +0200E +O0020E +00005E
PRO
507+0 Z-AXIS BORESIGHT
(VHF RANGING WITH CSM) VHF A XMTR - VOICERNG VHF B XMTR - OFF VHF B RCVR - ON TELEMETRY PCM - HI
(12331) KEY V37E33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 a TIG CDH (NOM 1242425) -120 amp00 10 (AGS 0 TIME)
(CONVERT TO MINUTES)
411+0 THRUST ALONG Z-BODY AXIS ENTER IF YOU DONT TARGET CSI
373R (NOM 26443 310R TIME TO CDH
4-13
423R DESIRED ALT RATE AT CDH
402R DELTA Hshy
450R DELTA VX
452R DELTA VZ
623+0 Z-AXIS PARALLEL TO CSM PLANE
IPRO F 16 45 MKS TFI -00001
-52 RESET ET
KEY V93E (REINIT W MATRIX WHEN MARKS =4)
KEY V32E (MARKS = 3)
F 06 75 DELTA HCDH DELTA TCDHTPI DELTA TTPI PRO
F 06 81 DELTA VCDH-LV CDH(N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
-47 KEY VSOE (OUT-OF-PLANE)
_ TIG CDH (NOM 124t24t25) -3000 TIME FROM CDH
F 06 16 l1 LOAD TIG PLANE CHANGE (NOM 123amp54-253 PRO
F 06 90 Y YDOT PSI N90 CSM
VYDOT PRO
-42 KEY V32E (MARKS=1O)
F 06 75 DELTA HCDH DELTA TCDIHTPI DELTA TTPITPI PRO
F 06 81 DELTA VCDH-LV
4-14
CDH (NS1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -OO1
KEY V34E (TERMINATE) F 37 B8
PLANE CHANGE
KEY 30E (EXTERNAL DELTA V)
TIG CDH (NOM 124124t25) -3000 TIME FROM CDH
F 06 33 LOAD TIG PLANE CHANGE (NOM 123154T25) PRO
F 06 81 DELTA VS-LV (NOM 00)
-36 COPY RDOT FOR 1ST CDH BU
KEY V90E (OUT-OF-PLANE)
F 06 16 1 1 LOAD TIG PLANE CHANGE (NOM 1231543251 PRO
F 06 90 Y YOOT PSI N90 CSM
YDOT
PRO
F 06 81 DELTA VS-LV(NOM 00)
COPY YDOT AND LOAD NEGATIVE IN R2 PRO
F 06 42 HA HP DELTA V PRO
F 16 45 MKS TFI MGA
PRO
F 37 BB
KEY 41E (RCS THRUSTING)
-30
4-15
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVRI
410+5 EXTERNAL DELTA V 450+0 451-YDOT 452+0 (LOAD CSM -YDOT)
407+0 ROTATE EXTERNAL DELTA V RF
16 95 DELTA VS-BODY
-3035 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATTVHOLD 407+1 FREEZE EXTERNAL DELTAV
F 16 85 DELTA VS-BODY -
NULL DELTA VIS
PRO F 37BB
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
507+0 Z-AXIS BORESIGHT
(12356) KEY 33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 TIG CDH (NOM 124t24t25) -120 OO ZOO (AGS 0 TIME)
(CONVERT TO MINUTES)
373R _ (NOM 2644) 310R TIME TO CDH
423R DESIRED ALT RATE AT CDH
(ADS OF MSFN) S-BAND - SLEW TOP = ACQUIRE HGA LOCK ON VOICE - BUVOICE -- VOICE VERIFY VOICE TLM BIOMED - LEFT (OR RIGHT)
402R DELTAH
4-16
F 16 45
-25
-23
F 06 75
F 06 81
F 16 45
-12
F 06 75
F 06 81
450R DELTA VX
452R DELTA VZ
PRO MKS TFI -00001
KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
COPY ROOT FOR 2ND CDH BU
KEY v32E (MARKS = 5)
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40DEG TO 1OODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + B PRESS IND PSIA
A QUANTITY IND _ PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING a TEMP MON SEL RCS QUAD 1 4 2 3 (120 - 190 DEG F)i
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
CDH(NB1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO MKS TFI -00001
PRO (FINAL COMP)
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
KEY V9OE (OUT-OF-PLANE)
-7
4-17
F 06 16 jj LOAD TIG CDH FROM DATA PAD (NOM 12424251 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT PRO
COPY YOOT FROM CSM AND LOAD NEGATIVE IN R2
CDH(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RDOT FOR 3RD CDH BU
COMPUTE CDH BU
TRANSMIT TGT DELTA VOS TO CSM AND SYNC COUNTDOWN
KEY V47E (INITIALIZE AGS F 06 16 GET OF AGS 0 TIME 120O00OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
KEY V83E F 16 54 R RDOT THETA
SET ORDEAL PRO
317R _ RANGE
440R RANGE RATE 400+3 AGS ALIGN 40OR (00000 COMPLETE)
277R THETA
-6
4-18
PRO F 3 BB
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY V06N86E F 06 86 DELTA VIS-LV
AGS(N86) CHART
DELTA VX(LVD
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
16 85 DELTA VS-BODY
50OR DELTA VX (NOM -0O3)
502R DELTA VZ (NOM 60)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD 407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS BODY
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS 5OOR 50IR 502R DELTA VX -DELTA VY DELTA VZ-
VERIFY PGNS RESIDUALS N85
DELTA VX(LM)
4-19
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
TPI
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO 507+0 Z-AXIS BORESIGHT
(12426) KEY 34E (TPI)
-36 RESET ET
F 06 37 - amp LOAD TIG TPI FROM DATA PAD (NOM 1250246) PRO
F 06 55 +00000 +02660E +13000 OMEGAT PRO
F 16 45 MARKS TFI -00001
-32 KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
-29 KEY V32E (MARKS = 3)
F 06 37 __ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
RESET ET
410+3 TPI SEARCH ROUTINE 307+04300 DELTA T TRANSFER
4-20
-26 310+02600 TFI TPI
303R THETA AT TPI
267R DELTA VTPI
371R DELTA VTPI + DELTA VTPF
KEY V32E (MARKS = 10)
F 06 37 _ _ _ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VIS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
TEMPIPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40ODEG TO IGODEG F A + B PRESS IND 181 +-3 PSIA
TEMPIPRESS MON SEL - HEL
A + B PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD I 4 2 3 (120 - 190 DEG F)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
RESET ET
-13 310+01300 TFI TPI
303R THETA AT TPI
-12 PRO (FINAL COMP) F 06 37 Z TIG TPIj__
4-21
TRANSMIT TIG OF TPI TO CSM-
PRO F 06 58 HP DELTA VTPI DELTA VTRF
PRO F 06 81 DELTA VS-LV
KEY V9OE (OUT-OF-PLANE)
F 06 16 1 LOAD TIG TPI FROM DATA PAD (NOM 12502461 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT
PRO F 06 81 DELTA VS-LV
COPY CSM YDOT AND LOAD NEGATIVE IN R2 N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 59 DELTA VS LOS
N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI MGA
RESET ET
PRO F 37 BB
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (12000t600)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE)
-10
-6
4-22
F 50 16 DOWNLINK COMPLETE PRO (UPDATE COMPLETE)
400+3 AGS ALIGN 400R (00000 COMPLETE)
-9 277R COPY TGT LOS ANGLE
310+00800
303R THETA AT TPI 410+4 DIRECT TRANSFER AT ET=-8 404+0 405+0 406+0 (MONITOR 470 471 4721
373R TIG TPI
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
KEY 41E (RCS THRUSTING) F 50 18 FOAl ANGLES (REQUEST MNVRI
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
-5 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUS
400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
COMPUTE TPI BU
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
4-23
1685 DELTA VS-BODY
50OR DELTA VX(NOM -115)
502R DELTA VZ(NOM 229)
-Z35 OSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS-BODY
(1250246) BURN +Z
VERIFY AGS RESIDUALS 500R 501R 502R DELTAVX DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
MCC1
KEY V76E (PGNS PULSE) PGNSMODECONT-AUTO
KEY V93E (BEFORE 1ST MARK REINITW MATRIX)
+2 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
4-24
(LOS OF MSFN) S-BAND - SLEW TO P = 90 Y = 0 S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
404+0 405+0 406+0
(MONITOR 470 471 4721
+9 277R COPY TGT LOS ANGLE
+12 PRO (COMPUTE MCC FOR TPI+15I F 06 81 DELTA VS-LV
PRO F 06 59 DELTA VS-LOS
PRO F 16 45 MKS TFI MGA
+13 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUOS
COMPUTE MCC1 BU
PRO F 37 BB
+14 KEY 41E (RCS THRUSTING) F 50 18 FOAL ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+1425 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+15 F 16 85 NULL DELTA VS
PRO F 37 BB
MCC2
KEY V76E (PGNS PULSE)
4-25
PGNS MODE CONT-AUTO
KEY V93E (BEFORE 1ST MARK REINIT W MATRIX)
+16 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
404+0 405+0 406+0 (MONITOR 470 471 47)shy
+24 277R COPY TGT LOS ANGLE
+27 PRO (COMPUTE MCC FORTPI+30) F 06 81 DELTA VS-LV
PRO F 06 59 DELIA VPS-LOS
PRO F 16 45 MKS TFI MGA
+28 277R COPY TGT LOS ANGLE
COPY R RDOT FROM TAPEMETER FOR BUS
COMPUTE MCC2 BU
F 37 BB PRO
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+2925 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+30 F 16 85 NULL DELTA VS
PRO F 37 BB
KEY OOE (P001
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
4-26
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT KEY V34E (TERMINATE)
KEY V37E47E (AVE G) F 16 83 DELTA VIS
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT VERIFY TAPE METER WITH DSKY
BRAKING GATE 30 FPS - 6000 FT 20 FPS - 3000 FT 10 FPS - 1500 FT 5 FPS - 600 FT
RENDEZVOUS
STATION KEEPING
5-1
50 ABORT PROCEDURE
This is a specific AGS nominal abort procedure due to a PGNS failure between insertion and station keeping
51
5-2
Nominal AGS Procedures
ASSUMPTIONS
AFTER INSERTION
I INSERTION COMPLETE (RFSIDUALS NULLED) g PGNS FAILURE BEFORE INSERTION 3 RAUAR NOT LOCKED ON
(UI CoNT-AGS ATlI[uUE MON-AGS(CDR) RATE ERR MON-CNPTR(LMP) ATTITUDE MON-AGS(LMP) SHFITRUN-+5 DEG X-POINTER-HI MULT RADAR IEST Sw-OFF LNb GMbL-OFF ENG ARM-OFF X-IRANSL-2 JETS DEAD BAND-MAX PGNS MODE CONT-OFF THROTJET-JET CB IMU OIR-ON HH MOVE-AUTO rRACK TTCATNANSL-ENABLE(CDR)
AL CPL-ON MODE SL-AGS RNGAL1 MON-RNbRNGRT RAIE ERR MON-RNDZ HDR(CDR) AVl CoNT(3)-PULSE AGS MODE CONT-AUTO ACA4JET-DISABLE(CDR) TTCATRANSL-DISABLE(LMP) ACA4JET-DISABLE(LMP)
bO7+U Z-AXIS BOPESIGHT 400+2 Z-AXIS STEERING PULSE TO NULL AGS ERRORS POINT Z-AXIS IN DIRECTION OF CSM MODE CONT-ATT HOLD ATT CONT(3)-MODE CONTROL O unnr - ZirF
5-3
SLEW PATE - LO
SLEW RR ANT TO OqON FUAI VERIFY MAX SIGNAL STRENGTH RH MOOE-AUTO TRACK NO TRACK LIGHT OFF -
ATT CONT(3h-PULSE
CHECK INSERTION VELOCITY WITH TAPEMETER COMPARE EAPEMETER WITH AGS STATE VECTOR DATA I
17R RANGE(NOM 2642)
440R RANGE RATE(NOM -425l)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
cSI
+3 417+1 (RADAR FILTER INITIALIZED) 41b+l (NO BOHESIGHT) b03-XXXXX RANGE RATE
+5 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGF
41b+1 CSI ROUTINE 373+o2065 CSi TIME 275+03028 TPI TIME 605+0077 COTANGENT OF LOS TO CSM 41b+1 (ONE-HALF OFBITAL-PERIOD) 411+0 HCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT
610R TIME TO CST
43 RESET ET
267R VELOCITY TO BE GAINED CSI
402R FLTA H
371R DFLTA V CDH
5-4
372R DFLTA T CSICDH
-42 415+1 (No BORESIGHT) bO6-xXXXX RANGE RATE
-40 415+1 (NO BORESIGHT)503-XXXXX RANGE RATE dORESIGHT ON CSM
415+1 316+XXXXX RANGE
-37 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE
-15 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE UORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-2 415+1 (No BOHESIGHT) bO3-XXXXX RANGF RATE
i1uR TIME TO CS
RESEF ET
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-30 COPY ROOT FOR 1ST CSI 81J
BORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-t7 415+1 (NO BORFSIGHT) 50-XXxXx RANGF RATE
267R VELOCITY TO HE GAINED CSI
402R LELTA H
371R OFLTA V COH
372R OELTA T CSICDH
-5 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 blb+XXXXX RANGE
-i2 415+1 (No BORESIGHT) 5n3-XXXXX RANGE RATE
415+1 (NO BORESIGHT)
5-5
503-XXXXX RANGF RATE
COPY Roor FOR 2NO CSI BU
bORESIGHT ON CSM 415+1 316+XXXXX RANGE
TEMPPRESS MON SEL - FUEL MAN
A AND 8 PRESS 181 +-3 PIG TEMPPRESS MON SEL - PRPLNT
A AND B TEMP IND 4ODEG 0 IOODEG F A AND B PRFSS IND 181 +-3 PSIA
tEMPPRESS MON SEL - HEL
A AND 8 PRESS IND PSIA
A QUANTITY IND- -- PERCENT RFMAINING
8 QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4p 2 3 (120 - 190 DFG F)
415+1 (NO BORESIGHT)-17 503-XXXXX RANGE RATE
-15 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
(LOS OF MSFN) S-BAND - SLEW 10 P = +90t Y U S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
-12 415+1 (No 8ORESIGHT)
503-XXXXX RANGE RATE
267R VFLOCITY TU BE GAINED CSI
402R OFLTA H
372R TIME CSICH
371R PREDICTED VEL 10 RE GAINED COH
263R OLT-OF-PLANE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATL
-10 COPY RANGE AND ROOT FOR 3RD CSI 8U
SORESIGH ON CSM 41b+1
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
4-5
410+1 CSI ROUTINE 373+02065 CS TIME 275+03028 TPI TIME
605400777 COTANGENT OF LOS TO-CSM 416+1 (ONE-HALF bRBITAL PERIOD) 411+0 RCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT 310R TIME TO CS
267R VELOCITY TO BE GAINED CSI
402R DELTA H
371R DELTA V CDH
372R _ DELTA T CSICDH
F 04 06 00001 00003 -(REFSMMAT) PRO -
F 50 25 00015 SELECT 1ST STAR ENTR
F 01 70 O02DE LOAD 1ST STAR PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FOAl ANGLES (AUTO MNVRI)
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVR)
F 01 71 002DE
KEY V76E PGNS MODE CONT-ATT HOLD
PRO +10 F 54 71 MARK 1ST STAR
PRO F 01 70 O02DE LOAD 2ND STAR
PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FDA ANGLES -(AUTO MNVRV
F 50 18 FDAI ANGLES (REQUEST PNVRt ENTR (BYPASS MNVR
F 01 71 002DE PGNS MODE CONT-ATT HOLD PRO
-35
4-6
+14 F 54 71 MARK 2ND STAR PRO
F 06 05 STAR ANGLE DIFFERENCE PRO
F 06 93 GYRO TORQUE ANGLES PRO
F 50 25 00014
PRO (CHECK ALIGNMENT IF TIME WILL PERMIT)
F 50 25 00015 SELECT 3RD STAR ENTR
F 01 70 OO2DE LOAD 3RD STAR PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FDAI ANGLES (AUTO MNVR)
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVR)
VERIFY ALIGNMENT VIA AOT
KEY V34E (TERMINATE) F 37 BB
V48E (LOAD DAP) F 01 46 11012
PRO F 06 47 LMWT CMWT
+17 PRO
CB AOT LAMP-OPEN
RESET ET (310R)
(12253) CB AC BUS A RNDZ RDR-CLOSE (WAIT 30 SEC) CB PGNS RNDZ RDR-CLOSE
RR MODE-LGC KEY V37E20E (ACQUIRE RADAR)
PGNS MODE CONT-AUTO F 50 18 FDA ANGLES (REQUEST MNVRJ
PRO (AUTO MNVR) 06 18 FDAI ANGLES (AUTO MNVR)
AGS MODE CONT-AUTO RATEERR MON-CMPTR (LMP)
F 50 18 FDAI ANGLES (REQUEST MNVR)
4-7
ENTR (BYPASS MNVR) NO TRK LT-OFF
F 50 72 RR TRUNSHFT VERIFY RR LOCK ON PRO
DSKY BLANKS
KEY V93E (BEFORE 1ST MARK REINIT W MATRIXI KEY V80E (UPDATE LM SV)
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (i20OOZOO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
400+3 AGS ALIGNshy400R (00000 COMPLETE) 507+0 Z-AXIS BORESIGHT 400+2 ACQUISITION STEERING
CS
(122amp55) KEY V37E32E (CSI)
F 06 11 1 S LOAD TIG CSI FROM DATA PAD (NOM 123S26- 271 PRO
F 06 55 +O000IN +02660E +13000 OMEGAT (CDH 180 DEG AFTER CSI PRO
F 06 37 LOAD TIG TPI FROM DATA PAD (NOM 1251021761 PRO
F 16 45 MKS TFI -00001
-30 COPY RDOT FOR 1ST CSI BU
31OR TIME TO CSI
267R VELOCITY TO BE GAINED CSI
402R DELTA H
371R DELTA V CDH
-22
4-8
372R _ DELTA T CSICDH
KEY V32E (MARKS=5
F 06 75 DELTA H DELTA T CSICDH DELTA T CDHTPI PRO
F 06 81 DELTA VOS-LV (CS) (NOM 501 DELTA VX)
CSI(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (CDH)
(NOM 60 DELTA VX) CDH(82)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
KEY V32E (MARKS=1C)
F 06 75 DELTA H DELTA TCSICDH DELTA TCDHTPI PRD
F 06 81 DELTA VS-LV (CSI) CSI(N811
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 82 DELTA VIS-LV(CDH)
CDH(82)
DELTA VX(LVI
DELTA VY(LV)
DELTA VZ(LV)
-12
4-9
-20 COPY RDOT FOR 2ND CSI BU
F 16 45
F 06 75
F 06 81
F 06 16
F 06 90
PRO MKS TFI -00001
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS NON SEL - PRPLNT A + B TEMP IND 40DEG TO lOODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + 8 PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4v 2 3 (120 - 190 DEG F
(LOS OF MSFN ) S-BAND - SLEW TO P = +90 Y a 0 S-BAND - FWD (OR AFT) S-BAND - DN VOICE BU BIOMED OFF
PRO (FINAL COMP)
267R - VELOCITY TO BE GAINED CSI
402R DELTA H
372R TIME CSICDHL
371R PREDICTED VEL TO BE GAINED CDH
263R OUT-OF-PLANE
DELTA H DELTA TCSICDH DELTA TCDHTPI PRO DELTA VS-LV (CSI)
KEY V9OE (OUT-OF-PLANED
0 LOAD TIG CSI FROM DATA PAD (NOM 12302627) PRO Y YDOT PSI
N90 CSM
YDOT
PRO
-7
4-10
F 06 81 DELTA VS-LV(CSI)
COPY YDOT FROM CSM AND LOAD NEGATIVE IN R2 CSIIN81I
DELTA VX(LV)
DELTA VYILV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (COH)
CDH(82)
DELTA VX(LV)
- DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RANGE AND RDOT FOR 3RD CS BU
COMPUTE CSI BU
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (i2000OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
(TRANSMIT CSI DATA TO CSMI VHF A XMTR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF TELEMETY PCM - LO
KEY VB3E F 16 54 R ROOT THETA
SET ORDEAL PRO
317R RANGE
440R RANGE RATE
4-11
400+3 AGS ALIGN t40OR (00000 COMPLETE)
277R THETA
PRO F 37 BB
-6 KEY 41E (RCS THRUSTING) F 50 18 FDAI-ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTAV 400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTAV 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA RF
TRANSMIT TGT DELTA VS TO CSM AND SYNC COUNTDOWN
16 85 DELTA VS-BODY
502R DELTA VZ (NOM 5Ql)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTAVS-BODY
(123t26t27) BURN +Z
NULL DELTA VS
4-12
VERIFY AGS RESIDUALS 50OR 501R 502R DELTA VX _ DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
CDH
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
KEY V67E (RESET W MATRIX) F 06 99 +0200E +O0020E +00005E
PRO
507+0 Z-AXIS BORESIGHT
(VHF RANGING WITH CSM) VHF A XMTR - VOICERNG VHF B XMTR - OFF VHF B RCVR - ON TELEMETRY PCM - HI
(12331) KEY V37E33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 a TIG CDH (NOM 1242425) -120 amp00 10 (AGS 0 TIME)
(CONVERT TO MINUTES)
411+0 THRUST ALONG Z-BODY AXIS ENTER IF YOU DONT TARGET CSI
373R (NOM 26443 310R TIME TO CDH
4-13
423R DESIRED ALT RATE AT CDH
402R DELTA Hshy
450R DELTA VX
452R DELTA VZ
623+0 Z-AXIS PARALLEL TO CSM PLANE
IPRO F 16 45 MKS TFI -00001
-52 RESET ET
KEY V93E (REINIT W MATRIX WHEN MARKS =4)
KEY V32E (MARKS = 3)
F 06 75 DELTA HCDH DELTA TCDHTPI DELTA TTPI PRO
F 06 81 DELTA VCDH-LV CDH(N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
-47 KEY VSOE (OUT-OF-PLANE)
_ TIG CDH (NOM 124t24t25) -3000 TIME FROM CDH
F 06 16 l1 LOAD TIG PLANE CHANGE (NOM 123amp54-253 PRO
F 06 90 Y YDOT PSI N90 CSM
VYDOT PRO
-42 KEY V32E (MARKS=1O)
F 06 75 DELTA HCDH DELTA TCDIHTPI DELTA TTPITPI PRO
F 06 81 DELTA VCDH-LV
4-14
CDH (NS1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -OO1
KEY V34E (TERMINATE) F 37 B8
PLANE CHANGE
KEY 30E (EXTERNAL DELTA V)
TIG CDH (NOM 124124t25) -3000 TIME FROM CDH
F 06 33 LOAD TIG PLANE CHANGE (NOM 123154T25) PRO
F 06 81 DELTA VS-LV (NOM 00)
-36 COPY RDOT FOR 1ST CDH BU
KEY V90E (OUT-OF-PLANE)
F 06 16 1 1 LOAD TIG PLANE CHANGE (NOM 1231543251 PRO
F 06 90 Y YOOT PSI N90 CSM
YDOT
PRO
F 06 81 DELTA VS-LV(NOM 00)
COPY YDOT AND LOAD NEGATIVE IN R2 PRO
F 06 42 HA HP DELTA V PRO
F 16 45 MKS TFI MGA
PRO
F 37 BB
KEY 41E (RCS THRUSTING)
-30
4-15
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVRI
410+5 EXTERNAL DELTA V 450+0 451-YDOT 452+0 (LOAD CSM -YDOT)
407+0 ROTATE EXTERNAL DELTA V RF
16 95 DELTA VS-BODY
-3035 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATTVHOLD 407+1 FREEZE EXTERNAL DELTAV
F 16 85 DELTA VS-BODY -
NULL DELTA VIS
PRO F 37BB
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
507+0 Z-AXIS BORESIGHT
(12356) KEY 33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 TIG CDH (NOM 124t24t25) -120 OO ZOO (AGS 0 TIME)
(CONVERT TO MINUTES)
373R _ (NOM 2644) 310R TIME TO CDH
423R DESIRED ALT RATE AT CDH
(ADS OF MSFN) S-BAND - SLEW TOP = ACQUIRE HGA LOCK ON VOICE - BUVOICE -- VOICE VERIFY VOICE TLM BIOMED - LEFT (OR RIGHT)
402R DELTAH
4-16
F 16 45
-25
-23
F 06 75
F 06 81
F 16 45
-12
F 06 75
F 06 81
450R DELTA VX
452R DELTA VZ
PRO MKS TFI -00001
KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
COPY ROOT FOR 2ND CDH BU
KEY v32E (MARKS = 5)
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40DEG TO 1OODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + B PRESS IND PSIA
A QUANTITY IND _ PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING a TEMP MON SEL RCS QUAD 1 4 2 3 (120 - 190 DEG F)i
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
CDH(NB1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO MKS TFI -00001
PRO (FINAL COMP)
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
KEY V9OE (OUT-OF-PLANE)
-7
4-17
F 06 16 jj LOAD TIG CDH FROM DATA PAD (NOM 12424251 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT PRO
COPY YOOT FROM CSM AND LOAD NEGATIVE IN R2
CDH(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RDOT FOR 3RD CDH BU
COMPUTE CDH BU
TRANSMIT TGT DELTA VOS TO CSM AND SYNC COUNTDOWN
KEY V47E (INITIALIZE AGS F 06 16 GET OF AGS 0 TIME 120O00OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
KEY V83E F 16 54 R RDOT THETA
SET ORDEAL PRO
317R _ RANGE
440R RANGE RATE 400+3 AGS ALIGN 40OR (00000 COMPLETE)
277R THETA
-6
4-18
PRO F 3 BB
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY V06N86E F 06 86 DELTA VIS-LV
AGS(N86) CHART
DELTA VX(LVD
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
16 85 DELTA VS-BODY
50OR DELTA VX (NOM -0O3)
502R DELTA VZ (NOM 60)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD 407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS BODY
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS 5OOR 50IR 502R DELTA VX -DELTA VY DELTA VZ-
VERIFY PGNS RESIDUALS N85
DELTA VX(LM)
4-19
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
TPI
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO 507+0 Z-AXIS BORESIGHT
(12426) KEY 34E (TPI)
-36 RESET ET
F 06 37 - amp LOAD TIG TPI FROM DATA PAD (NOM 1250246) PRO
F 06 55 +00000 +02660E +13000 OMEGAT PRO
F 16 45 MARKS TFI -00001
-32 KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
-29 KEY V32E (MARKS = 3)
F 06 37 __ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
RESET ET
410+3 TPI SEARCH ROUTINE 307+04300 DELTA T TRANSFER
4-20
-26 310+02600 TFI TPI
303R THETA AT TPI
267R DELTA VTPI
371R DELTA VTPI + DELTA VTPF
KEY V32E (MARKS = 10)
F 06 37 _ _ _ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VIS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
TEMPIPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40ODEG TO IGODEG F A + B PRESS IND 181 +-3 PSIA
TEMPIPRESS MON SEL - HEL
A + B PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD I 4 2 3 (120 - 190 DEG F)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
RESET ET
-13 310+01300 TFI TPI
303R THETA AT TPI
-12 PRO (FINAL COMP) F 06 37 Z TIG TPIj__
4-21
TRANSMIT TIG OF TPI TO CSM-
PRO F 06 58 HP DELTA VTPI DELTA VTRF
PRO F 06 81 DELTA VS-LV
KEY V9OE (OUT-OF-PLANE)
F 06 16 1 LOAD TIG TPI FROM DATA PAD (NOM 12502461 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT
PRO F 06 81 DELTA VS-LV
COPY CSM YDOT AND LOAD NEGATIVE IN R2 N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 59 DELTA VS LOS
N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI MGA
RESET ET
PRO F 37 BB
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (12000t600)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE)
-10
-6
4-22
F 50 16 DOWNLINK COMPLETE PRO (UPDATE COMPLETE)
400+3 AGS ALIGN 400R (00000 COMPLETE)
-9 277R COPY TGT LOS ANGLE
310+00800
303R THETA AT TPI 410+4 DIRECT TRANSFER AT ET=-8 404+0 405+0 406+0 (MONITOR 470 471 4721
373R TIG TPI
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
KEY 41E (RCS THRUSTING) F 50 18 FOAl ANGLES (REQUEST MNVRI
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
-5 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUS
400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
COMPUTE TPI BU
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
4-23
1685 DELTA VS-BODY
50OR DELTA VX(NOM -115)
502R DELTA VZ(NOM 229)
-Z35 OSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS-BODY
(1250246) BURN +Z
VERIFY AGS RESIDUALS 500R 501R 502R DELTAVX DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
MCC1
KEY V76E (PGNS PULSE) PGNSMODECONT-AUTO
KEY V93E (BEFORE 1ST MARK REINITW MATRIX)
+2 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
4-24
(LOS OF MSFN) S-BAND - SLEW TO P = 90 Y = 0 S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
404+0 405+0 406+0
(MONITOR 470 471 4721
+9 277R COPY TGT LOS ANGLE
+12 PRO (COMPUTE MCC FOR TPI+15I F 06 81 DELTA VS-LV
PRO F 06 59 DELTA VS-LOS
PRO F 16 45 MKS TFI MGA
+13 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUOS
COMPUTE MCC1 BU
PRO F 37 BB
+14 KEY 41E (RCS THRUSTING) F 50 18 FOAL ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+1425 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+15 F 16 85 NULL DELTA VS
PRO F 37 BB
MCC2
KEY V76E (PGNS PULSE)
4-25
PGNS MODE CONT-AUTO
KEY V93E (BEFORE 1ST MARK REINIT W MATRIX)
+16 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
404+0 405+0 406+0 (MONITOR 470 471 47)shy
+24 277R COPY TGT LOS ANGLE
+27 PRO (COMPUTE MCC FORTPI+30) F 06 81 DELTA VS-LV
PRO F 06 59 DELIA VPS-LOS
PRO F 16 45 MKS TFI MGA
+28 277R COPY TGT LOS ANGLE
COPY R RDOT FROM TAPEMETER FOR BUS
COMPUTE MCC2 BU
F 37 BB PRO
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+2925 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+30 F 16 85 NULL DELTA VS
PRO F 37 BB
KEY OOE (P001
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
4-26
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT KEY V34E (TERMINATE)
KEY V37E47E (AVE G) F 16 83 DELTA VIS
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT VERIFY TAPE METER WITH DSKY
BRAKING GATE 30 FPS - 6000 FT 20 FPS - 3000 FT 10 FPS - 1500 FT 5 FPS - 600 FT
RENDEZVOUS
STATION KEEPING
5-1
50 ABORT PROCEDURE
This is a specific AGS nominal abort procedure due to a PGNS failure between insertion and station keeping
51
5-2
Nominal AGS Procedures
ASSUMPTIONS
AFTER INSERTION
I INSERTION COMPLETE (RFSIDUALS NULLED) g PGNS FAILURE BEFORE INSERTION 3 RAUAR NOT LOCKED ON
(UI CoNT-AGS ATlI[uUE MON-AGS(CDR) RATE ERR MON-CNPTR(LMP) ATTITUDE MON-AGS(LMP) SHFITRUN-+5 DEG X-POINTER-HI MULT RADAR IEST Sw-OFF LNb GMbL-OFF ENG ARM-OFF X-IRANSL-2 JETS DEAD BAND-MAX PGNS MODE CONT-OFF THROTJET-JET CB IMU OIR-ON HH MOVE-AUTO rRACK TTCATNANSL-ENABLE(CDR)
AL CPL-ON MODE SL-AGS RNGAL1 MON-RNbRNGRT RAIE ERR MON-RNDZ HDR(CDR) AVl CoNT(3)-PULSE AGS MODE CONT-AUTO ACA4JET-DISABLE(CDR) TTCATRANSL-DISABLE(LMP) ACA4JET-DISABLE(LMP)
bO7+U Z-AXIS BOPESIGHT 400+2 Z-AXIS STEERING PULSE TO NULL AGS ERRORS POINT Z-AXIS IN DIRECTION OF CSM MODE CONT-ATT HOLD ATT CONT(3)-MODE CONTROL O unnr - ZirF
5-3
SLEW PATE - LO
SLEW RR ANT TO OqON FUAI VERIFY MAX SIGNAL STRENGTH RH MOOE-AUTO TRACK NO TRACK LIGHT OFF -
ATT CONT(3h-PULSE
CHECK INSERTION VELOCITY WITH TAPEMETER COMPARE EAPEMETER WITH AGS STATE VECTOR DATA I
17R RANGE(NOM 2642)
440R RANGE RATE(NOM -425l)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
cSI
+3 417+1 (RADAR FILTER INITIALIZED) 41b+l (NO BOHESIGHT) b03-XXXXX RANGE RATE
+5 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGF
41b+1 CSI ROUTINE 373+o2065 CSi TIME 275+03028 TPI TIME 605+0077 COTANGENT OF LOS TO CSM 41b+1 (ONE-HALF OFBITAL-PERIOD) 411+0 HCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT
610R TIME TO CST
43 RESET ET
267R VELOCITY TO BE GAINED CSI
402R FLTA H
371R DFLTA V CDH
5-4
372R DFLTA T CSICDH
-42 415+1 (No BORESIGHT) bO6-xXXXX RANGE RATE
-40 415+1 (NO BORESIGHT)503-XXXXX RANGE RATE dORESIGHT ON CSM
415+1 316+XXXXX RANGE
-37 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE
-15 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE UORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-2 415+1 (No BOHESIGHT) bO3-XXXXX RANGF RATE
i1uR TIME TO CS
RESEF ET
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-30 COPY ROOT FOR 1ST CSI 81J
BORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-t7 415+1 (NO BORFSIGHT) 50-XXxXx RANGF RATE
267R VELOCITY TO HE GAINED CSI
402R LELTA H
371R OFLTA V COH
372R OELTA T CSICDH
-5 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 blb+XXXXX RANGE
-i2 415+1 (No BORESIGHT) 5n3-XXXXX RANGE RATE
415+1 (NO BORESIGHT)
5-5
503-XXXXX RANGF RATE
COPY Roor FOR 2NO CSI BU
bORESIGHT ON CSM 415+1 316+XXXXX RANGE
TEMPPRESS MON SEL - FUEL MAN
A AND 8 PRESS 181 +-3 PIG TEMPPRESS MON SEL - PRPLNT
A AND B TEMP IND 4ODEG 0 IOODEG F A AND B PRFSS IND 181 +-3 PSIA
tEMPPRESS MON SEL - HEL
A AND 8 PRESS IND PSIA
A QUANTITY IND- -- PERCENT RFMAINING
8 QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4p 2 3 (120 - 190 DFG F)
415+1 (NO BORESIGHT)-17 503-XXXXX RANGE RATE
-15 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
(LOS OF MSFN) S-BAND - SLEW 10 P = +90t Y U S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
-12 415+1 (No 8ORESIGHT)
503-XXXXX RANGE RATE
267R VFLOCITY TU BE GAINED CSI
402R OFLTA H
372R TIME CSICH
371R PREDICTED VEL 10 RE GAINED COH
263R OLT-OF-PLANE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATL
-10 COPY RANGE AND ROOT FOR 3RD CSI 8U
SORESIGH ON CSM 41b+1
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
-35
4-6
+14 F 54 71 MARK 2ND STAR PRO
F 06 05 STAR ANGLE DIFFERENCE PRO
F 06 93 GYRO TORQUE ANGLES PRO
F 50 25 00014
PRO (CHECK ALIGNMENT IF TIME WILL PERMIT)
F 50 25 00015 SELECT 3RD STAR ENTR
F 01 70 OO2DE LOAD 3RD STAR PRO
PGNS MODE CONT-AUTO F 50 18 FDAI ANGLES (REQUEST MNVR)
PRO (AUTO MNVR) 06 18 FDAI ANGLES (AUTO MNVR)
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVR)
VERIFY ALIGNMENT VIA AOT
KEY V34E (TERMINATE) F 37 BB
V48E (LOAD DAP) F 01 46 11012
PRO F 06 47 LMWT CMWT
+17 PRO
CB AOT LAMP-OPEN
RESET ET (310R)
(12253) CB AC BUS A RNDZ RDR-CLOSE (WAIT 30 SEC) CB PGNS RNDZ RDR-CLOSE
RR MODE-LGC KEY V37E20E (ACQUIRE RADAR)
PGNS MODE CONT-AUTO F 50 18 FDA ANGLES (REQUEST MNVRJ
PRO (AUTO MNVR) 06 18 FDAI ANGLES (AUTO MNVR)
AGS MODE CONT-AUTO RATEERR MON-CMPTR (LMP)
F 50 18 FDAI ANGLES (REQUEST MNVR)
4-7
ENTR (BYPASS MNVR) NO TRK LT-OFF
F 50 72 RR TRUNSHFT VERIFY RR LOCK ON PRO
DSKY BLANKS
KEY V93E (BEFORE 1ST MARK REINIT W MATRIXI KEY V80E (UPDATE LM SV)
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (i20OOZOO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
400+3 AGS ALIGNshy400R (00000 COMPLETE) 507+0 Z-AXIS BORESIGHT 400+2 ACQUISITION STEERING
CS
(122amp55) KEY V37E32E (CSI)
F 06 11 1 S LOAD TIG CSI FROM DATA PAD (NOM 123S26- 271 PRO
F 06 55 +O000IN +02660E +13000 OMEGAT (CDH 180 DEG AFTER CSI PRO
F 06 37 LOAD TIG TPI FROM DATA PAD (NOM 1251021761 PRO
F 16 45 MKS TFI -00001
-30 COPY RDOT FOR 1ST CSI BU
31OR TIME TO CSI
267R VELOCITY TO BE GAINED CSI
402R DELTA H
371R DELTA V CDH
-22
4-8
372R _ DELTA T CSICDH
KEY V32E (MARKS=5
F 06 75 DELTA H DELTA T CSICDH DELTA T CDHTPI PRO
F 06 81 DELTA VOS-LV (CS) (NOM 501 DELTA VX)
CSI(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (CDH)
(NOM 60 DELTA VX) CDH(82)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
KEY V32E (MARKS=1C)
F 06 75 DELTA H DELTA TCSICDH DELTA TCDHTPI PRD
F 06 81 DELTA VS-LV (CSI) CSI(N811
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 82 DELTA VIS-LV(CDH)
CDH(82)
DELTA VX(LVI
DELTA VY(LV)
DELTA VZ(LV)
-12
4-9
-20 COPY RDOT FOR 2ND CSI BU
F 16 45
F 06 75
F 06 81
F 06 16
F 06 90
PRO MKS TFI -00001
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS NON SEL - PRPLNT A + B TEMP IND 40DEG TO lOODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + 8 PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4v 2 3 (120 - 190 DEG F
(LOS OF MSFN ) S-BAND - SLEW TO P = +90 Y a 0 S-BAND - FWD (OR AFT) S-BAND - DN VOICE BU BIOMED OFF
PRO (FINAL COMP)
267R - VELOCITY TO BE GAINED CSI
402R DELTA H
372R TIME CSICDHL
371R PREDICTED VEL TO BE GAINED CDH
263R OUT-OF-PLANE
DELTA H DELTA TCSICDH DELTA TCDHTPI PRO DELTA VS-LV (CSI)
KEY V9OE (OUT-OF-PLANED
0 LOAD TIG CSI FROM DATA PAD (NOM 12302627) PRO Y YDOT PSI
N90 CSM
YDOT
PRO
-7
4-10
F 06 81 DELTA VS-LV(CSI)
COPY YDOT FROM CSM AND LOAD NEGATIVE IN R2 CSIIN81I
DELTA VX(LV)
DELTA VYILV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (COH)
CDH(82)
DELTA VX(LV)
- DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RANGE AND RDOT FOR 3RD CS BU
COMPUTE CSI BU
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (i2000OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
(TRANSMIT CSI DATA TO CSMI VHF A XMTR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF TELEMETY PCM - LO
KEY VB3E F 16 54 R ROOT THETA
SET ORDEAL PRO
317R RANGE
440R RANGE RATE
4-11
400+3 AGS ALIGN t40OR (00000 COMPLETE)
277R THETA
PRO F 37 BB
-6 KEY 41E (RCS THRUSTING) F 50 18 FDAI-ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTAV 400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTAV 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA RF
TRANSMIT TGT DELTA VS TO CSM AND SYNC COUNTDOWN
16 85 DELTA VS-BODY
502R DELTA VZ (NOM 5Ql)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTAVS-BODY
(123t26t27) BURN +Z
NULL DELTA VS
4-12
VERIFY AGS RESIDUALS 50OR 501R 502R DELTA VX _ DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
CDH
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
KEY V67E (RESET W MATRIX) F 06 99 +0200E +O0020E +00005E
PRO
507+0 Z-AXIS BORESIGHT
(VHF RANGING WITH CSM) VHF A XMTR - VOICERNG VHF B XMTR - OFF VHF B RCVR - ON TELEMETRY PCM - HI
(12331) KEY V37E33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 a TIG CDH (NOM 1242425) -120 amp00 10 (AGS 0 TIME)
(CONVERT TO MINUTES)
411+0 THRUST ALONG Z-BODY AXIS ENTER IF YOU DONT TARGET CSI
373R (NOM 26443 310R TIME TO CDH
4-13
423R DESIRED ALT RATE AT CDH
402R DELTA Hshy
450R DELTA VX
452R DELTA VZ
623+0 Z-AXIS PARALLEL TO CSM PLANE
IPRO F 16 45 MKS TFI -00001
-52 RESET ET
KEY V93E (REINIT W MATRIX WHEN MARKS =4)
KEY V32E (MARKS = 3)
F 06 75 DELTA HCDH DELTA TCDHTPI DELTA TTPI PRO
F 06 81 DELTA VCDH-LV CDH(N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
-47 KEY VSOE (OUT-OF-PLANE)
_ TIG CDH (NOM 124t24t25) -3000 TIME FROM CDH
F 06 16 l1 LOAD TIG PLANE CHANGE (NOM 123amp54-253 PRO
F 06 90 Y YDOT PSI N90 CSM
VYDOT PRO
-42 KEY V32E (MARKS=1O)
F 06 75 DELTA HCDH DELTA TCDIHTPI DELTA TTPITPI PRO
F 06 81 DELTA VCDH-LV
4-14
CDH (NS1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -OO1
KEY V34E (TERMINATE) F 37 B8
PLANE CHANGE
KEY 30E (EXTERNAL DELTA V)
TIG CDH (NOM 124124t25) -3000 TIME FROM CDH
F 06 33 LOAD TIG PLANE CHANGE (NOM 123154T25) PRO
F 06 81 DELTA VS-LV (NOM 00)
-36 COPY RDOT FOR 1ST CDH BU
KEY V90E (OUT-OF-PLANE)
F 06 16 1 1 LOAD TIG PLANE CHANGE (NOM 1231543251 PRO
F 06 90 Y YOOT PSI N90 CSM
YDOT
PRO
F 06 81 DELTA VS-LV(NOM 00)
COPY YDOT AND LOAD NEGATIVE IN R2 PRO
F 06 42 HA HP DELTA V PRO
F 16 45 MKS TFI MGA
PRO
F 37 BB
KEY 41E (RCS THRUSTING)
-30
4-15
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVRI
410+5 EXTERNAL DELTA V 450+0 451-YDOT 452+0 (LOAD CSM -YDOT)
407+0 ROTATE EXTERNAL DELTA V RF
16 95 DELTA VS-BODY
-3035 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATTVHOLD 407+1 FREEZE EXTERNAL DELTAV
F 16 85 DELTA VS-BODY -
NULL DELTA VIS
PRO F 37BB
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
507+0 Z-AXIS BORESIGHT
(12356) KEY 33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 TIG CDH (NOM 124t24t25) -120 OO ZOO (AGS 0 TIME)
(CONVERT TO MINUTES)
373R _ (NOM 2644) 310R TIME TO CDH
423R DESIRED ALT RATE AT CDH
(ADS OF MSFN) S-BAND - SLEW TOP = ACQUIRE HGA LOCK ON VOICE - BUVOICE -- VOICE VERIFY VOICE TLM BIOMED - LEFT (OR RIGHT)
402R DELTAH
4-16
F 16 45
-25
-23
F 06 75
F 06 81
F 16 45
-12
F 06 75
F 06 81
450R DELTA VX
452R DELTA VZ
PRO MKS TFI -00001
KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
COPY ROOT FOR 2ND CDH BU
KEY v32E (MARKS = 5)
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40DEG TO 1OODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + B PRESS IND PSIA
A QUANTITY IND _ PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING a TEMP MON SEL RCS QUAD 1 4 2 3 (120 - 190 DEG F)i
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
CDH(NB1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO MKS TFI -00001
PRO (FINAL COMP)
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
KEY V9OE (OUT-OF-PLANE)
-7
4-17
F 06 16 jj LOAD TIG CDH FROM DATA PAD (NOM 12424251 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT PRO
COPY YOOT FROM CSM AND LOAD NEGATIVE IN R2
CDH(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RDOT FOR 3RD CDH BU
COMPUTE CDH BU
TRANSMIT TGT DELTA VOS TO CSM AND SYNC COUNTDOWN
KEY V47E (INITIALIZE AGS F 06 16 GET OF AGS 0 TIME 120O00OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
KEY V83E F 16 54 R RDOT THETA
SET ORDEAL PRO
317R _ RANGE
440R RANGE RATE 400+3 AGS ALIGN 40OR (00000 COMPLETE)
277R THETA
-6
4-18
PRO F 3 BB
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY V06N86E F 06 86 DELTA VIS-LV
AGS(N86) CHART
DELTA VX(LVD
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
16 85 DELTA VS-BODY
50OR DELTA VX (NOM -0O3)
502R DELTA VZ (NOM 60)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD 407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS BODY
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS 5OOR 50IR 502R DELTA VX -DELTA VY DELTA VZ-
VERIFY PGNS RESIDUALS N85
DELTA VX(LM)
4-19
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
TPI
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO 507+0 Z-AXIS BORESIGHT
(12426) KEY 34E (TPI)
-36 RESET ET
F 06 37 - amp LOAD TIG TPI FROM DATA PAD (NOM 1250246) PRO
F 06 55 +00000 +02660E +13000 OMEGAT PRO
F 16 45 MARKS TFI -00001
-32 KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
-29 KEY V32E (MARKS = 3)
F 06 37 __ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
RESET ET
410+3 TPI SEARCH ROUTINE 307+04300 DELTA T TRANSFER
4-20
-26 310+02600 TFI TPI
303R THETA AT TPI
267R DELTA VTPI
371R DELTA VTPI + DELTA VTPF
KEY V32E (MARKS = 10)
F 06 37 _ _ _ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VIS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
TEMPIPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40ODEG TO IGODEG F A + B PRESS IND 181 +-3 PSIA
TEMPIPRESS MON SEL - HEL
A + B PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD I 4 2 3 (120 - 190 DEG F)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
RESET ET
-13 310+01300 TFI TPI
303R THETA AT TPI
-12 PRO (FINAL COMP) F 06 37 Z TIG TPIj__
4-21
TRANSMIT TIG OF TPI TO CSM-
PRO F 06 58 HP DELTA VTPI DELTA VTRF
PRO F 06 81 DELTA VS-LV
KEY V9OE (OUT-OF-PLANE)
F 06 16 1 LOAD TIG TPI FROM DATA PAD (NOM 12502461 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT
PRO F 06 81 DELTA VS-LV
COPY CSM YDOT AND LOAD NEGATIVE IN R2 N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 59 DELTA VS LOS
N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI MGA
RESET ET
PRO F 37 BB
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (12000t600)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE)
-10
-6
4-22
F 50 16 DOWNLINK COMPLETE PRO (UPDATE COMPLETE)
400+3 AGS ALIGN 400R (00000 COMPLETE)
-9 277R COPY TGT LOS ANGLE
310+00800
303R THETA AT TPI 410+4 DIRECT TRANSFER AT ET=-8 404+0 405+0 406+0 (MONITOR 470 471 4721
373R TIG TPI
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
KEY 41E (RCS THRUSTING) F 50 18 FOAl ANGLES (REQUEST MNVRI
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
-5 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUS
400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
COMPUTE TPI BU
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
4-23
1685 DELTA VS-BODY
50OR DELTA VX(NOM -115)
502R DELTA VZ(NOM 229)
-Z35 OSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS-BODY
(1250246) BURN +Z
VERIFY AGS RESIDUALS 500R 501R 502R DELTAVX DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
MCC1
KEY V76E (PGNS PULSE) PGNSMODECONT-AUTO
KEY V93E (BEFORE 1ST MARK REINITW MATRIX)
+2 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
4-24
(LOS OF MSFN) S-BAND - SLEW TO P = 90 Y = 0 S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
404+0 405+0 406+0
(MONITOR 470 471 4721
+9 277R COPY TGT LOS ANGLE
+12 PRO (COMPUTE MCC FOR TPI+15I F 06 81 DELTA VS-LV
PRO F 06 59 DELTA VS-LOS
PRO F 16 45 MKS TFI MGA
+13 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUOS
COMPUTE MCC1 BU
PRO F 37 BB
+14 KEY 41E (RCS THRUSTING) F 50 18 FOAL ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+1425 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+15 F 16 85 NULL DELTA VS
PRO F 37 BB
MCC2
KEY V76E (PGNS PULSE)
4-25
PGNS MODE CONT-AUTO
KEY V93E (BEFORE 1ST MARK REINIT W MATRIX)
+16 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
404+0 405+0 406+0 (MONITOR 470 471 47)shy
+24 277R COPY TGT LOS ANGLE
+27 PRO (COMPUTE MCC FORTPI+30) F 06 81 DELTA VS-LV
PRO F 06 59 DELIA VPS-LOS
PRO F 16 45 MKS TFI MGA
+28 277R COPY TGT LOS ANGLE
COPY R RDOT FROM TAPEMETER FOR BUS
COMPUTE MCC2 BU
F 37 BB PRO
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+2925 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+30 F 16 85 NULL DELTA VS
PRO F 37 BB
KEY OOE (P001
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
4-26
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT KEY V34E (TERMINATE)
KEY V37E47E (AVE G) F 16 83 DELTA VIS
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT VERIFY TAPE METER WITH DSKY
BRAKING GATE 30 FPS - 6000 FT 20 FPS - 3000 FT 10 FPS - 1500 FT 5 FPS - 600 FT
RENDEZVOUS
STATION KEEPING
5-1
50 ABORT PROCEDURE
This is a specific AGS nominal abort procedure due to a PGNS failure between insertion and station keeping
51
5-2
Nominal AGS Procedures
ASSUMPTIONS
AFTER INSERTION
I INSERTION COMPLETE (RFSIDUALS NULLED) g PGNS FAILURE BEFORE INSERTION 3 RAUAR NOT LOCKED ON
(UI CoNT-AGS ATlI[uUE MON-AGS(CDR) RATE ERR MON-CNPTR(LMP) ATTITUDE MON-AGS(LMP) SHFITRUN-+5 DEG X-POINTER-HI MULT RADAR IEST Sw-OFF LNb GMbL-OFF ENG ARM-OFF X-IRANSL-2 JETS DEAD BAND-MAX PGNS MODE CONT-OFF THROTJET-JET CB IMU OIR-ON HH MOVE-AUTO rRACK TTCATNANSL-ENABLE(CDR)
AL CPL-ON MODE SL-AGS RNGAL1 MON-RNbRNGRT RAIE ERR MON-RNDZ HDR(CDR) AVl CoNT(3)-PULSE AGS MODE CONT-AUTO ACA4JET-DISABLE(CDR) TTCATRANSL-DISABLE(LMP) ACA4JET-DISABLE(LMP)
bO7+U Z-AXIS BOPESIGHT 400+2 Z-AXIS STEERING PULSE TO NULL AGS ERRORS POINT Z-AXIS IN DIRECTION OF CSM MODE CONT-ATT HOLD ATT CONT(3)-MODE CONTROL O unnr - ZirF
5-3
SLEW PATE - LO
SLEW RR ANT TO OqON FUAI VERIFY MAX SIGNAL STRENGTH RH MOOE-AUTO TRACK NO TRACK LIGHT OFF -
ATT CONT(3h-PULSE
CHECK INSERTION VELOCITY WITH TAPEMETER COMPARE EAPEMETER WITH AGS STATE VECTOR DATA I
17R RANGE(NOM 2642)
440R RANGE RATE(NOM -425l)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
cSI
+3 417+1 (RADAR FILTER INITIALIZED) 41b+l (NO BOHESIGHT) b03-XXXXX RANGE RATE
+5 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGF
41b+1 CSI ROUTINE 373+o2065 CSi TIME 275+03028 TPI TIME 605+0077 COTANGENT OF LOS TO CSM 41b+1 (ONE-HALF OFBITAL-PERIOD) 411+0 HCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT
610R TIME TO CST
43 RESET ET
267R VELOCITY TO BE GAINED CSI
402R FLTA H
371R DFLTA V CDH
5-4
372R DFLTA T CSICDH
-42 415+1 (No BORESIGHT) bO6-xXXXX RANGE RATE
-40 415+1 (NO BORESIGHT)503-XXXXX RANGE RATE dORESIGHT ON CSM
415+1 316+XXXXX RANGE
-37 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE
-15 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE UORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-2 415+1 (No BOHESIGHT) bO3-XXXXX RANGF RATE
i1uR TIME TO CS
RESEF ET
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-30 COPY ROOT FOR 1ST CSI 81J
BORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-t7 415+1 (NO BORFSIGHT) 50-XXxXx RANGF RATE
267R VELOCITY TO HE GAINED CSI
402R LELTA H
371R OFLTA V COH
372R OELTA T CSICDH
-5 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 blb+XXXXX RANGE
-i2 415+1 (No BORESIGHT) 5n3-XXXXX RANGE RATE
415+1 (NO BORESIGHT)
5-5
503-XXXXX RANGF RATE
COPY Roor FOR 2NO CSI BU
bORESIGHT ON CSM 415+1 316+XXXXX RANGE
TEMPPRESS MON SEL - FUEL MAN
A AND 8 PRESS 181 +-3 PIG TEMPPRESS MON SEL - PRPLNT
A AND B TEMP IND 4ODEG 0 IOODEG F A AND B PRFSS IND 181 +-3 PSIA
tEMPPRESS MON SEL - HEL
A AND 8 PRESS IND PSIA
A QUANTITY IND- -- PERCENT RFMAINING
8 QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4p 2 3 (120 - 190 DFG F)
415+1 (NO BORESIGHT)-17 503-XXXXX RANGE RATE
-15 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
(LOS OF MSFN) S-BAND - SLEW 10 P = +90t Y U S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
-12 415+1 (No 8ORESIGHT)
503-XXXXX RANGE RATE
267R VFLOCITY TU BE GAINED CSI
402R OFLTA H
372R TIME CSICH
371R PREDICTED VEL 10 RE GAINED COH
263R OLT-OF-PLANE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATL
-10 COPY RANGE AND ROOT FOR 3RD CSI 8U
SORESIGH ON CSM 41b+1
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
4-7
ENTR (BYPASS MNVR) NO TRK LT-OFF
F 50 72 RR TRUNSHFT VERIFY RR LOCK ON PRO
DSKY BLANKS
KEY V93E (BEFORE 1ST MARK REINIT W MATRIXI KEY V80E (UPDATE LM SV)
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (i20OOZOO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
400+3 AGS ALIGNshy400R (00000 COMPLETE) 507+0 Z-AXIS BORESIGHT 400+2 ACQUISITION STEERING
CS
(122amp55) KEY V37E32E (CSI)
F 06 11 1 S LOAD TIG CSI FROM DATA PAD (NOM 123S26- 271 PRO
F 06 55 +O000IN +02660E +13000 OMEGAT (CDH 180 DEG AFTER CSI PRO
F 06 37 LOAD TIG TPI FROM DATA PAD (NOM 1251021761 PRO
F 16 45 MKS TFI -00001
-30 COPY RDOT FOR 1ST CSI BU
31OR TIME TO CSI
267R VELOCITY TO BE GAINED CSI
402R DELTA H
371R DELTA V CDH
-22
4-8
372R _ DELTA T CSICDH
KEY V32E (MARKS=5
F 06 75 DELTA H DELTA T CSICDH DELTA T CDHTPI PRO
F 06 81 DELTA VOS-LV (CS) (NOM 501 DELTA VX)
CSI(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (CDH)
(NOM 60 DELTA VX) CDH(82)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
KEY V32E (MARKS=1C)
F 06 75 DELTA H DELTA TCSICDH DELTA TCDHTPI PRD
F 06 81 DELTA VS-LV (CSI) CSI(N811
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 82 DELTA VIS-LV(CDH)
CDH(82)
DELTA VX(LVI
DELTA VY(LV)
DELTA VZ(LV)
-12
4-9
-20 COPY RDOT FOR 2ND CSI BU
F 16 45
F 06 75
F 06 81
F 06 16
F 06 90
PRO MKS TFI -00001
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS NON SEL - PRPLNT A + B TEMP IND 40DEG TO lOODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + 8 PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4v 2 3 (120 - 190 DEG F
(LOS OF MSFN ) S-BAND - SLEW TO P = +90 Y a 0 S-BAND - FWD (OR AFT) S-BAND - DN VOICE BU BIOMED OFF
PRO (FINAL COMP)
267R - VELOCITY TO BE GAINED CSI
402R DELTA H
372R TIME CSICDHL
371R PREDICTED VEL TO BE GAINED CDH
263R OUT-OF-PLANE
DELTA H DELTA TCSICDH DELTA TCDHTPI PRO DELTA VS-LV (CSI)
KEY V9OE (OUT-OF-PLANED
0 LOAD TIG CSI FROM DATA PAD (NOM 12302627) PRO Y YDOT PSI
N90 CSM
YDOT
PRO
-7
4-10
F 06 81 DELTA VS-LV(CSI)
COPY YDOT FROM CSM AND LOAD NEGATIVE IN R2 CSIIN81I
DELTA VX(LV)
DELTA VYILV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (COH)
CDH(82)
DELTA VX(LV)
- DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RANGE AND RDOT FOR 3RD CS BU
COMPUTE CSI BU
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (i2000OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
(TRANSMIT CSI DATA TO CSMI VHF A XMTR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF TELEMETY PCM - LO
KEY VB3E F 16 54 R ROOT THETA
SET ORDEAL PRO
317R RANGE
440R RANGE RATE
4-11
400+3 AGS ALIGN t40OR (00000 COMPLETE)
277R THETA
PRO F 37 BB
-6 KEY 41E (RCS THRUSTING) F 50 18 FDAI-ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTAV 400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTAV 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA RF
TRANSMIT TGT DELTA VS TO CSM AND SYNC COUNTDOWN
16 85 DELTA VS-BODY
502R DELTA VZ (NOM 5Ql)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTAVS-BODY
(123t26t27) BURN +Z
NULL DELTA VS
4-12
VERIFY AGS RESIDUALS 50OR 501R 502R DELTA VX _ DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
CDH
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
KEY V67E (RESET W MATRIX) F 06 99 +0200E +O0020E +00005E
PRO
507+0 Z-AXIS BORESIGHT
(VHF RANGING WITH CSM) VHF A XMTR - VOICERNG VHF B XMTR - OFF VHF B RCVR - ON TELEMETRY PCM - HI
(12331) KEY V37E33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 a TIG CDH (NOM 1242425) -120 amp00 10 (AGS 0 TIME)
(CONVERT TO MINUTES)
411+0 THRUST ALONG Z-BODY AXIS ENTER IF YOU DONT TARGET CSI
373R (NOM 26443 310R TIME TO CDH
4-13
423R DESIRED ALT RATE AT CDH
402R DELTA Hshy
450R DELTA VX
452R DELTA VZ
623+0 Z-AXIS PARALLEL TO CSM PLANE
IPRO F 16 45 MKS TFI -00001
-52 RESET ET
KEY V93E (REINIT W MATRIX WHEN MARKS =4)
KEY V32E (MARKS = 3)
F 06 75 DELTA HCDH DELTA TCDHTPI DELTA TTPI PRO
F 06 81 DELTA VCDH-LV CDH(N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
-47 KEY VSOE (OUT-OF-PLANE)
_ TIG CDH (NOM 124t24t25) -3000 TIME FROM CDH
F 06 16 l1 LOAD TIG PLANE CHANGE (NOM 123amp54-253 PRO
F 06 90 Y YDOT PSI N90 CSM
VYDOT PRO
-42 KEY V32E (MARKS=1O)
F 06 75 DELTA HCDH DELTA TCDIHTPI DELTA TTPITPI PRO
F 06 81 DELTA VCDH-LV
4-14
CDH (NS1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -OO1
KEY V34E (TERMINATE) F 37 B8
PLANE CHANGE
KEY 30E (EXTERNAL DELTA V)
TIG CDH (NOM 124124t25) -3000 TIME FROM CDH
F 06 33 LOAD TIG PLANE CHANGE (NOM 123154T25) PRO
F 06 81 DELTA VS-LV (NOM 00)
-36 COPY RDOT FOR 1ST CDH BU
KEY V90E (OUT-OF-PLANE)
F 06 16 1 1 LOAD TIG PLANE CHANGE (NOM 1231543251 PRO
F 06 90 Y YOOT PSI N90 CSM
YDOT
PRO
F 06 81 DELTA VS-LV(NOM 00)
COPY YDOT AND LOAD NEGATIVE IN R2 PRO
F 06 42 HA HP DELTA V PRO
F 16 45 MKS TFI MGA
PRO
F 37 BB
KEY 41E (RCS THRUSTING)
-30
4-15
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVRI
410+5 EXTERNAL DELTA V 450+0 451-YDOT 452+0 (LOAD CSM -YDOT)
407+0 ROTATE EXTERNAL DELTA V RF
16 95 DELTA VS-BODY
-3035 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATTVHOLD 407+1 FREEZE EXTERNAL DELTAV
F 16 85 DELTA VS-BODY -
NULL DELTA VIS
PRO F 37BB
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
507+0 Z-AXIS BORESIGHT
(12356) KEY 33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 TIG CDH (NOM 124t24t25) -120 OO ZOO (AGS 0 TIME)
(CONVERT TO MINUTES)
373R _ (NOM 2644) 310R TIME TO CDH
423R DESIRED ALT RATE AT CDH
(ADS OF MSFN) S-BAND - SLEW TOP = ACQUIRE HGA LOCK ON VOICE - BUVOICE -- VOICE VERIFY VOICE TLM BIOMED - LEFT (OR RIGHT)
402R DELTAH
4-16
F 16 45
-25
-23
F 06 75
F 06 81
F 16 45
-12
F 06 75
F 06 81
450R DELTA VX
452R DELTA VZ
PRO MKS TFI -00001
KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
COPY ROOT FOR 2ND CDH BU
KEY v32E (MARKS = 5)
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40DEG TO 1OODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + B PRESS IND PSIA
A QUANTITY IND _ PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING a TEMP MON SEL RCS QUAD 1 4 2 3 (120 - 190 DEG F)i
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
CDH(NB1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO MKS TFI -00001
PRO (FINAL COMP)
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
KEY V9OE (OUT-OF-PLANE)
-7
4-17
F 06 16 jj LOAD TIG CDH FROM DATA PAD (NOM 12424251 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT PRO
COPY YOOT FROM CSM AND LOAD NEGATIVE IN R2
CDH(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RDOT FOR 3RD CDH BU
COMPUTE CDH BU
TRANSMIT TGT DELTA VOS TO CSM AND SYNC COUNTDOWN
KEY V47E (INITIALIZE AGS F 06 16 GET OF AGS 0 TIME 120O00OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
KEY V83E F 16 54 R RDOT THETA
SET ORDEAL PRO
317R _ RANGE
440R RANGE RATE 400+3 AGS ALIGN 40OR (00000 COMPLETE)
277R THETA
-6
4-18
PRO F 3 BB
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY V06N86E F 06 86 DELTA VIS-LV
AGS(N86) CHART
DELTA VX(LVD
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
16 85 DELTA VS-BODY
50OR DELTA VX (NOM -0O3)
502R DELTA VZ (NOM 60)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD 407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS BODY
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS 5OOR 50IR 502R DELTA VX -DELTA VY DELTA VZ-
VERIFY PGNS RESIDUALS N85
DELTA VX(LM)
4-19
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
TPI
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO 507+0 Z-AXIS BORESIGHT
(12426) KEY 34E (TPI)
-36 RESET ET
F 06 37 - amp LOAD TIG TPI FROM DATA PAD (NOM 1250246) PRO
F 06 55 +00000 +02660E +13000 OMEGAT PRO
F 16 45 MARKS TFI -00001
-32 KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
-29 KEY V32E (MARKS = 3)
F 06 37 __ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
RESET ET
410+3 TPI SEARCH ROUTINE 307+04300 DELTA T TRANSFER
4-20
-26 310+02600 TFI TPI
303R THETA AT TPI
267R DELTA VTPI
371R DELTA VTPI + DELTA VTPF
KEY V32E (MARKS = 10)
F 06 37 _ _ _ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VIS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
TEMPIPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40ODEG TO IGODEG F A + B PRESS IND 181 +-3 PSIA
TEMPIPRESS MON SEL - HEL
A + B PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD I 4 2 3 (120 - 190 DEG F)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
RESET ET
-13 310+01300 TFI TPI
303R THETA AT TPI
-12 PRO (FINAL COMP) F 06 37 Z TIG TPIj__
4-21
TRANSMIT TIG OF TPI TO CSM-
PRO F 06 58 HP DELTA VTPI DELTA VTRF
PRO F 06 81 DELTA VS-LV
KEY V9OE (OUT-OF-PLANE)
F 06 16 1 LOAD TIG TPI FROM DATA PAD (NOM 12502461 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT
PRO F 06 81 DELTA VS-LV
COPY CSM YDOT AND LOAD NEGATIVE IN R2 N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 59 DELTA VS LOS
N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI MGA
RESET ET
PRO F 37 BB
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (12000t600)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE)
-10
-6
4-22
F 50 16 DOWNLINK COMPLETE PRO (UPDATE COMPLETE)
400+3 AGS ALIGN 400R (00000 COMPLETE)
-9 277R COPY TGT LOS ANGLE
310+00800
303R THETA AT TPI 410+4 DIRECT TRANSFER AT ET=-8 404+0 405+0 406+0 (MONITOR 470 471 4721
373R TIG TPI
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
KEY 41E (RCS THRUSTING) F 50 18 FOAl ANGLES (REQUEST MNVRI
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
-5 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUS
400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
COMPUTE TPI BU
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
4-23
1685 DELTA VS-BODY
50OR DELTA VX(NOM -115)
502R DELTA VZ(NOM 229)
-Z35 OSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS-BODY
(1250246) BURN +Z
VERIFY AGS RESIDUALS 500R 501R 502R DELTAVX DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
MCC1
KEY V76E (PGNS PULSE) PGNSMODECONT-AUTO
KEY V93E (BEFORE 1ST MARK REINITW MATRIX)
+2 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
4-24
(LOS OF MSFN) S-BAND - SLEW TO P = 90 Y = 0 S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
404+0 405+0 406+0
(MONITOR 470 471 4721
+9 277R COPY TGT LOS ANGLE
+12 PRO (COMPUTE MCC FOR TPI+15I F 06 81 DELTA VS-LV
PRO F 06 59 DELTA VS-LOS
PRO F 16 45 MKS TFI MGA
+13 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUOS
COMPUTE MCC1 BU
PRO F 37 BB
+14 KEY 41E (RCS THRUSTING) F 50 18 FOAL ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+1425 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+15 F 16 85 NULL DELTA VS
PRO F 37 BB
MCC2
KEY V76E (PGNS PULSE)
4-25
PGNS MODE CONT-AUTO
KEY V93E (BEFORE 1ST MARK REINIT W MATRIX)
+16 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
404+0 405+0 406+0 (MONITOR 470 471 47)shy
+24 277R COPY TGT LOS ANGLE
+27 PRO (COMPUTE MCC FORTPI+30) F 06 81 DELTA VS-LV
PRO F 06 59 DELIA VPS-LOS
PRO F 16 45 MKS TFI MGA
+28 277R COPY TGT LOS ANGLE
COPY R RDOT FROM TAPEMETER FOR BUS
COMPUTE MCC2 BU
F 37 BB PRO
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+2925 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+30 F 16 85 NULL DELTA VS
PRO F 37 BB
KEY OOE (P001
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
4-26
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT KEY V34E (TERMINATE)
KEY V37E47E (AVE G) F 16 83 DELTA VIS
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT VERIFY TAPE METER WITH DSKY
BRAKING GATE 30 FPS - 6000 FT 20 FPS - 3000 FT 10 FPS - 1500 FT 5 FPS - 600 FT
RENDEZVOUS
STATION KEEPING
5-1
50 ABORT PROCEDURE
This is a specific AGS nominal abort procedure due to a PGNS failure between insertion and station keeping
51
5-2
Nominal AGS Procedures
ASSUMPTIONS
AFTER INSERTION
I INSERTION COMPLETE (RFSIDUALS NULLED) g PGNS FAILURE BEFORE INSERTION 3 RAUAR NOT LOCKED ON
(UI CoNT-AGS ATlI[uUE MON-AGS(CDR) RATE ERR MON-CNPTR(LMP) ATTITUDE MON-AGS(LMP) SHFITRUN-+5 DEG X-POINTER-HI MULT RADAR IEST Sw-OFF LNb GMbL-OFF ENG ARM-OFF X-IRANSL-2 JETS DEAD BAND-MAX PGNS MODE CONT-OFF THROTJET-JET CB IMU OIR-ON HH MOVE-AUTO rRACK TTCATNANSL-ENABLE(CDR)
AL CPL-ON MODE SL-AGS RNGAL1 MON-RNbRNGRT RAIE ERR MON-RNDZ HDR(CDR) AVl CoNT(3)-PULSE AGS MODE CONT-AUTO ACA4JET-DISABLE(CDR) TTCATRANSL-DISABLE(LMP) ACA4JET-DISABLE(LMP)
bO7+U Z-AXIS BOPESIGHT 400+2 Z-AXIS STEERING PULSE TO NULL AGS ERRORS POINT Z-AXIS IN DIRECTION OF CSM MODE CONT-ATT HOLD ATT CONT(3)-MODE CONTROL O unnr - ZirF
5-3
SLEW PATE - LO
SLEW RR ANT TO OqON FUAI VERIFY MAX SIGNAL STRENGTH RH MOOE-AUTO TRACK NO TRACK LIGHT OFF -
ATT CONT(3h-PULSE
CHECK INSERTION VELOCITY WITH TAPEMETER COMPARE EAPEMETER WITH AGS STATE VECTOR DATA I
17R RANGE(NOM 2642)
440R RANGE RATE(NOM -425l)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
cSI
+3 417+1 (RADAR FILTER INITIALIZED) 41b+l (NO BOHESIGHT) b03-XXXXX RANGE RATE
+5 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGF
41b+1 CSI ROUTINE 373+o2065 CSi TIME 275+03028 TPI TIME 605+0077 COTANGENT OF LOS TO CSM 41b+1 (ONE-HALF OFBITAL-PERIOD) 411+0 HCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT
610R TIME TO CST
43 RESET ET
267R VELOCITY TO BE GAINED CSI
402R FLTA H
371R DFLTA V CDH
5-4
372R DFLTA T CSICDH
-42 415+1 (No BORESIGHT) bO6-xXXXX RANGE RATE
-40 415+1 (NO BORESIGHT)503-XXXXX RANGE RATE dORESIGHT ON CSM
415+1 316+XXXXX RANGE
-37 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE
-15 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE UORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-2 415+1 (No BOHESIGHT) bO3-XXXXX RANGF RATE
i1uR TIME TO CS
RESEF ET
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-30 COPY ROOT FOR 1ST CSI 81J
BORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-t7 415+1 (NO BORFSIGHT) 50-XXxXx RANGF RATE
267R VELOCITY TO HE GAINED CSI
402R LELTA H
371R OFLTA V COH
372R OELTA T CSICDH
-5 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 blb+XXXXX RANGE
-i2 415+1 (No BORESIGHT) 5n3-XXXXX RANGE RATE
415+1 (NO BORESIGHT)
5-5
503-XXXXX RANGF RATE
COPY Roor FOR 2NO CSI BU
bORESIGHT ON CSM 415+1 316+XXXXX RANGE
TEMPPRESS MON SEL - FUEL MAN
A AND 8 PRESS 181 +-3 PIG TEMPPRESS MON SEL - PRPLNT
A AND B TEMP IND 4ODEG 0 IOODEG F A AND B PRFSS IND 181 +-3 PSIA
tEMPPRESS MON SEL - HEL
A AND 8 PRESS IND PSIA
A QUANTITY IND- -- PERCENT RFMAINING
8 QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4p 2 3 (120 - 190 DFG F)
415+1 (NO BORESIGHT)-17 503-XXXXX RANGE RATE
-15 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
(LOS OF MSFN) S-BAND - SLEW 10 P = +90t Y U S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
-12 415+1 (No 8ORESIGHT)
503-XXXXX RANGE RATE
267R VFLOCITY TU BE GAINED CSI
402R OFLTA H
372R TIME CSICH
371R PREDICTED VEL 10 RE GAINED COH
263R OLT-OF-PLANE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATL
-10 COPY RANGE AND ROOT FOR 3RD CSI 8U
SORESIGH ON CSM 41b+1
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
-22
4-8
372R _ DELTA T CSICDH
KEY V32E (MARKS=5
F 06 75 DELTA H DELTA T CSICDH DELTA T CDHTPI PRO
F 06 81 DELTA VOS-LV (CS) (NOM 501 DELTA VX)
CSI(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (CDH)
(NOM 60 DELTA VX) CDH(82)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
KEY V32E (MARKS=1C)
F 06 75 DELTA H DELTA TCSICDH DELTA TCDHTPI PRD
F 06 81 DELTA VS-LV (CSI) CSI(N811
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 82 DELTA VIS-LV(CDH)
CDH(82)
DELTA VX(LVI
DELTA VY(LV)
DELTA VZ(LV)
-12
4-9
-20 COPY RDOT FOR 2ND CSI BU
F 16 45
F 06 75
F 06 81
F 06 16
F 06 90
PRO MKS TFI -00001
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS NON SEL - PRPLNT A + B TEMP IND 40DEG TO lOODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + 8 PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4v 2 3 (120 - 190 DEG F
(LOS OF MSFN ) S-BAND - SLEW TO P = +90 Y a 0 S-BAND - FWD (OR AFT) S-BAND - DN VOICE BU BIOMED OFF
PRO (FINAL COMP)
267R - VELOCITY TO BE GAINED CSI
402R DELTA H
372R TIME CSICDHL
371R PREDICTED VEL TO BE GAINED CDH
263R OUT-OF-PLANE
DELTA H DELTA TCSICDH DELTA TCDHTPI PRO DELTA VS-LV (CSI)
KEY V9OE (OUT-OF-PLANED
0 LOAD TIG CSI FROM DATA PAD (NOM 12302627) PRO Y YDOT PSI
N90 CSM
YDOT
PRO
-7
4-10
F 06 81 DELTA VS-LV(CSI)
COPY YDOT FROM CSM AND LOAD NEGATIVE IN R2 CSIIN81I
DELTA VX(LV)
DELTA VYILV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (COH)
CDH(82)
DELTA VX(LV)
- DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RANGE AND RDOT FOR 3RD CS BU
COMPUTE CSI BU
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (i2000OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
(TRANSMIT CSI DATA TO CSMI VHF A XMTR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF TELEMETY PCM - LO
KEY VB3E F 16 54 R ROOT THETA
SET ORDEAL PRO
317R RANGE
440R RANGE RATE
4-11
400+3 AGS ALIGN t40OR (00000 COMPLETE)
277R THETA
PRO F 37 BB
-6 KEY 41E (RCS THRUSTING) F 50 18 FDAI-ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTAV 400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTAV 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA RF
TRANSMIT TGT DELTA VS TO CSM AND SYNC COUNTDOWN
16 85 DELTA VS-BODY
502R DELTA VZ (NOM 5Ql)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTAVS-BODY
(123t26t27) BURN +Z
NULL DELTA VS
4-12
VERIFY AGS RESIDUALS 50OR 501R 502R DELTA VX _ DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
CDH
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
KEY V67E (RESET W MATRIX) F 06 99 +0200E +O0020E +00005E
PRO
507+0 Z-AXIS BORESIGHT
(VHF RANGING WITH CSM) VHF A XMTR - VOICERNG VHF B XMTR - OFF VHF B RCVR - ON TELEMETRY PCM - HI
(12331) KEY V37E33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 a TIG CDH (NOM 1242425) -120 amp00 10 (AGS 0 TIME)
(CONVERT TO MINUTES)
411+0 THRUST ALONG Z-BODY AXIS ENTER IF YOU DONT TARGET CSI
373R (NOM 26443 310R TIME TO CDH
4-13
423R DESIRED ALT RATE AT CDH
402R DELTA Hshy
450R DELTA VX
452R DELTA VZ
623+0 Z-AXIS PARALLEL TO CSM PLANE
IPRO F 16 45 MKS TFI -00001
-52 RESET ET
KEY V93E (REINIT W MATRIX WHEN MARKS =4)
KEY V32E (MARKS = 3)
F 06 75 DELTA HCDH DELTA TCDHTPI DELTA TTPI PRO
F 06 81 DELTA VCDH-LV CDH(N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
-47 KEY VSOE (OUT-OF-PLANE)
_ TIG CDH (NOM 124t24t25) -3000 TIME FROM CDH
F 06 16 l1 LOAD TIG PLANE CHANGE (NOM 123amp54-253 PRO
F 06 90 Y YDOT PSI N90 CSM
VYDOT PRO
-42 KEY V32E (MARKS=1O)
F 06 75 DELTA HCDH DELTA TCDIHTPI DELTA TTPITPI PRO
F 06 81 DELTA VCDH-LV
4-14
CDH (NS1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -OO1
KEY V34E (TERMINATE) F 37 B8
PLANE CHANGE
KEY 30E (EXTERNAL DELTA V)
TIG CDH (NOM 124124t25) -3000 TIME FROM CDH
F 06 33 LOAD TIG PLANE CHANGE (NOM 123154T25) PRO
F 06 81 DELTA VS-LV (NOM 00)
-36 COPY RDOT FOR 1ST CDH BU
KEY V90E (OUT-OF-PLANE)
F 06 16 1 1 LOAD TIG PLANE CHANGE (NOM 1231543251 PRO
F 06 90 Y YOOT PSI N90 CSM
YDOT
PRO
F 06 81 DELTA VS-LV(NOM 00)
COPY YDOT AND LOAD NEGATIVE IN R2 PRO
F 06 42 HA HP DELTA V PRO
F 16 45 MKS TFI MGA
PRO
F 37 BB
KEY 41E (RCS THRUSTING)
-30
4-15
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVRI
410+5 EXTERNAL DELTA V 450+0 451-YDOT 452+0 (LOAD CSM -YDOT)
407+0 ROTATE EXTERNAL DELTA V RF
16 95 DELTA VS-BODY
-3035 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATTVHOLD 407+1 FREEZE EXTERNAL DELTAV
F 16 85 DELTA VS-BODY -
NULL DELTA VIS
PRO F 37BB
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
507+0 Z-AXIS BORESIGHT
(12356) KEY 33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 TIG CDH (NOM 124t24t25) -120 OO ZOO (AGS 0 TIME)
(CONVERT TO MINUTES)
373R _ (NOM 2644) 310R TIME TO CDH
423R DESIRED ALT RATE AT CDH
(ADS OF MSFN) S-BAND - SLEW TOP = ACQUIRE HGA LOCK ON VOICE - BUVOICE -- VOICE VERIFY VOICE TLM BIOMED - LEFT (OR RIGHT)
402R DELTAH
4-16
F 16 45
-25
-23
F 06 75
F 06 81
F 16 45
-12
F 06 75
F 06 81
450R DELTA VX
452R DELTA VZ
PRO MKS TFI -00001
KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
COPY ROOT FOR 2ND CDH BU
KEY v32E (MARKS = 5)
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40DEG TO 1OODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + B PRESS IND PSIA
A QUANTITY IND _ PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING a TEMP MON SEL RCS QUAD 1 4 2 3 (120 - 190 DEG F)i
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
CDH(NB1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO MKS TFI -00001
PRO (FINAL COMP)
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
KEY V9OE (OUT-OF-PLANE)
-7
4-17
F 06 16 jj LOAD TIG CDH FROM DATA PAD (NOM 12424251 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT PRO
COPY YOOT FROM CSM AND LOAD NEGATIVE IN R2
CDH(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RDOT FOR 3RD CDH BU
COMPUTE CDH BU
TRANSMIT TGT DELTA VOS TO CSM AND SYNC COUNTDOWN
KEY V47E (INITIALIZE AGS F 06 16 GET OF AGS 0 TIME 120O00OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
KEY V83E F 16 54 R RDOT THETA
SET ORDEAL PRO
317R _ RANGE
440R RANGE RATE 400+3 AGS ALIGN 40OR (00000 COMPLETE)
277R THETA
-6
4-18
PRO F 3 BB
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY V06N86E F 06 86 DELTA VIS-LV
AGS(N86) CHART
DELTA VX(LVD
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
16 85 DELTA VS-BODY
50OR DELTA VX (NOM -0O3)
502R DELTA VZ (NOM 60)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD 407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS BODY
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS 5OOR 50IR 502R DELTA VX -DELTA VY DELTA VZ-
VERIFY PGNS RESIDUALS N85
DELTA VX(LM)
4-19
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
TPI
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO 507+0 Z-AXIS BORESIGHT
(12426) KEY 34E (TPI)
-36 RESET ET
F 06 37 - amp LOAD TIG TPI FROM DATA PAD (NOM 1250246) PRO
F 06 55 +00000 +02660E +13000 OMEGAT PRO
F 16 45 MARKS TFI -00001
-32 KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
-29 KEY V32E (MARKS = 3)
F 06 37 __ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
RESET ET
410+3 TPI SEARCH ROUTINE 307+04300 DELTA T TRANSFER
4-20
-26 310+02600 TFI TPI
303R THETA AT TPI
267R DELTA VTPI
371R DELTA VTPI + DELTA VTPF
KEY V32E (MARKS = 10)
F 06 37 _ _ _ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VIS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
TEMPIPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40ODEG TO IGODEG F A + B PRESS IND 181 +-3 PSIA
TEMPIPRESS MON SEL - HEL
A + B PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD I 4 2 3 (120 - 190 DEG F)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
RESET ET
-13 310+01300 TFI TPI
303R THETA AT TPI
-12 PRO (FINAL COMP) F 06 37 Z TIG TPIj__
4-21
TRANSMIT TIG OF TPI TO CSM-
PRO F 06 58 HP DELTA VTPI DELTA VTRF
PRO F 06 81 DELTA VS-LV
KEY V9OE (OUT-OF-PLANE)
F 06 16 1 LOAD TIG TPI FROM DATA PAD (NOM 12502461 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT
PRO F 06 81 DELTA VS-LV
COPY CSM YDOT AND LOAD NEGATIVE IN R2 N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 59 DELTA VS LOS
N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI MGA
RESET ET
PRO F 37 BB
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (12000t600)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE)
-10
-6
4-22
F 50 16 DOWNLINK COMPLETE PRO (UPDATE COMPLETE)
400+3 AGS ALIGN 400R (00000 COMPLETE)
-9 277R COPY TGT LOS ANGLE
310+00800
303R THETA AT TPI 410+4 DIRECT TRANSFER AT ET=-8 404+0 405+0 406+0 (MONITOR 470 471 4721
373R TIG TPI
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
KEY 41E (RCS THRUSTING) F 50 18 FOAl ANGLES (REQUEST MNVRI
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
-5 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUS
400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
COMPUTE TPI BU
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
4-23
1685 DELTA VS-BODY
50OR DELTA VX(NOM -115)
502R DELTA VZ(NOM 229)
-Z35 OSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS-BODY
(1250246) BURN +Z
VERIFY AGS RESIDUALS 500R 501R 502R DELTAVX DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
MCC1
KEY V76E (PGNS PULSE) PGNSMODECONT-AUTO
KEY V93E (BEFORE 1ST MARK REINITW MATRIX)
+2 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
4-24
(LOS OF MSFN) S-BAND - SLEW TO P = 90 Y = 0 S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
404+0 405+0 406+0
(MONITOR 470 471 4721
+9 277R COPY TGT LOS ANGLE
+12 PRO (COMPUTE MCC FOR TPI+15I F 06 81 DELTA VS-LV
PRO F 06 59 DELTA VS-LOS
PRO F 16 45 MKS TFI MGA
+13 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUOS
COMPUTE MCC1 BU
PRO F 37 BB
+14 KEY 41E (RCS THRUSTING) F 50 18 FOAL ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+1425 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+15 F 16 85 NULL DELTA VS
PRO F 37 BB
MCC2
KEY V76E (PGNS PULSE)
4-25
PGNS MODE CONT-AUTO
KEY V93E (BEFORE 1ST MARK REINIT W MATRIX)
+16 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
404+0 405+0 406+0 (MONITOR 470 471 47)shy
+24 277R COPY TGT LOS ANGLE
+27 PRO (COMPUTE MCC FORTPI+30) F 06 81 DELTA VS-LV
PRO F 06 59 DELIA VPS-LOS
PRO F 16 45 MKS TFI MGA
+28 277R COPY TGT LOS ANGLE
COPY R RDOT FROM TAPEMETER FOR BUS
COMPUTE MCC2 BU
F 37 BB PRO
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+2925 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+30 F 16 85 NULL DELTA VS
PRO F 37 BB
KEY OOE (P001
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
4-26
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT KEY V34E (TERMINATE)
KEY V37E47E (AVE G) F 16 83 DELTA VIS
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT VERIFY TAPE METER WITH DSKY
BRAKING GATE 30 FPS - 6000 FT 20 FPS - 3000 FT 10 FPS - 1500 FT 5 FPS - 600 FT
RENDEZVOUS
STATION KEEPING
5-1
50 ABORT PROCEDURE
This is a specific AGS nominal abort procedure due to a PGNS failure between insertion and station keeping
51
5-2
Nominal AGS Procedures
ASSUMPTIONS
AFTER INSERTION
I INSERTION COMPLETE (RFSIDUALS NULLED) g PGNS FAILURE BEFORE INSERTION 3 RAUAR NOT LOCKED ON
(UI CoNT-AGS ATlI[uUE MON-AGS(CDR) RATE ERR MON-CNPTR(LMP) ATTITUDE MON-AGS(LMP) SHFITRUN-+5 DEG X-POINTER-HI MULT RADAR IEST Sw-OFF LNb GMbL-OFF ENG ARM-OFF X-IRANSL-2 JETS DEAD BAND-MAX PGNS MODE CONT-OFF THROTJET-JET CB IMU OIR-ON HH MOVE-AUTO rRACK TTCATNANSL-ENABLE(CDR)
AL CPL-ON MODE SL-AGS RNGAL1 MON-RNbRNGRT RAIE ERR MON-RNDZ HDR(CDR) AVl CoNT(3)-PULSE AGS MODE CONT-AUTO ACA4JET-DISABLE(CDR) TTCATRANSL-DISABLE(LMP) ACA4JET-DISABLE(LMP)
bO7+U Z-AXIS BOPESIGHT 400+2 Z-AXIS STEERING PULSE TO NULL AGS ERRORS POINT Z-AXIS IN DIRECTION OF CSM MODE CONT-ATT HOLD ATT CONT(3)-MODE CONTROL O unnr - ZirF
5-3
SLEW PATE - LO
SLEW RR ANT TO OqON FUAI VERIFY MAX SIGNAL STRENGTH RH MOOE-AUTO TRACK NO TRACK LIGHT OFF -
ATT CONT(3h-PULSE
CHECK INSERTION VELOCITY WITH TAPEMETER COMPARE EAPEMETER WITH AGS STATE VECTOR DATA I
17R RANGE(NOM 2642)
440R RANGE RATE(NOM -425l)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
cSI
+3 417+1 (RADAR FILTER INITIALIZED) 41b+l (NO BOHESIGHT) b03-XXXXX RANGE RATE
+5 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGF
41b+1 CSI ROUTINE 373+o2065 CSi TIME 275+03028 TPI TIME 605+0077 COTANGENT OF LOS TO CSM 41b+1 (ONE-HALF OFBITAL-PERIOD) 411+0 HCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT
610R TIME TO CST
43 RESET ET
267R VELOCITY TO BE GAINED CSI
402R FLTA H
371R DFLTA V CDH
5-4
372R DFLTA T CSICDH
-42 415+1 (No BORESIGHT) bO6-xXXXX RANGE RATE
-40 415+1 (NO BORESIGHT)503-XXXXX RANGE RATE dORESIGHT ON CSM
415+1 316+XXXXX RANGE
-37 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE
-15 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE UORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-2 415+1 (No BOHESIGHT) bO3-XXXXX RANGF RATE
i1uR TIME TO CS
RESEF ET
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-30 COPY ROOT FOR 1ST CSI 81J
BORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-t7 415+1 (NO BORFSIGHT) 50-XXxXx RANGF RATE
267R VELOCITY TO HE GAINED CSI
402R LELTA H
371R OFLTA V COH
372R OELTA T CSICDH
-5 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 blb+XXXXX RANGE
-i2 415+1 (No BORESIGHT) 5n3-XXXXX RANGE RATE
415+1 (NO BORESIGHT)
5-5
503-XXXXX RANGF RATE
COPY Roor FOR 2NO CSI BU
bORESIGHT ON CSM 415+1 316+XXXXX RANGE
TEMPPRESS MON SEL - FUEL MAN
A AND 8 PRESS 181 +-3 PIG TEMPPRESS MON SEL - PRPLNT
A AND B TEMP IND 4ODEG 0 IOODEG F A AND B PRFSS IND 181 +-3 PSIA
tEMPPRESS MON SEL - HEL
A AND 8 PRESS IND PSIA
A QUANTITY IND- -- PERCENT RFMAINING
8 QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4p 2 3 (120 - 190 DFG F)
415+1 (NO BORESIGHT)-17 503-XXXXX RANGE RATE
-15 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
(LOS OF MSFN) S-BAND - SLEW 10 P = +90t Y U S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
-12 415+1 (No 8ORESIGHT)
503-XXXXX RANGE RATE
267R VFLOCITY TU BE GAINED CSI
402R OFLTA H
372R TIME CSICH
371R PREDICTED VEL 10 RE GAINED COH
263R OLT-OF-PLANE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATL
-10 COPY RANGE AND ROOT FOR 3RD CSI 8U
SORESIGH ON CSM 41b+1
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
-12
4-9
-20 COPY RDOT FOR 2ND CSI BU
F 16 45
F 06 75
F 06 81
F 06 16
F 06 90
PRO MKS TFI -00001
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS NON SEL - PRPLNT A + B TEMP IND 40DEG TO lOODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + 8 PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4v 2 3 (120 - 190 DEG F
(LOS OF MSFN ) S-BAND - SLEW TO P = +90 Y a 0 S-BAND - FWD (OR AFT) S-BAND - DN VOICE BU BIOMED OFF
PRO (FINAL COMP)
267R - VELOCITY TO BE GAINED CSI
402R DELTA H
372R TIME CSICDHL
371R PREDICTED VEL TO BE GAINED CDH
263R OUT-OF-PLANE
DELTA H DELTA TCSICDH DELTA TCDHTPI PRO DELTA VS-LV (CSI)
KEY V9OE (OUT-OF-PLANED
0 LOAD TIG CSI FROM DATA PAD (NOM 12302627) PRO Y YDOT PSI
N90 CSM
YDOT
PRO
-7
4-10
F 06 81 DELTA VS-LV(CSI)
COPY YDOT FROM CSM AND LOAD NEGATIVE IN R2 CSIIN81I
DELTA VX(LV)
DELTA VYILV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (COH)
CDH(82)
DELTA VX(LV)
- DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RANGE AND RDOT FOR 3RD CS BU
COMPUTE CSI BU
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (i2000OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
(TRANSMIT CSI DATA TO CSMI VHF A XMTR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF TELEMETY PCM - LO
KEY VB3E F 16 54 R ROOT THETA
SET ORDEAL PRO
317R RANGE
440R RANGE RATE
4-11
400+3 AGS ALIGN t40OR (00000 COMPLETE)
277R THETA
PRO F 37 BB
-6 KEY 41E (RCS THRUSTING) F 50 18 FDAI-ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTAV 400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTAV 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA RF
TRANSMIT TGT DELTA VS TO CSM AND SYNC COUNTDOWN
16 85 DELTA VS-BODY
502R DELTA VZ (NOM 5Ql)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTAVS-BODY
(123t26t27) BURN +Z
NULL DELTA VS
4-12
VERIFY AGS RESIDUALS 50OR 501R 502R DELTA VX _ DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
CDH
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
KEY V67E (RESET W MATRIX) F 06 99 +0200E +O0020E +00005E
PRO
507+0 Z-AXIS BORESIGHT
(VHF RANGING WITH CSM) VHF A XMTR - VOICERNG VHF B XMTR - OFF VHF B RCVR - ON TELEMETRY PCM - HI
(12331) KEY V37E33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 a TIG CDH (NOM 1242425) -120 amp00 10 (AGS 0 TIME)
(CONVERT TO MINUTES)
411+0 THRUST ALONG Z-BODY AXIS ENTER IF YOU DONT TARGET CSI
373R (NOM 26443 310R TIME TO CDH
4-13
423R DESIRED ALT RATE AT CDH
402R DELTA Hshy
450R DELTA VX
452R DELTA VZ
623+0 Z-AXIS PARALLEL TO CSM PLANE
IPRO F 16 45 MKS TFI -00001
-52 RESET ET
KEY V93E (REINIT W MATRIX WHEN MARKS =4)
KEY V32E (MARKS = 3)
F 06 75 DELTA HCDH DELTA TCDHTPI DELTA TTPI PRO
F 06 81 DELTA VCDH-LV CDH(N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
-47 KEY VSOE (OUT-OF-PLANE)
_ TIG CDH (NOM 124t24t25) -3000 TIME FROM CDH
F 06 16 l1 LOAD TIG PLANE CHANGE (NOM 123amp54-253 PRO
F 06 90 Y YDOT PSI N90 CSM
VYDOT PRO
-42 KEY V32E (MARKS=1O)
F 06 75 DELTA HCDH DELTA TCDIHTPI DELTA TTPITPI PRO
F 06 81 DELTA VCDH-LV
4-14
CDH (NS1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -OO1
KEY V34E (TERMINATE) F 37 B8
PLANE CHANGE
KEY 30E (EXTERNAL DELTA V)
TIG CDH (NOM 124124t25) -3000 TIME FROM CDH
F 06 33 LOAD TIG PLANE CHANGE (NOM 123154T25) PRO
F 06 81 DELTA VS-LV (NOM 00)
-36 COPY RDOT FOR 1ST CDH BU
KEY V90E (OUT-OF-PLANE)
F 06 16 1 1 LOAD TIG PLANE CHANGE (NOM 1231543251 PRO
F 06 90 Y YOOT PSI N90 CSM
YDOT
PRO
F 06 81 DELTA VS-LV(NOM 00)
COPY YDOT AND LOAD NEGATIVE IN R2 PRO
F 06 42 HA HP DELTA V PRO
F 16 45 MKS TFI MGA
PRO
F 37 BB
KEY 41E (RCS THRUSTING)
-30
4-15
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVRI
410+5 EXTERNAL DELTA V 450+0 451-YDOT 452+0 (LOAD CSM -YDOT)
407+0 ROTATE EXTERNAL DELTA V RF
16 95 DELTA VS-BODY
-3035 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATTVHOLD 407+1 FREEZE EXTERNAL DELTAV
F 16 85 DELTA VS-BODY -
NULL DELTA VIS
PRO F 37BB
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
507+0 Z-AXIS BORESIGHT
(12356) KEY 33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 TIG CDH (NOM 124t24t25) -120 OO ZOO (AGS 0 TIME)
(CONVERT TO MINUTES)
373R _ (NOM 2644) 310R TIME TO CDH
423R DESIRED ALT RATE AT CDH
(ADS OF MSFN) S-BAND - SLEW TOP = ACQUIRE HGA LOCK ON VOICE - BUVOICE -- VOICE VERIFY VOICE TLM BIOMED - LEFT (OR RIGHT)
402R DELTAH
4-16
F 16 45
-25
-23
F 06 75
F 06 81
F 16 45
-12
F 06 75
F 06 81
450R DELTA VX
452R DELTA VZ
PRO MKS TFI -00001
KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
COPY ROOT FOR 2ND CDH BU
KEY v32E (MARKS = 5)
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40DEG TO 1OODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + B PRESS IND PSIA
A QUANTITY IND _ PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING a TEMP MON SEL RCS QUAD 1 4 2 3 (120 - 190 DEG F)i
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
CDH(NB1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO MKS TFI -00001
PRO (FINAL COMP)
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
KEY V9OE (OUT-OF-PLANE)
-7
4-17
F 06 16 jj LOAD TIG CDH FROM DATA PAD (NOM 12424251 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT PRO
COPY YOOT FROM CSM AND LOAD NEGATIVE IN R2
CDH(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RDOT FOR 3RD CDH BU
COMPUTE CDH BU
TRANSMIT TGT DELTA VOS TO CSM AND SYNC COUNTDOWN
KEY V47E (INITIALIZE AGS F 06 16 GET OF AGS 0 TIME 120O00OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
KEY V83E F 16 54 R RDOT THETA
SET ORDEAL PRO
317R _ RANGE
440R RANGE RATE 400+3 AGS ALIGN 40OR (00000 COMPLETE)
277R THETA
-6
4-18
PRO F 3 BB
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY V06N86E F 06 86 DELTA VIS-LV
AGS(N86) CHART
DELTA VX(LVD
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
16 85 DELTA VS-BODY
50OR DELTA VX (NOM -0O3)
502R DELTA VZ (NOM 60)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD 407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS BODY
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS 5OOR 50IR 502R DELTA VX -DELTA VY DELTA VZ-
VERIFY PGNS RESIDUALS N85
DELTA VX(LM)
4-19
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
TPI
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO 507+0 Z-AXIS BORESIGHT
(12426) KEY 34E (TPI)
-36 RESET ET
F 06 37 - amp LOAD TIG TPI FROM DATA PAD (NOM 1250246) PRO
F 06 55 +00000 +02660E +13000 OMEGAT PRO
F 16 45 MARKS TFI -00001
-32 KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
-29 KEY V32E (MARKS = 3)
F 06 37 __ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
RESET ET
410+3 TPI SEARCH ROUTINE 307+04300 DELTA T TRANSFER
4-20
-26 310+02600 TFI TPI
303R THETA AT TPI
267R DELTA VTPI
371R DELTA VTPI + DELTA VTPF
KEY V32E (MARKS = 10)
F 06 37 _ _ _ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VIS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
TEMPIPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40ODEG TO IGODEG F A + B PRESS IND 181 +-3 PSIA
TEMPIPRESS MON SEL - HEL
A + B PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD I 4 2 3 (120 - 190 DEG F)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
RESET ET
-13 310+01300 TFI TPI
303R THETA AT TPI
-12 PRO (FINAL COMP) F 06 37 Z TIG TPIj__
4-21
TRANSMIT TIG OF TPI TO CSM-
PRO F 06 58 HP DELTA VTPI DELTA VTRF
PRO F 06 81 DELTA VS-LV
KEY V9OE (OUT-OF-PLANE)
F 06 16 1 LOAD TIG TPI FROM DATA PAD (NOM 12502461 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT
PRO F 06 81 DELTA VS-LV
COPY CSM YDOT AND LOAD NEGATIVE IN R2 N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 59 DELTA VS LOS
N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI MGA
RESET ET
PRO F 37 BB
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (12000t600)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE)
-10
-6
4-22
F 50 16 DOWNLINK COMPLETE PRO (UPDATE COMPLETE)
400+3 AGS ALIGN 400R (00000 COMPLETE)
-9 277R COPY TGT LOS ANGLE
310+00800
303R THETA AT TPI 410+4 DIRECT TRANSFER AT ET=-8 404+0 405+0 406+0 (MONITOR 470 471 4721
373R TIG TPI
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
KEY 41E (RCS THRUSTING) F 50 18 FOAl ANGLES (REQUEST MNVRI
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
-5 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUS
400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
COMPUTE TPI BU
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
4-23
1685 DELTA VS-BODY
50OR DELTA VX(NOM -115)
502R DELTA VZ(NOM 229)
-Z35 OSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS-BODY
(1250246) BURN +Z
VERIFY AGS RESIDUALS 500R 501R 502R DELTAVX DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
MCC1
KEY V76E (PGNS PULSE) PGNSMODECONT-AUTO
KEY V93E (BEFORE 1ST MARK REINITW MATRIX)
+2 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
4-24
(LOS OF MSFN) S-BAND - SLEW TO P = 90 Y = 0 S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
404+0 405+0 406+0
(MONITOR 470 471 4721
+9 277R COPY TGT LOS ANGLE
+12 PRO (COMPUTE MCC FOR TPI+15I F 06 81 DELTA VS-LV
PRO F 06 59 DELTA VS-LOS
PRO F 16 45 MKS TFI MGA
+13 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUOS
COMPUTE MCC1 BU
PRO F 37 BB
+14 KEY 41E (RCS THRUSTING) F 50 18 FOAL ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+1425 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+15 F 16 85 NULL DELTA VS
PRO F 37 BB
MCC2
KEY V76E (PGNS PULSE)
4-25
PGNS MODE CONT-AUTO
KEY V93E (BEFORE 1ST MARK REINIT W MATRIX)
+16 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
404+0 405+0 406+0 (MONITOR 470 471 47)shy
+24 277R COPY TGT LOS ANGLE
+27 PRO (COMPUTE MCC FORTPI+30) F 06 81 DELTA VS-LV
PRO F 06 59 DELIA VPS-LOS
PRO F 16 45 MKS TFI MGA
+28 277R COPY TGT LOS ANGLE
COPY R RDOT FROM TAPEMETER FOR BUS
COMPUTE MCC2 BU
F 37 BB PRO
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+2925 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+30 F 16 85 NULL DELTA VS
PRO F 37 BB
KEY OOE (P001
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
4-26
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT KEY V34E (TERMINATE)
KEY V37E47E (AVE G) F 16 83 DELTA VIS
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT VERIFY TAPE METER WITH DSKY
BRAKING GATE 30 FPS - 6000 FT 20 FPS - 3000 FT 10 FPS - 1500 FT 5 FPS - 600 FT
RENDEZVOUS
STATION KEEPING
5-1
50 ABORT PROCEDURE
This is a specific AGS nominal abort procedure due to a PGNS failure between insertion and station keeping
51
5-2
Nominal AGS Procedures
ASSUMPTIONS
AFTER INSERTION
I INSERTION COMPLETE (RFSIDUALS NULLED) g PGNS FAILURE BEFORE INSERTION 3 RAUAR NOT LOCKED ON
(UI CoNT-AGS ATlI[uUE MON-AGS(CDR) RATE ERR MON-CNPTR(LMP) ATTITUDE MON-AGS(LMP) SHFITRUN-+5 DEG X-POINTER-HI MULT RADAR IEST Sw-OFF LNb GMbL-OFF ENG ARM-OFF X-IRANSL-2 JETS DEAD BAND-MAX PGNS MODE CONT-OFF THROTJET-JET CB IMU OIR-ON HH MOVE-AUTO rRACK TTCATNANSL-ENABLE(CDR)
AL CPL-ON MODE SL-AGS RNGAL1 MON-RNbRNGRT RAIE ERR MON-RNDZ HDR(CDR) AVl CoNT(3)-PULSE AGS MODE CONT-AUTO ACA4JET-DISABLE(CDR) TTCATRANSL-DISABLE(LMP) ACA4JET-DISABLE(LMP)
bO7+U Z-AXIS BOPESIGHT 400+2 Z-AXIS STEERING PULSE TO NULL AGS ERRORS POINT Z-AXIS IN DIRECTION OF CSM MODE CONT-ATT HOLD ATT CONT(3)-MODE CONTROL O unnr - ZirF
5-3
SLEW PATE - LO
SLEW RR ANT TO OqON FUAI VERIFY MAX SIGNAL STRENGTH RH MOOE-AUTO TRACK NO TRACK LIGHT OFF -
ATT CONT(3h-PULSE
CHECK INSERTION VELOCITY WITH TAPEMETER COMPARE EAPEMETER WITH AGS STATE VECTOR DATA I
17R RANGE(NOM 2642)
440R RANGE RATE(NOM -425l)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
cSI
+3 417+1 (RADAR FILTER INITIALIZED) 41b+l (NO BOHESIGHT) b03-XXXXX RANGE RATE
+5 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGF
41b+1 CSI ROUTINE 373+o2065 CSi TIME 275+03028 TPI TIME 605+0077 COTANGENT OF LOS TO CSM 41b+1 (ONE-HALF OFBITAL-PERIOD) 411+0 HCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT
610R TIME TO CST
43 RESET ET
267R VELOCITY TO BE GAINED CSI
402R FLTA H
371R DFLTA V CDH
5-4
372R DFLTA T CSICDH
-42 415+1 (No BORESIGHT) bO6-xXXXX RANGE RATE
-40 415+1 (NO BORESIGHT)503-XXXXX RANGE RATE dORESIGHT ON CSM
415+1 316+XXXXX RANGE
-37 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE
-15 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE UORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-2 415+1 (No BOHESIGHT) bO3-XXXXX RANGF RATE
i1uR TIME TO CS
RESEF ET
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-30 COPY ROOT FOR 1ST CSI 81J
BORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-t7 415+1 (NO BORFSIGHT) 50-XXxXx RANGF RATE
267R VELOCITY TO HE GAINED CSI
402R LELTA H
371R OFLTA V COH
372R OELTA T CSICDH
-5 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 blb+XXXXX RANGE
-i2 415+1 (No BORESIGHT) 5n3-XXXXX RANGE RATE
415+1 (NO BORESIGHT)
5-5
503-XXXXX RANGF RATE
COPY Roor FOR 2NO CSI BU
bORESIGHT ON CSM 415+1 316+XXXXX RANGE
TEMPPRESS MON SEL - FUEL MAN
A AND 8 PRESS 181 +-3 PIG TEMPPRESS MON SEL - PRPLNT
A AND B TEMP IND 4ODEG 0 IOODEG F A AND B PRFSS IND 181 +-3 PSIA
tEMPPRESS MON SEL - HEL
A AND 8 PRESS IND PSIA
A QUANTITY IND- -- PERCENT RFMAINING
8 QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4p 2 3 (120 - 190 DFG F)
415+1 (NO BORESIGHT)-17 503-XXXXX RANGE RATE
-15 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
(LOS OF MSFN) S-BAND - SLEW 10 P = +90t Y U S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
-12 415+1 (No 8ORESIGHT)
503-XXXXX RANGE RATE
267R VFLOCITY TU BE GAINED CSI
402R OFLTA H
372R TIME CSICH
371R PREDICTED VEL 10 RE GAINED COH
263R OLT-OF-PLANE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATL
-10 COPY RANGE AND ROOT FOR 3RD CSI 8U
SORESIGH ON CSM 41b+1
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
-7
4-10
F 06 81 DELTA VS-LV(CSI)
COPY YDOT FROM CSM AND LOAD NEGATIVE IN R2 CSIIN81I
DELTA VX(LV)
DELTA VYILV)
DELTA VZ(LV)
PRO F 06 82 DELTA VS-LV (COH)
CDH(82)
DELTA VX(LV)
- DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RANGE AND RDOT FOR 3RD CS BU
COMPUTE CSI BU
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (i2000OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
(TRANSMIT CSI DATA TO CSMI VHF A XMTR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF TELEMETY PCM - LO
KEY VB3E F 16 54 R ROOT THETA
SET ORDEAL PRO
317R RANGE
440R RANGE RATE
4-11
400+3 AGS ALIGN t40OR (00000 COMPLETE)
277R THETA
PRO F 37 BB
-6 KEY 41E (RCS THRUSTING) F 50 18 FDAI-ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTAV 400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTAV 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA RF
TRANSMIT TGT DELTA VS TO CSM AND SYNC COUNTDOWN
16 85 DELTA VS-BODY
502R DELTA VZ (NOM 5Ql)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTAVS-BODY
(123t26t27) BURN +Z
NULL DELTA VS
4-12
VERIFY AGS RESIDUALS 50OR 501R 502R DELTA VX _ DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
CDH
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
KEY V67E (RESET W MATRIX) F 06 99 +0200E +O0020E +00005E
PRO
507+0 Z-AXIS BORESIGHT
(VHF RANGING WITH CSM) VHF A XMTR - VOICERNG VHF B XMTR - OFF VHF B RCVR - ON TELEMETRY PCM - HI
(12331) KEY V37E33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 a TIG CDH (NOM 1242425) -120 amp00 10 (AGS 0 TIME)
(CONVERT TO MINUTES)
411+0 THRUST ALONG Z-BODY AXIS ENTER IF YOU DONT TARGET CSI
373R (NOM 26443 310R TIME TO CDH
4-13
423R DESIRED ALT RATE AT CDH
402R DELTA Hshy
450R DELTA VX
452R DELTA VZ
623+0 Z-AXIS PARALLEL TO CSM PLANE
IPRO F 16 45 MKS TFI -00001
-52 RESET ET
KEY V93E (REINIT W MATRIX WHEN MARKS =4)
KEY V32E (MARKS = 3)
F 06 75 DELTA HCDH DELTA TCDHTPI DELTA TTPI PRO
F 06 81 DELTA VCDH-LV CDH(N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
-47 KEY VSOE (OUT-OF-PLANE)
_ TIG CDH (NOM 124t24t25) -3000 TIME FROM CDH
F 06 16 l1 LOAD TIG PLANE CHANGE (NOM 123amp54-253 PRO
F 06 90 Y YDOT PSI N90 CSM
VYDOT PRO
-42 KEY V32E (MARKS=1O)
F 06 75 DELTA HCDH DELTA TCDIHTPI DELTA TTPITPI PRO
F 06 81 DELTA VCDH-LV
4-14
CDH (NS1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -OO1
KEY V34E (TERMINATE) F 37 B8
PLANE CHANGE
KEY 30E (EXTERNAL DELTA V)
TIG CDH (NOM 124124t25) -3000 TIME FROM CDH
F 06 33 LOAD TIG PLANE CHANGE (NOM 123154T25) PRO
F 06 81 DELTA VS-LV (NOM 00)
-36 COPY RDOT FOR 1ST CDH BU
KEY V90E (OUT-OF-PLANE)
F 06 16 1 1 LOAD TIG PLANE CHANGE (NOM 1231543251 PRO
F 06 90 Y YOOT PSI N90 CSM
YDOT
PRO
F 06 81 DELTA VS-LV(NOM 00)
COPY YDOT AND LOAD NEGATIVE IN R2 PRO
F 06 42 HA HP DELTA V PRO
F 16 45 MKS TFI MGA
PRO
F 37 BB
KEY 41E (RCS THRUSTING)
-30
4-15
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVRI
410+5 EXTERNAL DELTA V 450+0 451-YDOT 452+0 (LOAD CSM -YDOT)
407+0 ROTATE EXTERNAL DELTA V RF
16 95 DELTA VS-BODY
-3035 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATTVHOLD 407+1 FREEZE EXTERNAL DELTAV
F 16 85 DELTA VS-BODY -
NULL DELTA VIS
PRO F 37BB
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
507+0 Z-AXIS BORESIGHT
(12356) KEY 33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 TIG CDH (NOM 124t24t25) -120 OO ZOO (AGS 0 TIME)
(CONVERT TO MINUTES)
373R _ (NOM 2644) 310R TIME TO CDH
423R DESIRED ALT RATE AT CDH
(ADS OF MSFN) S-BAND - SLEW TOP = ACQUIRE HGA LOCK ON VOICE - BUVOICE -- VOICE VERIFY VOICE TLM BIOMED - LEFT (OR RIGHT)
402R DELTAH
4-16
F 16 45
-25
-23
F 06 75
F 06 81
F 16 45
-12
F 06 75
F 06 81
450R DELTA VX
452R DELTA VZ
PRO MKS TFI -00001
KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
COPY ROOT FOR 2ND CDH BU
KEY v32E (MARKS = 5)
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40DEG TO 1OODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + B PRESS IND PSIA
A QUANTITY IND _ PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING a TEMP MON SEL RCS QUAD 1 4 2 3 (120 - 190 DEG F)i
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
CDH(NB1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO MKS TFI -00001
PRO (FINAL COMP)
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
KEY V9OE (OUT-OF-PLANE)
-7
4-17
F 06 16 jj LOAD TIG CDH FROM DATA PAD (NOM 12424251 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT PRO
COPY YOOT FROM CSM AND LOAD NEGATIVE IN R2
CDH(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RDOT FOR 3RD CDH BU
COMPUTE CDH BU
TRANSMIT TGT DELTA VOS TO CSM AND SYNC COUNTDOWN
KEY V47E (INITIALIZE AGS F 06 16 GET OF AGS 0 TIME 120O00OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
KEY V83E F 16 54 R RDOT THETA
SET ORDEAL PRO
317R _ RANGE
440R RANGE RATE 400+3 AGS ALIGN 40OR (00000 COMPLETE)
277R THETA
-6
4-18
PRO F 3 BB
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY V06N86E F 06 86 DELTA VIS-LV
AGS(N86) CHART
DELTA VX(LVD
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
16 85 DELTA VS-BODY
50OR DELTA VX (NOM -0O3)
502R DELTA VZ (NOM 60)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD 407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS BODY
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS 5OOR 50IR 502R DELTA VX -DELTA VY DELTA VZ-
VERIFY PGNS RESIDUALS N85
DELTA VX(LM)
4-19
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
TPI
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO 507+0 Z-AXIS BORESIGHT
(12426) KEY 34E (TPI)
-36 RESET ET
F 06 37 - amp LOAD TIG TPI FROM DATA PAD (NOM 1250246) PRO
F 06 55 +00000 +02660E +13000 OMEGAT PRO
F 16 45 MARKS TFI -00001
-32 KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
-29 KEY V32E (MARKS = 3)
F 06 37 __ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
RESET ET
410+3 TPI SEARCH ROUTINE 307+04300 DELTA T TRANSFER
4-20
-26 310+02600 TFI TPI
303R THETA AT TPI
267R DELTA VTPI
371R DELTA VTPI + DELTA VTPF
KEY V32E (MARKS = 10)
F 06 37 _ _ _ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VIS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
TEMPIPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40ODEG TO IGODEG F A + B PRESS IND 181 +-3 PSIA
TEMPIPRESS MON SEL - HEL
A + B PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD I 4 2 3 (120 - 190 DEG F)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
RESET ET
-13 310+01300 TFI TPI
303R THETA AT TPI
-12 PRO (FINAL COMP) F 06 37 Z TIG TPIj__
4-21
TRANSMIT TIG OF TPI TO CSM-
PRO F 06 58 HP DELTA VTPI DELTA VTRF
PRO F 06 81 DELTA VS-LV
KEY V9OE (OUT-OF-PLANE)
F 06 16 1 LOAD TIG TPI FROM DATA PAD (NOM 12502461 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT
PRO F 06 81 DELTA VS-LV
COPY CSM YDOT AND LOAD NEGATIVE IN R2 N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 59 DELTA VS LOS
N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI MGA
RESET ET
PRO F 37 BB
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (12000t600)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE)
-10
-6
4-22
F 50 16 DOWNLINK COMPLETE PRO (UPDATE COMPLETE)
400+3 AGS ALIGN 400R (00000 COMPLETE)
-9 277R COPY TGT LOS ANGLE
310+00800
303R THETA AT TPI 410+4 DIRECT TRANSFER AT ET=-8 404+0 405+0 406+0 (MONITOR 470 471 4721
373R TIG TPI
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
KEY 41E (RCS THRUSTING) F 50 18 FOAl ANGLES (REQUEST MNVRI
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
-5 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUS
400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
COMPUTE TPI BU
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
4-23
1685 DELTA VS-BODY
50OR DELTA VX(NOM -115)
502R DELTA VZ(NOM 229)
-Z35 OSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS-BODY
(1250246) BURN +Z
VERIFY AGS RESIDUALS 500R 501R 502R DELTAVX DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
MCC1
KEY V76E (PGNS PULSE) PGNSMODECONT-AUTO
KEY V93E (BEFORE 1ST MARK REINITW MATRIX)
+2 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
4-24
(LOS OF MSFN) S-BAND - SLEW TO P = 90 Y = 0 S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
404+0 405+0 406+0
(MONITOR 470 471 4721
+9 277R COPY TGT LOS ANGLE
+12 PRO (COMPUTE MCC FOR TPI+15I F 06 81 DELTA VS-LV
PRO F 06 59 DELTA VS-LOS
PRO F 16 45 MKS TFI MGA
+13 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUOS
COMPUTE MCC1 BU
PRO F 37 BB
+14 KEY 41E (RCS THRUSTING) F 50 18 FOAL ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+1425 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+15 F 16 85 NULL DELTA VS
PRO F 37 BB
MCC2
KEY V76E (PGNS PULSE)
4-25
PGNS MODE CONT-AUTO
KEY V93E (BEFORE 1ST MARK REINIT W MATRIX)
+16 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
404+0 405+0 406+0 (MONITOR 470 471 47)shy
+24 277R COPY TGT LOS ANGLE
+27 PRO (COMPUTE MCC FORTPI+30) F 06 81 DELTA VS-LV
PRO F 06 59 DELIA VPS-LOS
PRO F 16 45 MKS TFI MGA
+28 277R COPY TGT LOS ANGLE
COPY R RDOT FROM TAPEMETER FOR BUS
COMPUTE MCC2 BU
F 37 BB PRO
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+2925 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+30 F 16 85 NULL DELTA VS
PRO F 37 BB
KEY OOE (P001
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
4-26
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT KEY V34E (TERMINATE)
KEY V37E47E (AVE G) F 16 83 DELTA VIS
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT VERIFY TAPE METER WITH DSKY
BRAKING GATE 30 FPS - 6000 FT 20 FPS - 3000 FT 10 FPS - 1500 FT 5 FPS - 600 FT
RENDEZVOUS
STATION KEEPING
5-1
50 ABORT PROCEDURE
This is a specific AGS nominal abort procedure due to a PGNS failure between insertion and station keeping
51
5-2
Nominal AGS Procedures
ASSUMPTIONS
AFTER INSERTION
I INSERTION COMPLETE (RFSIDUALS NULLED) g PGNS FAILURE BEFORE INSERTION 3 RAUAR NOT LOCKED ON
(UI CoNT-AGS ATlI[uUE MON-AGS(CDR) RATE ERR MON-CNPTR(LMP) ATTITUDE MON-AGS(LMP) SHFITRUN-+5 DEG X-POINTER-HI MULT RADAR IEST Sw-OFF LNb GMbL-OFF ENG ARM-OFF X-IRANSL-2 JETS DEAD BAND-MAX PGNS MODE CONT-OFF THROTJET-JET CB IMU OIR-ON HH MOVE-AUTO rRACK TTCATNANSL-ENABLE(CDR)
AL CPL-ON MODE SL-AGS RNGAL1 MON-RNbRNGRT RAIE ERR MON-RNDZ HDR(CDR) AVl CoNT(3)-PULSE AGS MODE CONT-AUTO ACA4JET-DISABLE(CDR) TTCATRANSL-DISABLE(LMP) ACA4JET-DISABLE(LMP)
bO7+U Z-AXIS BOPESIGHT 400+2 Z-AXIS STEERING PULSE TO NULL AGS ERRORS POINT Z-AXIS IN DIRECTION OF CSM MODE CONT-ATT HOLD ATT CONT(3)-MODE CONTROL O unnr - ZirF
5-3
SLEW PATE - LO
SLEW RR ANT TO OqON FUAI VERIFY MAX SIGNAL STRENGTH RH MOOE-AUTO TRACK NO TRACK LIGHT OFF -
ATT CONT(3h-PULSE
CHECK INSERTION VELOCITY WITH TAPEMETER COMPARE EAPEMETER WITH AGS STATE VECTOR DATA I
17R RANGE(NOM 2642)
440R RANGE RATE(NOM -425l)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
cSI
+3 417+1 (RADAR FILTER INITIALIZED) 41b+l (NO BOHESIGHT) b03-XXXXX RANGE RATE
+5 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGF
41b+1 CSI ROUTINE 373+o2065 CSi TIME 275+03028 TPI TIME 605+0077 COTANGENT OF LOS TO CSM 41b+1 (ONE-HALF OFBITAL-PERIOD) 411+0 HCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT
610R TIME TO CST
43 RESET ET
267R VELOCITY TO BE GAINED CSI
402R FLTA H
371R DFLTA V CDH
5-4
372R DFLTA T CSICDH
-42 415+1 (No BORESIGHT) bO6-xXXXX RANGE RATE
-40 415+1 (NO BORESIGHT)503-XXXXX RANGE RATE dORESIGHT ON CSM
415+1 316+XXXXX RANGE
-37 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE
-15 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE UORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-2 415+1 (No BOHESIGHT) bO3-XXXXX RANGF RATE
i1uR TIME TO CS
RESEF ET
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-30 COPY ROOT FOR 1ST CSI 81J
BORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-t7 415+1 (NO BORFSIGHT) 50-XXxXx RANGF RATE
267R VELOCITY TO HE GAINED CSI
402R LELTA H
371R OFLTA V COH
372R OELTA T CSICDH
-5 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 blb+XXXXX RANGE
-i2 415+1 (No BORESIGHT) 5n3-XXXXX RANGE RATE
415+1 (NO BORESIGHT)
5-5
503-XXXXX RANGF RATE
COPY Roor FOR 2NO CSI BU
bORESIGHT ON CSM 415+1 316+XXXXX RANGE
TEMPPRESS MON SEL - FUEL MAN
A AND 8 PRESS 181 +-3 PIG TEMPPRESS MON SEL - PRPLNT
A AND B TEMP IND 4ODEG 0 IOODEG F A AND B PRFSS IND 181 +-3 PSIA
tEMPPRESS MON SEL - HEL
A AND 8 PRESS IND PSIA
A QUANTITY IND- -- PERCENT RFMAINING
8 QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4p 2 3 (120 - 190 DFG F)
415+1 (NO BORESIGHT)-17 503-XXXXX RANGE RATE
-15 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
(LOS OF MSFN) S-BAND - SLEW 10 P = +90t Y U S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
-12 415+1 (No 8ORESIGHT)
503-XXXXX RANGE RATE
267R VFLOCITY TU BE GAINED CSI
402R OFLTA H
372R TIME CSICH
371R PREDICTED VEL 10 RE GAINED COH
263R OLT-OF-PLANE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATL
-10 COPY RANGE AND ROOT FOR 3RD CSI 8U
SORESIGH ON CSM 41b+1
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
4-11
400+3 AGS ALIGN t40OR (00000 COMPLETE)
277R THETA
PRO F 37 BB
-6 KEY 41E (RCS THRUSTING) F 50 18 FDAI-ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTAV 400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTAV 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA RF
TRANSMIT TGT DELTA VS TO CSM AND SYNC COUNTDOWN
16 85 DELTA VS-BODY
502R DELTA VZ (NOM 5Ql)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTAVS-BODY
(123t26t27) BURN +Z
NULL DELTA VS
4-12
VERIFY AGS RESIDUALS 50OR 501R 502R DELTA VX _ DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
CDH
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
KEY V67E (RESET W MATRIX) F 06 99 +0200E +O0020E +00005E
PRO
507+0 Z-AXIS BORESIGHT
(VHF RANGING WITH CSM) VHF A XMTR - VOICERNG VHF B XMTR - OFF VHF B RCVR - ON TELEMETRY PCM - HI
(12331) KEY V37E33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 a TIG CDH (NOM 1242425) -120 amp00 10 (AGS 0 TIME)
(CONVERT TO MINUTES)
411+0 THRUST ALONG Z-BODY AXIS ENTER IF YOU DONT TARGET CSI
373R (NOM 26443 310R TIME TO CDH
4-13
423R DESIRED ALT RATE AT CDH
402R DELTA Hshy
450R DELTA VX
452R DELTA VZ
623+0 Z-AXIS PARALLEL TO CSM PLANE
IPRO F 16 45 MKS TFI -00001
-52 RESET ET
KEY V93E (REINIT W MATRIX WHEN MARKS =4)
KEY V32E (MARKS = 3)
F 06 75 DELTA HCDH DELTA TCDHTPI DELTA TTPI PRO
F 06 81 DELTA VCDH-LV CDH(N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
-47 KEY VSOE (OUT-OF-PLANE)
_ TIG CDH (NOM 124t24t25) -3000 TIME FROM CDH
F 06 16 l1 LOAD TIG PLANE CHANGE (NOM 123amp54-253 PRO
F 06 90 Y YDOT PSI N90 CSM
VYDOT PRO
-42 KEY V32E (MARKS=1O)
F 06 75 DELTA HCDH DELTA TCDIHTPI DELTA TTPITPI PRO
F 06 81 DELTA VCDH-LV
4-14
CDH (NS1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -OO1
KEY V34E (TERMINATE) F 37 B8
PLANE CHANGE
KEY 30E (EXTERNAL DELTA V)
TIG CDH (NOM 124124t25) -3000 TIME FROM CDH
F 06 33 LOAD TIG PLANE CHANGE (NOM 123154T25) PRO
F 06 81 DELTA VS-LV (NOM 00)
-36 COPY RDOT FOR 1ST CDH BU
KEY V90E (OUT-OF-PLANE)
F 06 16 1 1 LOAD TIG PLANE CHANGE (NOM 1231543251 PRO
F 06 90 Y YOOT PSI N90 CSM
YDOT
PRO
F 06 81 DELTA VS-LV(NOM 00)
COPY YDOT AND LOAD NEGATIVE IN R2 PRO
F 06 42 HA HP DELTA V PRO
F 16 45 MKS TFI MGA
PRO
F 37 BB
KEY 41E (RCS THRUSTING)
-30
4-15
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVRI
410+5 EXTERNAL DELTA V 450+0 451-YDOT 452+0 (LOAD CSM -YDOT)
407+0 ROTATE EXTERNAL DELTA V RF
16 95 DELTA VS-BODY
-3035 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATTVHOLD 407+1 FREEZE EXTERNAL DELTAV
F 16 85 DELTA VS-BODY -
NULL DELTA VIS
PRO F 37BB
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
507+0 Z-AXIS BORESIGHT
(12356) KEY 33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 TIG CDH (NOM 124t24t25) -120 OO ZOO (AGS 0 TIME)
(CONVERT TO MINUTES)
373R _ (NOM 2644) 310R TIME TO CDH
423R DESIRED ALT RATE AT CDH
(ADS OF MSFN) S-BAND - SLEW TOP = ACQUIRE HGA LOCK ON VOICE - BUVOICE -- VOICE VERIFY VOICE TLM BIOMED - LEFT (OR RIGHT)
402R DELTAH
4-16
F 16 45
-25
-23
F 06 75
F 06 81
F 16 45
-12
F 06 75
F 06 81
450R DELTA VX
452R DELTA VZ
PRO MKS TFI -00001
KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
COPY ROOT FOR 2ND CDH BU
KEY v32E (MARKS = 5)
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40DEG TO 1OODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + B PRESS IND PSIA
A QUANTITY IND _ PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING a TEMP MON SEL RCS QUAD 1 4 2 3 (120 - 190 DEG F)i
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
CDH(NB1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO MKS TFI -00001
PRO (FINAL COMP)
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
KEY V9OE (OUT-OF-PLANE)
-7
4-17
F 06 16 jj LOAD TIG CDH FROM DATA PAD (NOM 12424251 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT PRO
COPY YOOT FROM CSM AND LOAD NEGATIVE IN R2
CDH(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RDOT FOR 3RD CDH BU
COMPUTE CDH BU
TRANSMIT TGT DELTA VOS TO CSM AND SYNC COUNTDOWN
KEY V47E (INITIALIZE AGS F 06 16 GET OF AGS 0 TIME 120O00OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
KEY V83E F 16 54 R RDOT THETA
SET ORDEAL PRO
317R _ RANGE
440R RANGE RATE 400+3 AGS ALIGN 40OR (00000 COMPLETE)
277R THETA
-6
4-18
PRO F 3 BB
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY V06N86E F 06 86 DELTA VIS-LV
AGS(N86) CHART
DELTA VX(LVD
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
16 85 DELTA VS-BODY
50OR DELTA VX (NOM -0O3)
502R DELTA VZ (NOM 60)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD 407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS BODY
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS 5OOR 50IR 502R DELTA VX -DELTA VY DELTA VZ-
VERIFY PGNS RESIDUALS N85
DELTA VX(LM)
4-19
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
TPI
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO 507+0 Z-AXIS BORESIGHT
(12426) KEY 34E (TPI)
-36 RESET ET
F 06 37 - amp LOAD TIG TPI FROM DATA PAD (NOM 1250246) PRO
F 06 55 +00000 +02660E +13000 OMEGAT PRO
F 16 45 MARKS TFI -00001
-32 KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
-29 KEY V32E (MARKS = 3)
F 06 37 __ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
RESET ET
410+3 TPI SEARCH ROUTINE 307+04300 DELTA T TRANSFER
4-20
-26 310+02600 TFI TPI
303R THETA AT TPI
267R DELTA VTPI
371R DELTA VTPI + DELTA VTPF
KEY V32E (MARKS = 10)
F 06 37 _ _ _ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VIS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
TEMPIPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40ODEG TO IGODEG F A + B PRESS IND 181 +-3 PSIA
TEMPIPRESS MON SEL - HEL
A + B PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD I 4 2 3 (120 - 190 DEG F)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
RESET ET
-13 310+01300 TFI TPI
303R THETA AT TPI
-12 PRO (FINAL COMP) F 06 37 Z TIG TPIj__
4-21
TRANSMIT TIG OF TPI TO CSM-
PRO F 06 58 HP DELTA VTPI DELTA VTRF
PRO F 06 81 DELTA VS-LV
KEY V9OE (OUT-OF-PLANE)
F 06 16 1 LOAD TIG TPI FROM DATA PAD (NOM 12502461 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT
PRO F 06 81 DELTA VS-LV
COPY CSM YDOT AND LOAD NEGATIVE IN R2 N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 59 DELTA VS LOS
N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI MGA
RESET ET
PRO F 37 BB
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (12000t600)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE)
-10
-6
4-22
F 50 16 DOWNLINK COMPLETE PRO (UPDATE COMPLETE)
400+3 AGS ALIGN 400R (00000 COMPLETE)
-9 277R COPY TGT LOS ANGLE
310+00800
303R THETA AT TPI 410+4 DIRECT TRANSFER AT ET=-8 404+0 405+0 406+0 (MONITOR 470 471 4721
373R TIG TPI
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
KEY 41E (RCS THRUSTING) F 50 18 FOAl ANGLES (REQUEST MNVRI
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
-5 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUS
400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
COMPUTE TPI BU
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
4-23
1685 DELTA VS-BODY
50OR DELTA VX(NOM -115)
502R DELTA VZ(NOM 229)
-Z35 OSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS-BODY
(1250246) BURN +Z
VERIFY AGS RESIDUALS 500R 501R 502R DELTAVX DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
MCC1
KEY V76E (PGNS PULSE) PGNSMODECONT-AUTO
KEY V93E (BEFORE 1ST MARK REINITW MATRIX)
+2 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
4-24
(LOS OF MSFN) S-BAND - SLEW TO P = 90 Y = 0 S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
404+0 405+0 406+0
(MONITOR 470 471 4721
+9 277R COPY TGT LOS ANGLE
+12 PRO (COMPUTE MCC FOR TPI+15I F 06 81 DELTA VS-LV
PRO F 06 59 DELTA VS-LOS
PRO F 16 45 MKS TFI MGA
+13 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUOS
COMPUTE MCC1 BU
PRO F 37 BB
+14 KEY 41E (RCS THRUSTING) F 50 18 FOAL ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+1425 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+15 F 16 85 NULL DELTA VS
PRO F 37 BB
MCC2
KEY V76E (PGNS PULSE)
4-25
PGNS MODE CONT-AUTO
KEY V93E (BEFORE 1ST MARK REINIT W MATRIX)
+16 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
404+0 405+0 406+0 (MONITOR 470 471 47)shy
+24 277R COPY TGT LOS ANGLE
+27 PRO (COMPUTE MCC FORTPI+30) F 06 81 DELTA VS-LV
PRO F 06 59 DELIA VPS-LOS
PRO F 16 45 MKS TFI MGA
+28 277R COPY TGT LOS ANGLE
COPY R RDOT FROM TAPEMETER FOR BUS
COMPUTE MCC2 BU
F 37 BB PRO
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+2925 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+30 F 16 85 NULL DELTA VS
PRO F 37 BB
KEY OOE (P001
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
4-26
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT KEY V34E (TERMINATE)
KEY V37E47E (AVE G) F 16 83 DELTA VIS
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT VERIFY TAPE METER WITH DSKY
BRAKING GATE 30 FPS - 6000 FT 20 FPS - 3000 FT 10 FPS - 1500 FT 5 FPS - 600 FT
RENDEZVOUS
STATION KEEPING
5-1
50 ABORT PROCEDURE
This is a specific AGS nominal abort procedure due to a PGNS failure between insertion and station keeping
51
5-2
Nominal AGS Procedures
ASSUMPTIONS
AFTER INSERTION
I INSERTION COMPLETE (RFSIDUALS NULLED) g PGNS FAILURE BEFORE INSERTION 3 RAUAR NOT LOCKED ON
(UI CoNT-AGS ATlI[uUE MON-AGS(CDR) RATE ERR MON-CNPTR(LMP) ATTITUDE MON-AGS(LMP) SHFITRUN-+5 DEG X-POINTER-HI MULT RADAR IEST Sw-OFF LNb GMbL-OFF ENG ARM-OFF X-IRANSL-2 JETS DEAD BAND-MAX PGNS MODE CONT-OFF THROTJET-JET CB IMU OIR-ON HH MOVE-AUTO rRACK TTCATNANSL-ENABLE(CDR)
AL CPL-ON MODE SL-AGS RNGAL1 MON-RNbRNGRT RAIE ERR MON-RNDZ HDR(CDR) AVl CoNT(3)-PULSE AGS MODE CONT-AUTO ACA4JET-DISABLE(CDR) TTCATRANSL-DISABLE(LMP) ACA4JET-DISABLE(LMP)
bO7+U Z-AXIS BOPESIGHT 400+2 Z-AXIS STEERING PULSE TO NULL AGS ERRORS POINT Z-AXIS IN DIRECTION OF CSM MODE CONT-ATT HOLD ATT CONT(3)-MODE CONTROL O unnr - ZirF
5-3
SLEW PATE - LO
SLEW RR ANT TO OqON FUAI VERIFY MAX SIGNAL STRENGTH RH MOOE-AUTO TRACK NO TRACK LIGHT OFF -
ATT CONT(3h-PULSE
CHECK INSERTION VELOCITY WITH TAPEMETER COMPARE EAPEMETER WITH AGS STATE VECTOR DATA I
17R RANGE(NOM 2642)
440R RANGE RATE(NOM -425l)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
cSI
+3 417+1 (RADAR FILTER INITIALIZED) 41b+l (NO BOHESIGHT) b03-XXXXX RANGE RATE
+5 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGF
41b+1 CSI ROUTINE 373+o2065 CSi TIME 275+03028 TPI TIME 605+0077 COTANGENT OF LOS TO CSM 41b+1 (ONE-HALF OFBITAL-PERIOD) 411+0 HCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT
610R TIME TO CST
43 RESET ET
267R VELOCITY TO BE GAINED CSI
402R FLTA H
371R DFLTA V CDH
5-4
372R DFLTA T CSICDH
-42 415+1 (No BORESIGHT) bO6-xXXXX RANGE RATE
-40 415+1 (NO BORESIGHT)503-XXXXX RANGE RATE dORESIGHT ON CSM
415+1 316+XXXXX RANGE
-37 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE
-15 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE UORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-2 415+1 (No BOHESIGHT) bO3-XXXXX RANGF RATE
i1uR TIME TO CS
RESEF ET
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-30 COPY ROOT FOR 1ST CSI 81J
BORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-t7 415+1 (NO BORFSIGHT) 50-XXxXx RANGF RATE
267R VELOCITY TO HE GAINED CSI
402R LELTA H
371R OFLTA V COH
372R OELTA T CSICDH
-5 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 blb+XXXXX RANGE
-i2 415+1 (No BORESIGHT) 5n3-XXXXX RANGE RATE
415+1 (NO BORESIGHT)
5-5
503-XXXXX RANGF RATE
COPY Roor FOR 2NO CSI BU
bORESIGHT ON CSM 415+1 316+XXXXX RANGE
TEMPPRESS MON SEL - FUEL MAN
A AND 8 PRESS 181 +-3 PIG TEMPPRESS MON SEL - PRPLNT
A AND B TEMP IND 4ODEG 0 IOODEG F A AND B PRFSS IND 181 +-3 PSIA
tEMPPRESS MON SEL - HEL
A AND 8 PRESS IND PSIA
A QUANTITY IND- -- PERCENT RFMAINING
8 QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4p 2 3 (120 - 190 DFG F)
415+1 (NO BORESIGHT)-17 503-XXXXX RANGE RATE
-15 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
(LOS OF MSFN) S-BAND - SLEW 10 P = +90t Y U S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
-12 415+1 (No 8ORESIGHT)
503-XXXXX RANGE RATE
267R VFLOCITY TU BE GAINED CSI
402R OFLTA H
372R TIME CSICH
371R PREDICTED VEL 10 RE GAINED COH
263R OLT-OF-PLANE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATL
-10 COPY RANGE AND ROOT FOR 3RD CSI 8U
SORESIGH ON CSM 41b+1
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
4-12
VERIFY AGS RESIDUALS 50OR 501R 502R DELTA VX _ DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
CDH
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
KEY V67E (RESET W MATRIX) F 06 99 +0200E +O0020E +00005E
PRO
507+0 Z-AXIS BORESIGHT
(VHF RANGING WITH CSM) VHF A XMTR - VOICERNG VHF B XMTR - OFF VHF B RCVR - ON TELEMETRY PCM - HI
(12331) KEY V37E33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 a TIG CDH (NOM 1242425) -120 amp00 10 (AGS 0 TIME)
(CONVERT TO MINUTES)
411+0 THRUST ALONG Z-BODY AXIS ENTER IF YOU DONT TARGET CSI
373R (NOM 26443 310R TIME TO CDH
4-13
423R DESIRED ALT RATE AT CDH
402R DELTA Hshy
450R DELTA VX
452R DELTA VZ
623+0 Z-AXIS PARALLEL TO CSM PLANE
IPRO F 16 45 MKS TFI -00001
-52 RESET ET
KEY V93E (REINIT W MATRIX WHEN MARKS =4)
KEY V32E (MARKS = 3)
F 06 75 DELTA HCDH DELTA TCDHTPI DELTA TTPI PRO
F 06 81 DELTA VCDH-LV CDH(N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
-47 KEY VSOE (OUT-OF-PLANE)
_ TIG CDH (NOM 124t24t25) -3000 TIME FROM CDH
F 06 16 l1 LOAD TIG PLANE CHANGE (NOM 123amp54-253 PRO
F 06 90 Y YDOT PSI N90 CSM
VYDOT PRO
-42 KEY V32E (MARKS=1O)
F 06 75 DELTA HCDH DELTA TCDIHTPI DELTA TTPITPI PRO
F 06 81 DELTA VCDH-LV
4-14
CDH (NS1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -OO1
KEY V34E (TERMINATE) F 37 B8
PLANE CHANGE
KEY 30E (EXTERNAL DELTA V)
TIG CDH (NOM 124124t25) -3000 TIME FROM CDH
F 06 33 LOAD TIG PLANE CHANGE (NOM 123154T25) PRO
F 06 81 DELTA VS-LV (NOM 00)
-36 COPY RDOT FOR 1ST CDH BU
KEY V90E (OUT-OF-PLANE)
F 06 16 1 1 LOAD TIG PLANE CHANGE (NOM 1231543251 PRO
F 06 90 Y YOOT PSI N90 CSM
YDOT
PRO
F 06 81 DELTA VS-LV(NOM 00)
COPY YDOT AND LOAD NEGATIVE IN R2 PRO
F 06 42 HA HP DELTA V PRO
F 16 45 MKS TFI MGA
PRO
F 37 BB
KEY 41E (RCS THRUSTING)
-30
4-15
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVRI
410+5 EXTERNAL DELTA V 450+0 451-YDOT 452+0 (LOAD CSM -YDOT)
407+0 ROTATE EXTERNAL DELTA V RF
16 95 DELTA VS-BODY
-3035 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATTVHOLD 407+1 FREEZE EXTERNAL DELTAV
F 16 85 DELTA VS-BODY -
NULL DELTA VIS
PRO F 37BB
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
507+0 Z-AXIS BORESIGHT
(12356) KEY 33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 TIG CDH (NOM 124t24t25) -120 OO ZOO (AGS 0 TIME)
(CONVERT TO MINUTES)
373R _ (NOM 2644) 310R TIME TO CDH
423R DESIRED ALT RATE AT CDH
(ADS OF MSFN) S-BAND - SLEW TOP = ACQUIRE HGA LOCK ON VOICE - BUVOICE -- VOICE VERIFY VOICE TLM BIOMED - LEFT (OR RIGHT)
402R DELTAH
4-16
F 16 45
-25
-23
F 06 75
F 06 81
F 16 45
-12
F 06 75
F 06 81
450R DELTA VX
452R DELTA VZ
PRO MKS TFI -00001
KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
COPY ROOT FOR 2ND CDH BU
KEY v32E (MARKS = 5)
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40DEG TO 1OODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + B PRESS IND PSIA
A QUANTITY IND _ PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING a TEMP MON SEL RCS QUAD 1 4 2 3 (120 - 190 DEG F)i
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
CDH(NB1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO MKS TFI -00001
PRO (FINAL COMP)
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
KEY V9OE (OUT-OF-PLANE)
-7
4-17
F 06 16 jj LOAD TIG CDH FROM DATA PAD (NOM 12424251 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT PRO
COPY YOOT FROM CSM AND LOAD NEGATIVE IN R2
CDH(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RDOT FOR 3RD CDH BU
COMPUTE CDH BU
TRANSMIT TGT DELTA VOS TO CSM AND SYNC COUNTDOWN
KEY V47E (INITIALIZE AGS F 06 16 GET OF AGS 0 TIME 120O00OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
KEY V83E F 16 54 R RDOT THETA
SET ORDEAL PRO
317R _ RANGE
440R RANGE RATE 400+3 AGS ALIGN 40OR (00000 COMPLETE)
277R THETA
-6
4-18
PRO F 3 BB
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY V06N86E F 06 86 DELTA VIS-LV
AGS(N86) CHART
DELTA VX(LVD
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
16 85 DELTA VS-BODY
50OR DELTA VX (NOM -0O3)
502R DELTA VZ (NOM 60)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD 407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS BODY
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS 5OOR 50IR 502R DELTA VX -DELTA VY DELTA VZ-
VERIFY PGNS RESIDUALS N85
DELTA VX(LM)
4-19
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
TPI
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO 507+0 Z-AXIS BORESIGHT
(12426) KEY 34E (TPI)
-36 RESET ET
F 06 37 - amp LOAD TIG TPI FROM DATA PAD (NOM 1250246) PRO
F 06 55 +00000 +02660E +13000 OMEGAT PRO
F 16 45 MARKS TFI -00001
-32 KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
-29 KEY V32E (MARKS = 3)
F 06 37 __ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
RESET ET
410+3 TPI SEARCH ROUTINE 307+04300 DELTA T TRANSFER
4-20
-26 310+02600 TFI TPI
303R THETA AT TPI
267R DELTA VTPI
371R DELTA VTPI + DELTA VTPF
KEY V32E (MARKS = 10)
F 06 37 _ _ _ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VIS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
TEMPIPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40ODEG TO IGODEG F A + B PRESS IND 181 +-3 PSIA
TEMPIPRESS MON SEL - HEL
A + B PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD I 4 2 3 (120 - 190 DEG F)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
RESET ET
-13 310+01300 TFI TPI
303R THETA AT TPI
-12 PRO (FINAL COMP) F 06 37 Z TIG TPIj__
4-21
TRANSMIT TIG OF TPI TO CSM-
PRO F 06 58 HP DELTA VTPI DELTA VTRF
PRO F 06 81 DELTA VS-LV
KEY V9OE (OUT-OF-PLANE)
F 06 16 1 LOAD TIG TPI FROM DATA PAD (NOM 12502461 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT
PRO F 06 81 DELTA VS-LV
COPY CSM YDOT AND LOAD NEGATIVE IN R2 N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 59 DELTA VS LOS
N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI MGA
RESET ET
PRO F 37 BB
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (12000t600)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE)
-10
-6
4-22
F 50 16 DOWNLINK COMPLETE PRO (UPDATE COMPLETE)
400+3 AGS ALIGN 400R (00000 COMPLETE)
-9 277R COPY TGT LOS ANGLE
310+00800
303R THETA AT TPI 410+4 DIRECT TRANSFER AT ET=-8 404+0 405+0 406+0 (MONITOR 470 471 4721
373R TIG TPI
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
KEY 41E (RCS THRUSTING) F 50 18 FOAl ANGLES (REQUEST MNVRI
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
-5 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUS
400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
COMPUTE TPI BU
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
4-23
1685 DELTA VS-BODY
50OR DELTA VX(NOM -115)
502R DELTA VZ(NOM 229)
-Z35 OSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS-BODY
(1250246) BURN +Z
VERIFY AGS RESIDUALS 500R 501R 502R DELTAVX DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
MCC1
KEY V76E (PGNS PULSE) PGNSMODECONT-AUTO
KEY V93E (BEFORE 1ST MARK REINITW MATRIX)
+2 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
4-24
(LOS OF MSFN) S-BAND - SLEW TO P = 90 Y = 0 S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
404+0 405+0 406+0
(MONITOR 470 471 4721
+9 277R COPY TGT LOS ANGLE
+12 PRO (COMPUTE MCC FOR TPI+15I F 06 81 DELTA VS-LV
PRO F 06 59 DELTA VS-LOS
PRO F 16 45 MKS TFI MGA
+13 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUOS
COMPUTE MCC1 BU
PRO F 37 BB
+14 KEY 41E (RCS THRUSTING) F 50 18 FOAL ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+1425 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+15 F 16 85 NULL DELTA VS
PRO F 37 BB
MCC2
KEY V76E (PGNS PULSE)
4-25
PGNS MODE CONT-AUTO
KEY V93E (BEFORE 1ST MARK REINIT W MATRIX)
+16 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
404+0 405+0 406+0 (MONITOR 470 471 47)shy
+24 277R COPY TGT LOS ANGLE
+27 PRO (COMPUTE MCC FORTPI+30) F 06 81 DELTA VS-LV
PRO F 06 59 DELIA VPS-LOS
PRO F 16 45 MKS TFI MGA
+28 277R COPY TGT LOS ANGLE
COPY R RDOT FROM TAPEMETER FOR BUS
COMPUTE MCC2 BU
F 37 BB PRO
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+2925 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+30 F 16 85 NULL DELTA VS
PRO F 37 BB
KEY OOE (P001
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
4-26
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT KEY V34E (TERMINATE)
KEY V37E47E (AVE G) F 16 83 DELTA VIS
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT VERIFY TAPE METER WITH DSKY
BRAKING GATE 30 FPS - 6000 FT 20 FPS - 3000 FT 10 FPS - 1500 FT 5 FPS - 600 FT
RENDEZVOUS
STATION KEEPING
5-1
50 ABORT PROCEDURE
This is a specific AGS nominal abort procedure due to a PGNS failure between insertion and station keeping
51
5-2
Nominal AGS Procedures
ASSUMPTIONS
AFTER INSERTION
I INSERTION COMPLETE (RFSIDUALS NULLED) g PGNS FAILURE BEFORE INSERTION 3 RAUAR NOT LOCKED ON
(UI CoNT-AGS ATlI[uUE MON-AGS(CDR) RATE ERR MON-CNPTR(LMP) ATTITUDE MON-AGS(LMP) SHFITRUN-+5 DEG X-POINTER-HI MULT RADAR IEST Sw-OFF LNb GMbL-OFF ENG ARM-OFF X-IRANSL-2 JETS DEAD BAND-MAX PGNS MODE CONT-OFF THROTJET-JET CB IMU OIR-ON HH MOVE-AUTO rRACK TTCATNANSL-ENABLE(CDR)
AL CPL-ON MODE SL-AGS RNGAL1 MON-RNbRNGRT RAIE ERR MON-RNDZ HDR(CDR) AVl CoNT(3)-PULSE AGS MODE CONT-AUTO ACA4JET-DISABLE(CDR) TTCATRANSL-DISABLE(LMP) ACA4JET-DISABLE(LMP)
bO7+U Z-AXIS BOPESIGHT 400+2 Z-AXIS STEERING PULSE TO NULL AGS ERRORS POINT Z-AXIS IN DIRECTION OF CSM MODE CONT-ATT HOLD ATT CONT(3)-MODE CONTROL O unnr - ZirF
5-3
SLEW PATE - LO
SLEW RR ANT TO OqON FUAI VERIFY MAX SIGNAL STRENGTH RH MOOE-AUTO TRACK NO TRACK LIGHT OFF -
ATT CONT(3h-PULSE
CHECK INSERTION VELOCITY WITH TAPEMETER COMPARE EAPEMETER WITH AGS STATE VECTOR DATA I
17R RANGE(NOM 2642)
440R RANGE RATE(NOM -425l)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
cSI
+3 417+1 (RADAR FILTER INITIALIZED) 41b+l (NO BOHESIGHT) b03-XXXXX RANGE RATE
+5 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGF
41b+1 CSI ROUTINE 373+o2065 CSi TIME 275+03028 TPI TIME 605+0077 COTANGENT OF LOS TO CSM 41b+1 (ONE-HALF OFBITAL-PERIOD) 411+0 HCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT
610R TIME TO CST
43 RESET ET
267R VELOCITY TO BE GAINED CSI
402R FLTA H
371R DFLTA V CDH
5-4
372R DFLTA T CSICDH
-42 415+1 (No BORESIGHT) bO6-xXXXX RANGE RATE
-40 415+1 (NO BORESIGHT)503-XXXXX RANGE RATE dORESIGHT ON CSM
415+1 316+XXXXX RANGE
-37 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE
-15 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE UORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-2 415+1 (No BOHESIGHT) bO3-XXXXX RANGF RATE
i1uR TIME TO CS
RESEF ET
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-30 COPY ROOT FOR 1ST CSI 81J
BORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-t7 415+1 (NO BORFSIGHT) 50-XXxXx RANGF RATE
267R VELOCITY TO HE GAINED CSI
402R LELTA H
371R OFLTA V COH
372R OELTA T CSICDH
-5 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 blb+XXXXX RANGE
-i2 415+1 (No BORESIGHT) 5n3-XXXXX RANGE RATE
415+1 (NO BORESIGHT)
5-5
503-XXXXX RANGF RATE
COPY Roor FOR 2NO CSI BU
bORESIGHT ON CSM 415+1 316+XXXXX RANGE
TEMPPRESS MON SEL - FUEL MAN
A AND 8 PRESS 181 +-3 PIG TEMPPRESS MON SEL - PRPLNT
A AND B TEMP IND 4ODEG 0 IOODEG F A AND B PRFSS IND 181 +-3 PSIA
tEMPPRESS MON SEL - HEL
A AND 8 PRESS IND PSIA
A QUANTITY IND- -- PERCENT RFMAINING
8 QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4p 2 3 (120 - 190 DFG F)
415+1 (NO BORESIGHT)-17 503-XXXXX RANGE RATE
-15 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
(LOS OF MSFN) S-BAND - SLEW 10 P = +90t Y U S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
-12 415+1 (No 8ORESIGHT)
503-XXXXX RANGE RATE
267R VFLOCITY TU BE GAINED CSI
402R OFLTA H
372R TIME CSICH
371R PREDICTED VEL 10 RE GAINED COH
263R OLT-OF-PLANE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATL
-10 COPY RANGE AND ROOT FOR 3RD CSI 8U
SORESIGH ON CSM 41b+1
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
4-13
423R DESIRED ALT RATE AT CDH
402R DELTA Hshy
450R DELTA VX
452R DELTA VZ
623+0 Z-AXIS PARALLEL TO CSM PLANE
IPRO F 16 45 MKS TFI -00001
-52 RESET ET
KEY V93E (REINIT W MATRIX WHEN MARKS =4)
KEY V32E (MARKS = 3)
F 06 75 DELTA HCDH DELTA TCDHTPI DELTA TTPI PRO
F 06 81 DELTA VCDH-LV CDH(N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -00001
-47 KEY VSOE (OUT-OF-PLANE)
_ TIG CDH (NOM 124t24t25) -3000 TIME FROM CDH
F 06 16 l1 LOAD TIG PLANE CHANGE (NOM 123amp54-253 PRO
F 06 90 Y YDOT PSI N90 CSM
VYDOT PRO
-42 KEY V32E (MARKS=1O)
F 06 75 DELTA HCDH DELTA TCDIHTPI DELTA TTPITPI PRO
F 06 81 DELTA VCDH-LV
4-14
CDH (NS1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -OO1
KEY V34E (TERMINATE) F 37 B8
PLANE CHANGE
KEY 30E (EXTERNAL DELTA V)
TIG CDH (NOM 124124t25) -3000 TIME FROM CDH
F 06 33 LOAD TIG PLANE CHANGE (NOM 123154T25) PRO
F 06 81 DELTA VS-LV (NOM 00)
-36 COPY RDOT FOR 1ST CDH BU
KEY V90E (OUT-OF-PLANE)
F 06 16 1 1 LOAD TIG PLANE CHANGE (NOM 1231543251 PRO
F 06 90 Y YOOT PSI N90 CSM
YDOT
PRO
F 06 81 DELTA VS-LV(NOM 00)
COPY YDOT AND LOAD NEGATIVE IN R2 PRO
F 06 42 HA HP DELTA V PRO
F 16 45 MKS TFI MGA
PRO
F 37 BB
KEY 41E (RCS THRUSTING)
-30
4-15
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVRI
410+5 EXTERNAL DELTA V 450+0 451-YDOT 452+0 (LOAD CSM -YDOT)
407+0 ROTATE EXTERNAL DELTA V RF
16 95 DELTA VS-BODY
-3035 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATTVHOLD 407+1 FREEZE EXTERNAL DELTAV
F 16 85 DELTA VS-BODY -
NULL DELTA VIS
PRO F 37BB
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
507+0 Z-AXIS BORESIGHT
(12356) KEY 33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 TIG CDH (NOM 124t24t25) -120 OO ZOO (AGS 0 TIME)
(CONVERT TO MINUTES)
373R _ (NOM 2644) 310R TIME TO CDH
423R DESIRED ALT RATE AT CDH
(ADS OF MSFN) S-BAND - SLEW TOP = ACQUIRE HGA LOCK ON VOICE - BUVOICE -- VOICE VERIFY VOICE TLM BIOMED - LEFT (OR RIGHT)
402R DELTAH
4-16
F 16 45
-25
-23
F 06 75
F 06 81
F 16 45
-12
F 06 75
F 06 81
450R DELTA VX
452R DELTA VZ
PRO MKS TFI -00001
KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
COPY ROOT FOR 2ND CDH BU
KEY v32E (MARKS = 5)
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40DEG TO 1OODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + B PRESS IND PSIA
A QUANTITY IND _ PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING a TEMP MON SEL RCS QUAD 1 4 2 3 (120 - 190 DEG F)i
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
CDH(NB1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO MKS TFI -00001
PRO (FINAL COMP)
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
KEY V9OE (OUT-OF-PLANE)
-7
4-17
F 06 16 jj LOAD TIG CDH FROM DATA PAD (NOM 12424251 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT PRO
COPY YOOT FROM CSM AND LOAD NEGATIVE IN R2
CDH(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RDOT FOR 3RD CDH BU
COMPUTE CDH BU
TRANSMIT TGT DELTA VOS TO CSM AND SYNC COUNTDOWN
KEY V47E (INITIALIZE AGS F 06 16 GET OF AGS 0 TIME 120O00OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
KEY V83E F 16 54 R RDOT THETA
SET ORDEAL PRO
317R _ RANGE
440R RANGE RATE 400+3 AGS ALIGN 40OR (00000 COMPLETE)
277R THETA
-6
4-18
PRO F 3 BB
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY V06N86E F 06 86 DELTA VIS-LV
AGS(N86) CHART
DELTA VX(LVD
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
16 85 DELTA VS-BODY
50OR DELTA VX (NOM -0O3)
502R DELTA VZ (NOM 60)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD 407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS BODY
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS 5OOR 50IR 502R DELTA VX -DELTA VY DELTA VZ-
VERIFY PGNS RESIDUALS N85
DELTA VX(LM)
4-19
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
TPI
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO 507+0 Z-AXIS BORESIGHT
(12426) KEY 34E (TPI)
-36 RESET ET
F 06 37 - amp LOAD TIG TPI FROM DATA PAD (NOM 1250246) PRO
F 06 55 +00000 +02660E +13000 OMEGAT PRO
F 16 45 MARKS TFI -00001
-32 KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
-29 KEY V32E (MARKS = 3)
F 06 37 __ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
RESET ET
410+3 TPI SEARCH ROUTINE 307+04300 DELTA T TRANSFER
4-20
-26 310+02600 TFI TPI
303R THETA AT TPI
267R DELTA VTPI
371R DELTA VTPI + DELTA VTPF
KEY V32E (MARKS = 10)
F 06 37 _ _ _ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VIS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
TEMPIPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40ODEG TO IGODEG F A + B PRESS IND 181 +-3 PSIA
TEMPIPRESS MON SEL - HEL
A + B PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD I 4 2 3 (120 - 190 DEG F)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
RESET ET
-13 310+01300 TFI TPI
303R THETA AT TPI
-12 PRO (FINAL COMP) F 06 37 Z TIG TPIj__
4-21
TRANSMIT TIG OF TPI TO CSM-
PRO F 06 58 HP DELTA VTPI DELTA VTRF
PRO F 06 81 DELTA VS-LV
KEY V9OE (OUT-OF-PLANE)
F 06 16 1 LOAD TIG TPI FROM DATA PAD (NOM 12502461 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT
PRO F 06 81 DELTA VS-LV
COPY CSM YDOT AND LOAD NEGATIVE IN R2 N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 59 DELTA VS LOS
N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI MGA
RESET ET
PRO F 37 BB
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (12000t600)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE)
-10
-6
4-22
F 50 16 DOWNLINK COMPLETE PRO (UPDATE COMPLETE)
400+3 AGS ALIGN 400R (00000 COMPLETE)
-9 277R COPY TGT LOS ANGLE
310+00800
303R THETA AT TPI 410+4 DIRECT TRANSFER AT ET=-8 404+0 405+0 406+0 (MONITOR 470 471 4721
373R TIG TPI
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
KEY 41E (RCS THRUSTING) F 50 18 FOAl ANGLES (REQUEST MNVRI
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
-5 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUS
400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
COMPUTE TPI BU
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
4-23
1685 DELTA VS-BODY
50OR DELTA VX(NOM -115)
502R DELTA VZ(NOM 229)
-Z35 OSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS-BODY
(1250246) BURN +Z
VERIFY AGS RESIDUALS 500R 501R 502R DELTAVX DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
MCC1
KEY V76E (PGNS PULSE) PGNSMODECONT-AUTO
KEY V93E (BEFORE 1ST MARK REINITW MATRIX)
+2 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
4-24
(LOS OF MSFN) S-BAND - SLEW TO P = 90 Y = 0 S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
404+0 405+0 406+0
(MONITOR 470 471 4721
+9 277R COPY TGT LOS ANGLE
+12 PRO (COMPUTE MCC FOR TPI+15I F 06 81 DELTA VS-LV
PRO F 06 59 DELTA VS-LOS
PRO F 16 45 MKS TFI MGA
+13 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUOS
COMPUTE MCC1 BU
PRO F 37 BB
+14 KEY 41E (RCS THRUSTING) F 50 18 FOAL ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+1425 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+15 F 16 85 NULL DELTA VS
PRO F 37 BB
MCC2
KEY V76E (PGNS PULSE)
4-25
PGNS MODE CONT-AUTO
KEY V93E (BEFORE 1ST MARK REINIT W MATRIX)
+16 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
404+0 405+0 406+0 (MONITOR 470 471 47)shy
+24 277R COPY TGT LOS ANGLE
+27 PRO (COMPUTE MCC FORTPI+30) F 06 81 DELTA VS-LV
PRO F 06 59 DELIA VPS-LOS
PRO F 16 45 MKS TFI MGA
+28 277R COPY TGT LOS ANGLE
COPY R RDOT FROM TAPEMETER FOR BUS
COMPUTE MCC2 BU
F 37 BB PRO
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+2925 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+30 F 16 85 NULL DELTA VS
PRO F 37 BB
KEY OOE (P001
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
4-26
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT KEY V34E (TERMINATE)
KEY V37E47E (AVE G) F 16 83 DELTA VIS
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT VERIFY TAPE METER WITH DSKY
BRAKING GATE 30 FPS - 6000 FT 20 FPS - 3000 FT 10 FPS - 1500 FT 5 FPS - 600 FT
RENDEZVOUS
STATION KEEPING
5-1
50 ABORT PROCEDURE
This is a specific AGS nominal abort procedure due to a PGNS failure between insertion and station keeping
51
5-2
Nominal AGS Procedures
ASSUMPTIONS
AFTER INSERTION
I INSERTION COMPLETE (RFSIDUALS NULLED) g PGNS FAILURE BEFORE INSERTION 3 RAUAR NOT LOCKED ON
(UI CoNT-AGS ATlI[uUE MON-AGS(CDR) RATE ERR MON-CNPTR(LMP) ATTITUDE MON-AGS(LMP) SHFITRUN-+5 DEG X-POINTER-HI MULT RADAR IEST Sw-OFF LNb GMbL-OFF ENG ARM-OFF X-IRANSL-2 JETS DEAD BAND-MAX PGNS MODE CONT-OFF THROTJET-JET CB IMU OIR-ON HH MOVE-AUTO rRACK TTCATNANSL-ENABLE(CDR)
AL CPL-ON MODE SL-AGS RNGAL1 MON-RNbRNGRT RAIE ERR MON-RNDZ HDR(CDR) AVl CoNT(3)-PULSE AGS MODE CONT-AUTO ACA4JET-DISABLE(CDR) TTCATRANSL-DISABLE(LMP) ACA4JET-DISABLE(LMP)
bO7+U Z-AXIS BOPESIGHT 400+2 Z-AXIS STEERING PULSE TO NULL AGS ERRORS POINT Z-AXIS IN DIRECTION OF CSM MODE CONT-ATT HOLD ATT CONT(3)-MODE CONTROL O unnr - ZirF
5-3
SLEW PATE - LO
SLEW RR ANT TO OqON FUAI VERIFY MAX SIGNAL STRENGTH RH MOOE-AUTO TRACK NO TRACK LIGHT OFF -
ATT CONT(3h-PULSE
CHECK INSERTION VELOCITY WITH TAPEMETER COMPARE EAPEMETER WITH AGS STATE VECTOR DATA I
17R RANGE(NOM 2642)
440R RANGE RATE(NOM -425l)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
cSI
+3 417+1 (RADAR FILTER INITIALIZED) 41b+l (NO BOHESIGHT) b03-XXXXX RANGE RATE
+5 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGF
41b+1 CSI ROUTINE 373+o2065 CSi TIME 275+03028 TPI TIME 605+0077 COTANGENT OF LOS TO CSM 41b+1 (ONE-HALF OFBITAL-PERIOD) 411+0 HCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT
610R TIME TO CST
43 RESET ET
267R VELOCITY TO BE GAINED CSI
402R FLTA H
371R DFLTA V CDH
5-4
372R DFLTA T CSICDH
-42 415+1 (No BORESIGHT) bO6-xXXXX RANGE RATE
-40 415+1 (NO BORESIGHT)503-XXXXX RANGE RATE dORESIGHT ON CSM
415+1 316+XXXXX RANGE
-37 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE
-15 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE UORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-2 415+1 (No BOHESIGHT) bO3-XXXXX RANGF RATE
i1uR TIME TO CS
RESEF ET
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-30 COPY ROOT FOR 1ST CSI 81J
BORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-t7 415+1 (NO BORFSIGHT) 50-XXxXx RANGF RATE
267R VELOCITY TO HE GAINED CSI
402R LELTA H
371R OFLTA V COH
372R OELTA T CSICDH
-5 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 blb+XXXXX RANGE
-i2 415+1 (No BORESIGHT) 5n3-XXXXX RANGE RATE
415+1 (NO BORESIGHT)
5-5
503-XXXXX RANGF RATE
COPY Roor FOR 2NO CSI BU
bORESIGHT ON CSM 415+1 316+XXXXX RANGE
TEMPPRESS MON SEL - FUEL MAN
A AND 8 PRESS 181 +-3 PIG TEMPPRESS MON SEL - PRPLNT
A AND B TEMP IND 4ODEG 0 IOODEG F A AND B PRFSS IND 181 +-3 PSIA
tEMPPRESS MON SEL - HEL
A AND 8 PRESS IND PSIA
A QUANTITY IND- -- PERCENT RFMAINING
8 QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4p 2 3 (120 - 190 DFG F)
415+1 (NO BORESIGHT)-17 503-XXXXX RANGE RATE
-15 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
(LOS OF MSFN) S-BAND - SLEW 10 P = +90t Y U S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
-12 415+1 (No 8ORESIGHT)
503-XXXXX RANGE RATE
267R VFLOCITY TU BE GAINED CSI
402R OFLTA H
372R TIME CSICH
371R PREDICTED VEL 10 RE GAINED COH
263R OLT-OF-PLANE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATL
-10 COPY RANGE AND ROOT FOR 3RD CSI 8U
SORESIGH ON CSM 41b+1
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
4-14
CDH (NS1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI -OO1
KEY V34E (TERMINATE) F 37 B8
PLANE CHANGE
KEY 30E (EXTERNAL DELTA V)
TIG CDH (NOM 124124t25) -3000 TIME FROM CDH
F 06 33 LOAD TIG PLANE CHANGE (NOM 123154T25) PRO
F 06 81 DELTA VS-LV (NOM 00)
-36 COPY RDOT FOR 1ST CDH BU
KEY V90E (OUT-OF-PLANE)
F 06 16 1 1 LOAD TIG PLANE CHANGE (NOM 1231543251 PRO
F 06 90 Y YOOT PSI N90 CSM
YDOT
PRO
F 06 81 DELTA VS-LV(NOM 00)
COPY YDOT AND LOAD NEGATIVE IN R2 PRO
F 06 42 HA HP DELTA V PRO
F 16 45 MKS TFI MGA
PRO
F 37 BB
KEY 41E (RCS THRUSTING)
-30
4-15
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVRI
410+5 EXTERNAL DELTA V 450+0 451-YDOT 452+0 (LOAD CSM -YDOT)
407+0 ROTATE EXTERNAL DELTA V RF
16 95 DELTA VS-BODY
-3035 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATTVHOLD 407+1 FREEZE EXTERNAL DELTAV
F 16 85 DELTA VS-BODY -
NULL DELTA VIS
PRO F 37BB
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
507+0 Z-AXIS BORESIGHT
(12356) KEY 33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 TIG CDH (NOM 124t24t25) -120 OO ZOO (AGS 0 TIME)
(CONVERT TO MINUTES)
373R _ (NOM 2644) 310R TIME TO CDH
423R DESIRED ALT RATE AT CDH
(ADS OF MSFN) S-BAND - SLEW TOP = ACQUIRE HGA LOCK ON VOICE - BUVOICE -- VOICE VERIFY VOICE TLM BIOMED - LEFT (OR RIGHT)
402R DELTAH
4-16
F 16 45
-25
-23
F 06 75
F 06 81
F 16 45
-12
F 06 75
F 06 81
450R DELTA VX
452R DELTA VZ
PRO MKS TFI -00001
KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
COPY ROOT FOR 2ND CDH BU
KEY v32E (MARKS = 5)
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40DEG TO 1OODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + B PRESS IND PSIA
A QUANTITY IND _ PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING a TEMP MON SEL RCS QUAD 1 4 2 3 (120 - 190 DEG F)i
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
CDH(NB1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO MKS TFI -00001
PRO (FINAL COMP)
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
KEY V9OE (OUT-OF-PLANE)
-7
4-17
F 06 16 jj LOAD TIG CDH FROM DATA PAD (NOM 12424251 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT PRO
COPY YOOT FROM CSM AND LOAD NEGATIVE IN R2
CDH(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RDOT FOR 3RD CDH BU
COMPUTE CDH BU
TRANSMIT TGT DELTA VOS TO CSM AND SYNC COUNTDOWN
KEY V47E (INITIALIZE AGS F 06 16 GET OF AGS 0 TIME 120O00OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
KEY V83E F 16 54 R RDOT THETA
SET ORDEAL PRO
317R _ RANGE
440R RANGE RATE 400+3 AGS ALIGN 40OR (00000 COMPLETE)
277R THETA
-6
4-18
PRO F 3 BB
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY V06N86E F 06 86 DELTA VIS-LV
AGS(N86) CHART
DELTA VX(LVD
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
16 85 DELTA VS-BODY
50OR DELTA VX (NOM -0O3)
502R DELTA VZ (NOM 60)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD 407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS BODY
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS 5OOR 50IR 502R DELTA VX -DELTA VY DELTA VZ-
VERIFY PGNS RESIDUALS N85
DELTA VX(LM)
4-19
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
TPI
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO 507+0 Z-AXIS BORESIGHT
(12426) KEY 34E (TPI)
-36 RESET ET
F 06 37 - amp LOAD TIG TPI FROM DATA PAD (NOM 1250246) PRO
F 06 55 +00000 +02660E +13000 OMEGAT PRO
F 16 45 MARKS TFI -00001
-32 KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
-29 KEY V32E (MARKS = 3)
F 06 37 __ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
RESET ET
410+3 TPI SEARCH ROUTINE 307+04300 DELTA T TRANSFER
4-20
-26 310+02600 TFI TPI
303R THETA AT TPI
267R DELTA VTPI
371R DELTA VTPI + DELTA VTPF
KEY V32E (MARKS = 10)
F 06 37 _ _ _ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VIS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
TEMPIPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40ODEG TO IGODEG F A + B PRESS IND 181 +-3 PSIA
TEMPIPRESS MON SEL - HEL
A + B PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD I 4 2 3 (120 - 190 DEG F)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
RESET ET
-13 310+01300 TFI TPI
303R THETA AT TPI
-12 PRO (FINAL COMP) F 06 37 Z TIG TPIj__
4-21
TRANSMIT TIG OF TPI TO CSM-
PRO F 06 58 HP DELTA VTPI DELTA VTRF
PRO F 06 81 DELTA VS-LV
KEY V9OE (OUT-OF-PLANE)
F 06 16 1 LOAD TIG TPI FROM DATA PAD (NOM 12502461 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT
PRO F 06 81 DELTA VS-LV
COPY CSM YDOT AND LOAD NEGATIVE IN R2 N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 59 DELTA VS LOS
N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI MGA
RESET ET
PRO F 37 BB
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (12000t600)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE)
-10
-6
4-22
F 50 16 DOWNLINK COMPLETE PRO (UPDATE COMPLETE)
400+3 AGS ALIGN 400R (00000 COMPLETE)
-9 277R COPY TGT LOS ANGLE
310+00800
303R THETA AT TPI 410+4 DIRECT TRANSFER AT ET=-8 404+0 405+0 406+0 (MONITOR 470 471 4721
373R TIG TPI
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
KEY 41E (RCS THRUSTING) F 50 18 FOAl ANGLES (REQUEST MNVRI
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
-5 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUS
400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
COMPUTE TPI BU
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
4-23
1685 DELTA VS-BODY
50OR DELTA VX(NOM -115)
502R DELTA VZ(NOM 229)
-Z35 OSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS-BODY
(1250246) BURN +Z
VERIFY AGS RESIDUALS 500R 501R 502R DELTAVX DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
MCC1
KEY V76E (PGNS PULSE) PGNSMODECONT-AUTO
KEY V93E (BEFORE 1ST MARK REINITW MATRIX)
+2 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
4-24
(LOS OF MSFN) S-BAND - SLEW TO P = 90 Y = 0 S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
404+0 405+0 406+0
(MONITOR 470 471 4721
+9 277R COPY TGT LOS ANGLE
+12 PRO (COMPUTE MCC FOR TPI+15I F 06 81 DELTA VS-LV
PRO F 06 59 DELTA VS-LOS
PRO F 16 45 MKS TFI MGA
+13 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUOS
COMPUTE MCC1 BU
PRO F 37 BB
+14 KEY 41E (RCS THRUSTING) F 50 18 FOAL ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+1425 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+15 F 16 85 NULL DELTA VS
PRO F 37 BB
MCC2
KEY V76E (PGNS PULSE)
4-25
PGNS MODE CONT-AUTO
KEY V93E (BEFORE 1ST MARK REINIT W MATRIX)
+16 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
404+0 405+0 406+0 (MONITOR 470 471 47)shy
+24 277R COPY TGT LOS ANGLE
+27 PRO (COMPUTE MCC FORTPI+30) F 06 81 DELTA VS-LV
PRO F 06 59 DELIA VPS-LOS
PRO F 16 45 MKS TFI MGA
+28 277R COPY TGT LOS ANGLE
COPY R RDOT FROM TAPEMETER FOR BUS
COMPUTE MCC2 BU
F 37 BB PRO
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+2925 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+30 F 16 85 NULL DELTA VS
PRO F 37 BB
KEY OOE (P001
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
4-26
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT KEY V34E (TERMINATE)
KEY V37E47E (AVE G) F 16 83 DELTA VIS
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT VERIFY TAPE METER WITH DSKY
BRAKING GATE 30 FPS - 6000 FT 20 FPS - 3000 FT 10 FPS - 1500 FT 5 FPS - 600 FT
RENDEZVOUS
STATION KEEPING
5-1
50 ABORT PROCEDURE
This is a specific AGS nominal abort procedure due to a PGNS failure between insertion and station keeping
51
5-2
Nominal AGS Procedures
ASSUMPTIONS
AFTER INSERTION
I INSERTION COMPLETE (RFSIDUALS NULLED) g PGNS FAILURE BEFORE INSERTION 3 RAUAR NOT LOCKED ON
(UI CoNT-AGS ATlI[uUE MON-AGS(CDR) RATE ERR MON-CNPTR(LMP) ATTITUDE MON-AGS(LMP) SHFITRUN-+5 DEG X-POINTER-HI MULT RADAR IEST Sw-OFF LNb GMbL-OFF ENG ARM-OFF X-IRANSL-2 JETS DEAD BAND-MAX PGNS MODE CONT-OFF THROTJET-JET CB IMU OIR-ON HH MOVE-AUTO rRACK TTCATNANSL-ENABLE(CDR)
AL CPL-ON MODE SL-AGS RNGAL1 MON-RNbRNGRT RAIE ERR MON-RNDZ HDR(CDR) AVl CoNT(3)-PULSE AGS MODE CONT-AUTO ACA4JET-DISABLE(CDR) TTCATRANSL-DISABLE(LMP) ACA4JET-DISABLE(LMP)
bO7+U Z-AXIS BOPESIGHT 400+2 Z-AXIS STEERING PULSE TO NULL AGS ERRORS POINT Z-AXIS IN DIRECTION OF CSM MODE CONT-ATT HOLD ATT CONT(3)-MODE CONTROL O unnr - ZirF
5-3
SLEW PATE - LO
SLEW RR ANT TO OqON FUAI VERIFY MAX SIGNAL STRENGTH RH MOOE-AUTO TRACK NO TRACK LIGHT OFF -
ATT CONT(3h-PULSE
CHECK INSERTION VELOCITY WITH TAPEMETER COMPARE EAPEMETER WITH AGS STATE VECTOR DATA I
17R RANGE(NOM 2642)
440R RANGE RATE(NOM -425l)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
cSI
+3 417+1 (RADAR FILTER INITIALIZED) 41b+l (NO BOHESIGHT) b03-XXXXX RANGE RATE
+5 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGF
41b+1 CSI ROUTINE 373+o2065 CSi TIME 275+03028 TPI TIME 605+0077 COTANGENT OF LOS TO CSM 41b+1 (ONE-HALF OFBITAL-PERIOD) 411+0 HCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT
610R TIME TO CST
43 RESET ET
267R VELOCITY TO BE GAINED CSI
402R FLTA H
371R DFLTA V CDH
5-4
372R DFLTA T CSICDH
-42 415+1 (No BORESIGHT) bO6-xXXXX RANGE RATE
-40 415+1 (NO BORESIGHT)503-XXXXX RANGE RATE dORESIGHT ON CSM
415+1 316+XXXXX RANGE
-37 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE
-15 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE UORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-2 415+1 (No BOHESIGHT) bO3-XXXXX RANGF RATE
i1uR TIME TO CS
RESEF ET
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-30 COPY ROOT FOR 1ST CSI 81J
BORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-t7 415+1 (NO BORFSIGHT) 50-XXxXx RANGF RATE
267R VELOCITY TO HE GAINED CSI
402R LELTA H
371R OFLTA V COH
372R OELTA T CSICDH
-5 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 blb+XXXXX RANGE
-i2 415+1 (No BORESIGHT) 5n3-XXXXX RANGE RATE
415+1 (NO BORESIGHT)
5-5
503-XXXXX RANGF RATE
COPY Roor FOR 2NO CSI BU
bORESIGHT ON CSM 415+1 316+XXXXX RANGE
TEMPPRESS MON SEL - FUEL MAN
A AND 8 PRESS 181 +-3 PIG TEMPPRESS MON SEL - PRPLNT
A AND B TEMP IND 4ODEG 0 IOODEG F A AND B PRFSS IND 181 +-3 PSIA
tEMPPRESS MON SEL - HEL
A AND 8 PRESS IND PSIA
A QUANTITY IND- -- PERCENT RFMAINING
8 QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4p 2 3 (120 - 190 DFG F)
415+1 (NO BORESIGHT)-17 503-XXXXX RANGE RATE
-15 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
(LOS OF MSFN) S-BAND - SLEW 10 P = +90t Y U S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
-12 415+1 (No 8ORESIGHT)
503-XXXXX RANGE RATE
267R VFLOCITY TU BE GAINED CSI
402R OFLTA H
372R TIME CSICH
371R PREDICTED VEL 10 RE GAINED COH
263R OLT-OF-PLANE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATL
-10 COPY RANGE AND ROOT FOR 3RD CSI 8U
SORESIGH ON CSM 41b+1
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
-30
4-15
F 50 18 FDAI ANGLES (REQUEST MNVR) ENTR (BYPASS MNVRI
410+5 EXTERNAL DELTA V 450+0 451-YDOT 452+0 (LOAD CSM -YDOT)
407+0 ROTATE EXTERNAL DELTA V RF
16 95 DELTA VS-BODY
-3035 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATTVHOLD 407+1 FREEZE EXTERNAL DELTAV
F 16 85 DELTA VS-BODY -
NULL DELTA VIS
PRO F 37BB
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO
507+0 Z-AXIS BORESIGHT
(12356) KEY 33E (CDH PRE-THRUST)
410+2 CDH ROUTINE
F 06 13 TIG CDH (NOM 124t24t25) -120 OO ZOO (AGS 0 TIME)
(CONVERT TO MINUTES)
373R _ (NOM 2644) 310R TIME TO CDH
423R DESIRED ALT RATE AT CDH
(ADS OF MSFN) S-BAND - SLEW TOP = ACQUIRE HGA LOCK ON VOICE - BUVOICE -- VOICE VERIFY VOICE TLM BIOMED - LEFT (OR RIGHT)
402R DELTAH
4-16
F 16 45
-25
-23
F 06 75
F 06 81
F 16 45
-12
F 06 75
F 06 81
450R DELTA VX
452R DELTA VZ
PRO MKS TFI -00001
KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
COPY ROOT FOR 2ND CDH BU
KEY v32E (MARKS = 5)
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40DEG TO 1OODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + B PRESS IND PSIA
A QUANTITY IND _ PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING a TEMP MON SEL RCS QUAD 1 4 2 3 (120 - 190 DEG F)i
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
CDH(NB1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO MKS TFI -00001
PRO (FINAL COMP)
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
KEY V9OE (OUT-OF-PLANE)
-7
4-17
F 06 16 jj LOAD TIG CDH FROM DATA PAD (NOM 12424251 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT PRO
COPY YOOT FROM CSM AND LOAD NEGATIVE IN R2
CDH(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RDOT FOR 3RD CDH BU
COMPUTE CDH BU
TRANSMIT TGT DELTA VOS TO CSM AND SYNC COUNTDOWN
KEY V47E (INITIALIZE AGS F 06 16 GET OF AGS 0 TIME 120O00OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
KEY V83E F 16 54 R RDOT THETA
SET ORDEAL PRO
317R _ RANGE
440R RANGE RATE 400+3 AGS ALIGN 40OR (00000 COMPLETE)
277R THETA
-6
4-18
PRO F 3 BB
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY V06N86E F 06 86 DELTA VIS-LV
AGS(N86) CHART
DELTA VX(LVD
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
16 85 DELTA VS-BODY
50OR DELTA VX (NOM -0O3)
502R DELTA VZ (NOM 60)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD 407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS BODY
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS 5OOR 50IR 502R DELTA VX -DELTA VY DELTA VZ-
VERIFY PGNS RESIDUALS N85
DELTA VX(LM)
4-19
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
TPI
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO 507+0 Z-AXIS BORESIGHT
(12426) KEY 34E (TPI)
-36 RESET ET
F 06 37 - amp LOAD TIG TPI FROM DATA PAD (NOM 1250246) PRO
F 06 55 +00000 +02660E +13000 OMEGAT PRO
F 16 45 MARKS TFI -00001
-32 KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
-29 KEY V32E (MARKS = 3)
F 06 37 __ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
RESET ET
410+3 TPI SEARCH ROUTINE 307+04300 DELTA T TRANSFER
4-20
-26 310+02600 TFI TPI
303R THETA AT TPI
267R DELTA VTPI
371R DELTA VTPI + DELTA VTPF
KEY V32E (MARKS = 10)
F 06 37 _ _ _ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VIS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
TEMPIPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40ODEG TO IGODEG F A + B PRESS IND 181 +-3 PSIA
TEMPIPRESS MON SEL - HEL
A + B PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD I 4 2 3 (120 - 190 DEG F)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
RESET ET
-13 310+01300 TFI TPI
303R THETA AT TPI
-12 PRO (FINAL COMP) F 06 37 Z TIG TPIj__
4-21
TRANSMIT TIG OF TPI TO CSM-
PRO F 06 58 HP DELTA VTPI DELTA VTRF
PRO F 06 81 DELTA VS-LV
KEY V9OE (OUT-OF-PLANE)
F 06 16 1 LOAD TIG TPI FROM DATA PAD (NOM 12502461 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT
PRO F 06 81 DELTA VS-LV
COPY CSM YDOT AND LOAD NEGATIVE IN R2 N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 59 DELTA VS LOS
N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI MGA
RESET ET
PRO F 37 BB
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (12000t600)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE)
-10
-6
4-22
F 50 16 DOWNLINK COMPLETE PRO (UPDATE COMPLETE)
400+3 AGS ALIGN 400R (00000 COMPLETE)
-9 277R COPY TGT LOS ANGLE
310+00800
303R THETA AT TPI 410+4 DIRECT TRANSFER AT ET=-8 404+0 405+0 406+0 (MONITOR 470 471 4721
373R TIG TPI
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
KEY 41E (RCS THRUSTING) F 50 18 FOAl ANGLES (REQUEST MNVRI
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
-5 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUS
400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
COMPUTE TPI BU
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
4-23
1685 DELTA VS-BODY
50OR DELTA VX(NOM -115)
502R DELTA VZ(NOM 229)
-Z35 OSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS-BODY
(1250246) BURN +Z
VERIFY AGS RESIDUALS 500R 501R 502R DELTAVX DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
MCC1
KEY V76E (PGNS PULSE) PGNSMODECONT-AUTO
KEY V93E (BEFORE 1ST MARK REINITW MATRIX)
+2 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
4-24
(LOS OF MSFN) S-BAND - SLEW TO P = 90 Y = 0 S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
404+0 405+0 406+0
(MONITOR 470 471 4721
+9 277R COPY TGT LOS ANGLE
+12 PRO (COMPUTE MCC FOR TPI+15I F 06 81 DELTA VS-LV
PRO F 06 59 DELTA VS-LOS
PRO F 16 45 MKS TFI MGA
+13 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUOS
COMPUTE MCC1 BU
PRO F 37 BB
+14 KEY 41E (RCS THRUSTING) F 50 18 FOAL ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+1425 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+15 F 16 85 NULL DELTA VS
PRO F 37 BB
MCC2
KEY V76E (PGNS PULSE)
4-25
PGNS MODE CONT-AUTO
KEY V93E (BEFORE 1ST MARK REINIT W MATRIX)
+16 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
404+0 405+0 406+0 (MONITOR 470 471 47)shy
+24 277R COPY TGT LOS ANGLE
+27 PRO (COMPUTE MCC FORTPI+30) F 06 81 DELTA VS-LV
PRO F 06 59 DELIA VPS-LOS
PRO F 16 45 MKS TFI MGA
+28 277R COPY TGT LOS ANGLE
COPY R RDOT FROM TAPEMETER FOR BUS
COMPUTE MCC2 BU
F 37 BB PRO
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+2925 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+30 F 16 85 NULL DELTA VS
PRO F 37 BB
KEY OOE (P001
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
4-26
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT KEY V34E (TERMINATE)
KEY V37E47E (AVE G) F 16 83 DELTA VIS
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT VERIFY TAPE METER WITH DSKY
BRAKING GATE 30 FPS - 6000 FT 20 FPS - 3000 FT 10 FPS - 1500 FT 5 FPS - 600 FT
RENDEZVOUS
STATION KEEPING
5-1
50 ABORT PROCEDURE
This is a specific AGS nominal abort procedure due to a PGNS failure between insertion and station keeping
51
5-2
Nominal AGS Procedures
ASSUMPTIONS
AFTER INSERTION
I INSERTION COMPLETE (RFSIDUALS NULLED) g PGNS FAILURE BEFORE INSERTION 3 RAUAR NOT LOCKED ON
(UI CoNT-AGS ATlI[uUE MON-AGS(CDR) RATE ERR MON-CNPTR(LMP) ATTITUDE MON-AGS(LMP) SHFITRUN-+5 DEG X-POINTER-HI MULT RADAR IEST Sw-OFF LNb GMbL-OFF ENG ARM-OFF X-IRANSL-2 JETS DEAD BAND-MAX PGNS MODE CONT-OFF THROTJET-JET CB IMU OIR-ON HH MOVE-AUTO rRACK TTCATNANSL-ENABLE(CDR)
AL CPL-ON MODE SL-AGS RNGAL1 MON-RNbRNGRT RAIE ERR MON-RNDZ HDR(CDR) AVl CoNT(3)-PULSE AGS MODE CONT-AUTO ACA4JET-DISABLE(CDR) TTCATRANSL-DISABLE(LMP) ACA4JET-DISABLE(LMP)
bO7+U Z-AXIS BOPESIGHT 400+2 Z-AXIS STEERING PULSE TO NULL AGS ERRORS POINT Z-AXIS IN DIRECTION OF CSM MODE CONT-ATT HOLD ATT CONT(3)-MODE CONTROL O unnr - ZirF
5-3
SLEW PATE - LO
SLEW RR ANT TO OqON FUAI VERIFY MAX SIGNAL STRENGTH RH MOOE-AUTO TRACK NO TRACK LIGHT OFF -
ATT CONT(3h-PULSE
CHECK INSERTION VELOCITY WITH TAPEMETER COMPARE EAPEMETER WITH AGS STATE VECTOR DATA I
17R RANGE(NOM 2642)
440R RANGE RATE(NOM -425l)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
cSI
+3 417+1 (RADAR FILTER INITIALIZED) 41b+l (NO BOHESIGHT) b03-XXXXX RANGE RATE
+5 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGF
41b+1 CSI ROUTINE 373+o2065 CSi TIME 275+03028 TPI TIME 605+0077 COTANGENT OF LOS TO CSM 41b+1 (ONE-HALF OFBITAL-PERIOD) 411+0 HCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT
610R TIME TO CST
43 RESET ET
267R VELOCITY TO BE GAINED CSI
402R FLTA H
371R DFLTA V CDH
5-4
372R DFLTA T CSICDH
-42 415+1 (No BORESIGHT) bO6-xXXXX RANGE RATE
-40 415+1 (NO BORESIGHT)503-XXXXX RANGE RATE dORESIGHT ON CSM
415+1 316+XXXXX RANGE
-37 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE
-15 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE UORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-2 415+1 (No BOHESIGHT) bO3-XXXXX RANGF RATE
i1uR TIME TO CS
RESEF ET
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-30 COPY ROOT FOR 1ST CSI 81J
BORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-t7 415+1 (NO BORFSIGHT) 50-XXxXx RANGF RATE
267R VELOCITY TO HE GAINED CSI
402R LELTA H
371R OFLTA V COH
372R OELTA T CSICDH
-5 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 blb+XXXXX RANGE
-i2 415+1 (No BORESIGHT) 5n3-XXXXX RANGE RATE
415+1 (NO BORESIGHT)
5-5
503-XXXXX RANGF RATE
COPY Roor FOR 2NO CSI BU
bORESIGHT ON CSM 415+1 316+XXXXX RANGE
TEMPPRESS MON SEL - FUEL MAN
A AND 8 PRESS 181 +-3 PIG TEMPPRESS MON SEL - PRPLNT
A AND B TEMP IND 4ODEG 0 IOODEG F A AND B PRFSS IND 181 +-3 PSIA
tEMPPRESS MON SEL - HEL
A AND 8 PRESS IND PSIA
A QUANTITY IND- -- PERCENT RFMAINING
8 QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4p 2 3 (120 - 190 DFG F)
415+1 (NO BORESIGHT)-17 503-XXXXX RANGE RATE
-15 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
(LOS OF MSFN) S-BAND - SLEW 10 P = +90t Y U S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
-12 415+1 (No 8ORESIGHT)
503-XXXXX RANGE RATE
267R VFLOCITY TU BE GAINED CSI
402R OFLTA H
372R TIME CSICH
371R PREDICTED VEL 10 RE GAINED COH
263R OLT-OF-PLANE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATL
-10 COPY RANGE AND ROOT FOR 3RD CSI 8U
SORESIGH ON CSM 41b+1
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
4-16
F 16 45
-25
-23
F 06 75
F 06 81
F 16 45
-12
F 06 75
F 06 81
450R DELTA VX
452R DELTA VZ
PRO MKS TFI -00001
KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
COPY ROOT FOR 2ND CDH BU
KEY v32E (MARKS = 5)
TEMPPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40DEG TO 1OODEG F A + B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A + B PRESS IND PSIA
A QUANTITY IND _ PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING a TEMP MON SEL RCS QUAD 1 4 2 3 (120 - 190 DEG F)i
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
CDH(NB1)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO MKS TFI -00001
PRO (FINAL COMP)
DELTA HCDH DELTA TCDHTPI DELTA TTPITPI PRO DELTA VCDH-LV
KEY V9OE (OUT-OF-PLANE)
-7
4-17
F 06 16 jj LOAD TIG CDH FROM DATA PAD (NOM 12424251 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT PRO
COPY YOOT FROM CSM AND LOAD NEGATIVE IN R2
CDH(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RDOT FOR 3RD CDH BU
COMPUTE CDH BU
TRANSMIT TGT DELTA VOS TO CSM AND SYNC COUNTDOWN
KEY V47E (INITIALIZE AGS F 06 16 GET OF AGS 0 TIME 120O00OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
KEY V83E F 16 54 R RDOT THETA
SET ORDEAL PRO
317R _ RANGE
440R RANGE RATE 400+3 AGS ALIGN 40OR (00000 COMPLETE)
277R THETA
-6
4-18
PRO F 3 BB
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY V06N86E F 06 86 DELTA VIS-LV
AGS(N86) CHART
DELTA VX(LVD
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
16 85 DELTA VS-BODY
50OR DELTA VX (NOM -0O3)
502R DELTA VZ (NOM 60)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD 407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS BODY
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS 5OOR 50IR 502R DELTA VX -DELTA VY DELTA VZ-
VERIFY PGNS RESIDUALS N85
DELTA VX(LM)
4-19
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
TPI
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO 507+0 Z-AXIS BORESIGHT
(12426) KEY 34E (TPI)
-36 RESET ET
F 06 37 - amp LOAD TIG TPI FROM DATA PAD (NOM 1250246) PRO
F 06 55 +00000 +02660E +13000 OMEGAT PRO
F 16 45 MARKS TFI -00001
-32 KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
-29 KEY V32E (MARKS = 3)
F 06 37 __ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
RESET ET
410+3 TPI SEARCH ROUTINE 307+04300 DELTA T TRANSFER
4-20
-26 310+02600 TFI TPI
303R THETA AT TPI
267R DELTA VTPI
371R DELTA VTPI + DELTA VTPF
KEY V32E (MARKS = 10)
F 06 37 _ _ _ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VIS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
TEMPIPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40ODEG TO IGODEG F A + B PRESS IND 181 +-3 PSIA
TEMPIPRESS MON SEL - HEL
A + B PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD I 4 2 3 (120 - 190 DEG F)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
RESET ET
-13 310+01300 TFI TPI
303R THETA AT TPI
-12 PRO (FINAL COMP) F 06 37 Z TIG TPIj__
4-21
TRANSMIT TIG OF TPI TO CSM-
PRO F 06 58 HP DELTA VTPI DELTA VTRF
PRO F 06 81 DELTA VS-LV
KEY V9OE (OUT-OF-PLANE)
F 06 16 1 LOAD TIG TPI FROM DATA PAD (NOM 12502461 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT
PRO F 06 81 DELTA VS-LV
COPY CSM YDOT AND LOAD NEGATIVE IN R2 N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 59 DELTA VS LOS
N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI MGA
RESET ET
PRO F 37 BB
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (12000t600)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE)
-10
-6
4-22
F 50 16 DOWNLINK COMPLETE PRO (UPDATE COMPLETE)
400+3 AGS ALIGN 400R (00000 COMPLETE)
-9 277R COPY TGT LOS ANGLE
310+00800
303R THETA AT TPI 410+4 DIRECT TRANSFER AT ET=-8 404+0 405+0 406+0 (MONITOR 470 471 4721
373R TIG TPI
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
KEY 41E (RCS THRUSTING) F 50 18 FOAl ANGLES (REQUEST MNVRI
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
-5 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUS
400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
COMPUTE TPI BU
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
4-23
1685 DELTA VS-BODY
50OR DELTA VX(NOM -115)
502R DELTA VZ(NOM 229)
-Z35 OSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS-BODY
(1250246) BURN +Z
VERIFY AGS RESIDUALS 500R 501R 502R DELTAVX DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
MCC1
KEY V76E (PGNS PULSE) PGNSMODECONT-AUTO
KEY V93E (BEFORE 1ST MARK REINITW MATRIX)
+2 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
4-24
(LOS OF MSFN) S-BAND - SLEW TO P = 90 Y = 0 S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
404+0 405+0 406+0
(MONITOR 470 471 4721
+9 277R COPY TGT LOS ANGLE
+12 PRO (COMPUTE MCC FOR TPI+15I F 06 81 DELTA VS-LV
PRO F 06 59 DELTA VS-LOS
PRO F 16 45 MKS TFI MGA
+13 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUOS
COMPUTE MCC1 BU
PRO F 37 BB
+14 KEY 41E (RCS THRUSTING) F 50 18 FOAL ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+1425 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+15 F 16 85 NULL DELTA VS
PRO F 37 BB
MCC2
KEY V76E (PGNS PULSE)
4-25
PGNS MODE CONT-AUTO
KEY V93E (BEFORE 1ST MARK REINIT W MATRIX)
+16 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
404+0 405+0 406+0 (MONITOR 470 471 47)shy
+24 277R COPY TGT LOS ANGLE
+27 PRO (COMPUTE MCC FORTPI+30) F 06 81 DELTA VS-LV
PRO F 06 59 DELIA VPS-LOS
PRO F 16 45 MKS TFI MGA
+28 277R COPY TGT LOS ANGLE
COPY R RDOT FROM TAPEMETER FOR BUS
COMPUTE MCC2 BU
F 37 BB PRO
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+2925 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+30 F 16 85 NULL DELTA VS
PRO F 37 BB
KEY OOE (P001
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
4-26
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT KEY V34E (TERMINATE)
KEY V37E47E (AVE G) F 16 83 DELTA VIS
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT VERIFY TAPE METER WITH DSKY
BRAKING GATE 30 FPS - 6000 FT 20 FPS - 3000 FT 10 FPS - 1500 FT 5 FPS - 600 FT
RENDEZVOUS
STATION KEEPING
5-1
50 ABORT PROCEDURE
This is a specific AGS nominal abort procedure due to a PGNS failure between insertion and station keeping
51
5-2
Nominal AGS Procedures
ASSUMPTIONS
AFTER INSERTION
I INSERTION COMPLETE (RFSIDUALS NULLED) g PGNS FAILURE BEFORE INSERTION 3 RAUAR NOT LOCKED ON
(UI CoNT-AGS ATlI[uUE MON-AGS(CDR) RATE ERR MON-CNPTR(LMP) ATTITUDE MON-AGS(LMP) SHFITRUN-+5 DEG X-POINTER-HI MULT RADAR IEST Sw-OFF LNb GMbL-OFF ENG ARM-OFF X-IRANSL-2 JETS DEAD BAND-MAX PGNS MODE CONT-OFF THROTJET-JET CB IMU OIR-ON HH MOVE-AUTO rRACK TTCATNANSL-ENABLE(CDR)
AL CPL-ON MODE SL-AGS RNGAL1 MON-RNbRNGRT RAIE ERR MON-RNDZ HDR(CDR) AVl CoNT(3)-PULSE AGS MODE CONT-AUTO ACA4JET-DISABLE(CDR) TTCATRANSL-DISABLE(LMP) ACA4JET-DISABLE(LMP)
bO7+U Z-AXIS BOPESIGHT 400+2 Z-AXIS STEERING PULSE TO NULL AGS ERRORS POINT Z-AXIS IN DIRECTION OF CSM MODE CONT-ATT HOLD ATT CONT(3)-MODE CONTROL O unnr - ZirF
5-3
SLEW PATE - LO
SLEW RR ANT TO OqON FUAI VERIFY MAX SIGNAL STRENGTH RH MOOE-AUTO TRACK NO TRACK LIGHT OFF -
ATT CONT(3h-PULSE
CHECK INSERTION VELOCITY WITH TAPEMETER COMPARE EAPEMETER WITH AGS STATE VECTOR DATA I
17R RANGE(NOM 2642)
440R RANGE RATE(NOM -425l)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
cSI
+3 417+1 (RADAR FILTER INITIALIZED) 41b+l (NO BOHESIGHT) b03-XXXXX RANGE RATE
+5 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGF
41b+1 CSI ROUTINE 373+o2065 CSi TIME 275+03028 TPI TIME 605+0077 COTANGENT OF LOS TO CSM 41b+1 (ONE-HALF OFBITAL-PERIOD) 411+0 HCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT
610R TIME TO CST
43 RESET ET
267R VELOCITY TO BE GAINED CSI
402R FLTA H
371R DFLTA V CDH
5-4
372R DFLTA T CSICDH
-42 415+1 (No BORESIGHT) bO6-xXXXX RANGE RATE
-40 415+1 (NO BORESIGHT)503-XXXXX RANGE RATE dORESIGHT ON CSM
415+1 316+XXXXX RANGE
-37 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE
-15 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE UORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-2 415+1 (No BOHESIGHT) bO3-XXXXX RANGF RATE
i1uR TIME TO CS
RESEF ET
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-30 COPY ROOT FOR 1ST CSI 81J
BORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-t7 415+1 (NO BORFSIGHT) 50-XXxXx RANGF RATE
267R VELOCITY TO HE GAINED CSI
402R LELTA H
371R OFLTA V COH
372R OELTA T CSICDH
-5 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 blb+XXXXX RANGE
-i2 415+1 (No BORESIGHT) 5n3-XXXXX RANGE RATE
415+1 (NO BORESIGHT)
5-5
503-XXXXX RANGF RATE
COPY Roor FOR 2NO CSI BU
bORESIGHT ON CSM 415+1 316+XXXXX RANGE
TEMPPRESS MON SEL - FUEL MAN
A AND 8 PRESS 181 +-3 PIG TEMPPRESS MON SEL - PRPLNT
A AND B TEMP IND 4ODEG 0 IOODEG F A AND B PRFSS IND 181 +-3 PSIA
tEMPPRESS MON SEL - HEL
A AND 8 PRESS IND PSIA
A QUANTITY IND- -- PERCENT RFMAINING
8 QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4p 2 3 (120 - 190 DFG F)
415+1 (NO BORESIGHT)-17 503-XXXXX RANGE RATE
-15 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
(LOS OF MSFN) S-BAND - SLEW 10 P = +90t Y U S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
-12 415+1 (No 8ORESIGHT)
503-XXXXX RANGE RATE
267R VFLOCITY TU BE GAINED CSI
402R OFLTA H
372R TIME CSICH
371R PREDICTED VEL 10 RE GAINED COH
263R OLT-OF-PLANE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATL
-10 COPY RANGE AND ROOT FOR 3RD CSI 8U
SORESIGH ON CSM 41b+1
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
-7
4-17
F 06 16 jj LOAD TIG CDH FROM DATA PAD (NOM 12424251 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT PRO
COPY YOOT FROM CSM AND LOAD NEGATIVE IN R2
CDH(N81)
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 16 45 MKS TFI MGA
-10 COPY RDOT FOR 3RD CDH BU
COMPUTE CDH BU
TRANSMIT TGT DELTA VOS TO CSM AND SYNC COUNTDOWN
KEY V47E (INITIALIZE AGS F 06 16 GET OF AGS 0 TIME 120O00OO)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE) F 50 16 DOWNLINK COMPLETE
PRO (UPDATE COMPLETE)
F 16 45 MKS TFI MGA
KEY V83E F 16 54 R RDOT THETA
SET ORDEAL PRO
317R _ RANGE
440R RANGE RATE 400+3 AGS ALIGN 40OR (00000 COMPLETE)
277R THETA
-6
4-18
PRO F 3 BB
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY V06N86E F 06 86 DELTA VIS-LV
AGS(N86) CHART
DELTA VX(LVD
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
16 85 DELTA VS-BODY
50OR DELTA VX (NOM -0O3)
502R DELTA VZ (NOM 60)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD 407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS BODY
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS 5OOR 50IR 502R DELTA VX -DELTA VY DELTA VZ-
VERIFY PGNS RESIDUALS N85
DELTA VX(LM)
4-19
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
TPI
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO 507+0 Z-AXIS BORESIGHT
(12426) KEY 34E (TPI)
-36 RESET ET
F 06 37 - amp LOAD TIG TPI FROM DATA PAD (NOM 1250246) PRO
F 06 55 +00000 +02660E +13000 OMEGAT PRO
F 16 45 MARKS TFI -00001
-32 KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
-29 KEY V32E (MARKS = 3)
F 06 37 __ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
RESET ET
410+3 TPI SEARCH ROUTINE 307+04300 DELTA T TRANSFER
4-20
-26 310+02600 TFI TPI
303R THETA AT TPI
267R DELTA VTPI
371R DELTA VTPI + DELTA VTPF
KEY V32E (MARKS = 10)
F 06 37 _ _ _ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VIS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
TEMPIPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40ODEG TO IGODEG F A + B PRESS IND 181 +-3 PSIA
TEMPIPRESS MON SEL - HEL
A + B PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD I 4 2 3 (120 - 190 DEG F)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
RESET ET
-13 310+01300 TFI TPI
303R THETA AT TPI
-12 PRO (FINAL COMP) F 06 37 Z TIG TPIj__
4-21
TRANSMIT TIG OF TPI TO CSM-
PRO F 06 58 HP DELTA VTPI DELTA VTRF
PRO F 06 81 DELTA VS-LV
KEY V9OE (OUT-OF-PLANE)
F 06 16 1 LOAD TIG TPI FROM DATA PAD (NOM 12502461 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT
PRO F 06 81 DELTA VS-LV
COPY CSM YDOT AND LOAD NEGATIVE IN R2 N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 59 DELTA VS LOS
N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI MGA
RESET ET
PRO F 37 BB
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (12000t600)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE)
-10
-6
4-22
F 50 16 DOWNLINK COMPLETE PRO (UPDATE COMPLETE)
400+3 AGS ALIGN 400R (00000 COMPLETE)
-9 277R COPY TGT LOS ANGLE
310+00800
303R THETA AT TPI 410+4 DIRECT TRANSFER AT ET=-8 404+0 405+0 406+0 (MONITOR 470 471 4721
373R TIG TPI
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
KEY 41E (RCS THRUSTING) F 50 18 FOAl ANGLES (REQUEST MNVRI
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
-5 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUS
400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
COMPUTE TPI BU
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
4-23
1685 DELTA VS-BODY
50OR DELTA VX(NOM -115)
502R DELTA VZ(NOM 229)
-Z35 OSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS-BODY
(1250246) BURN +Z
VERIFY AGS RESIDUALS 500R 501R 502R DELTAVX DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
MCC1
KEY V76E (PGNS PULSE) PGNSMODECONT-AUTO
KEY V93E (BEFORE 1ST MARK REINITW MATRIX)
+2 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
4-24
(LOS OF MSFN) S-BAND - SLEW TO P = 90 Y = 0 S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
404+0 405+0 406+0
(MONITOR 470 471 4721
+9 277R COPY TGT LOS ANGLE
+12 PRO (COMPUTE MCC FOR TPI+15I F 06 81 DELTA VS-LV
PRO F 06 59 DELTA VS-LOS
PRO F 16 45 MKS TFI MGA
+13 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUOS
COMPUTE MCC1 BU
PRO F 37 BB
+14 KEY 41E (RCS THRUSTING) F 50 18 FOAL ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+1425 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+15 F 16 85 NULL DELTA VS
PRO F 37 BB
MCC2
KEY V76E (PGNS PULSE)
4-25
PGNS MODE CONT-AUTO
KEY V93E (BEFORE 1ST MARK REINIT W MATRIX)
+16 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
404+0 405+0 406+0 (MONITOR 470 471 47)shy
+24 277R COPY TGT LOS ANGLE
+27 PRO (COMPUTE MCC FORTPI+30) F 06 81 DELTA VS-LV
PRO F 06 59 DELIA VPS-LOS
PRO F 16 45 MKS TFI MGA
+28 277R COPY TGT LOS ANGLE
COPY R RDOT FROM TAPEMETER FOR BUS
COMPUTE MCC2 BU
F 37 BB PRO
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+2925 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+30 F 16 85 NULL DELTA VS
PRO F 37 BB
KEY OOE (P001
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
4-26
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT KEY V34E (TERMINATE)
KEY V37E47E (AVE G) F 16 83 DELTA VIS
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT VERIFY TAPE METER WITH DSKY
BRAKING GATE 30 FPS - 6000 FT 20 FPS - 3000 FT 10 FPS - 1500 FT 5 FPS - 600 FT
RENDEZVOUS
STATION KEEPING
5-1
50 ABORT PROCEDURE
This is a specific AGS nominal abort procedure due to a PGNS failure between insertion and station keeping
51
5-2
Nominal AGS Procedures
ASSUMPTIONS
AFTER INSERTION
I INSERTION COMPLETE (RFSIDUALS NULLED) g PGNS FAILURE BEFORE INSERTION 3 RAUAR NOT LOCKED ON
(UI CoNT-AGS ATlI[uUE MON-AGS(CDR) RATE ERR MON-CNPTR(LMP) ATTITUDE MON-AGS(LMP) SHFITRUN-+5 DEG X-POINTER-HI MULT RADAR IEST Sw-OFF LNb GMbL-OFF ENG ARM-OFF X-IRANSL-2 JETS DEAD BAND-MAX PGNS MODE CONT-OFF THROTJET-JET CB IMU OIR-ON HH MOVE-AUTO rRACK TTCATNANSL-ENABLE(CDR)
AL CPL-ON MODE SL-AGS RNGAL1 MON-RNbRNGRT RAIE ERR MON-RNDZ HDR(CDR) AVl CoNT(3)-PULSE AGS MODE CONT-AUTO ACA4JET-DISABLE(CDR) TTCATRANSL-DISABLE(LMP) ACA4JET-DISABLE(LMP)
bO7+U Z-AXIS BOPESIGHT 400+2 Z-AXIS STEERING PULSE TO NULL AGS ERRORS POINT Z-AXIS IN DIRECTION OF CSM MODE CONT-ATT HOLD ATT CONT(3)-MODE CONTROL O unnr - ZirF
5-3
SLEW PATE - LO
SLEW RR ANT TO OqON FUAI VERIFY MAX SIGNAL STRENGTH RH MOOE-AUTO TRACK NO TRACK LIGHT OFF -
ATT CONT(3h-PULSE
CHECK INSERTION VELOCITY WITH TAPEMETER COMPARE EAPEMETER WITH AGS STATE VECTOR DATA I
17R RANGE(NOM 2642)
440R RANGE RATE(NOM -425l)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
cSI
+3 417+1 (RADAR FILTER INITIALIZED) 41b+l (NO BOHESIGHT) b03-XXXXX RANGE RATE
+5 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGF
41b+1 CSI ROUTINE 373+o2065 CSi TIME 275+03028 TPI TIME 605+0077 COTANGENT OF LOS TO CSM 41b+1 (ONE-HALF OFBITAL-PERIOD) 411+0 HCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT
610R TIME TO CST
43 RESET ET
267R VELOCITY TO BE GAINED CSI
402R FLTA H
371R DFLTA V CDH
5-4
372R DFLTA T CSICDH
-42 415+1 (No BORESIGHT) bO6-xXXXX RANGE RATE
-40 415+1 (NO BORESIGHT)503-XXXXX RANGE RATE dORESIGHT ON CSM
415+1 316+XXXXX RANGE
-37 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE
-15 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE UORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-2 415+1 (No BOHESIGHT) bO3-XXXXX RANGF RATE
i1uR TIME TO CS
RESEF ET
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-30 COPY ROOT FOR 1ST CSI 81J
BORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-t7 415+1 (NO BORFSIGHT) 50-XXxXx RANGF RATE
267R VELOCITY TO HE GAINED CSI
402R LELTA H
371R OFLTA V COH
372R OELTA T CSICDH
-5 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 blb+XXXXX RANGE
-i2 415+1 (No BORESIGHT) 5n3-XXXXX RANGE RATE
415+1 (NO BORESIGHT)
5-5
503-XXXXX RANGF RATE
COPY Roor FOR 2NO CSI BU
bORESIGHT ON CSM 415+1 316+XXXXX RANGE
TEMPPRESS MON SEL - FUEL MAN
A AND 8 PRESS 181 +-3 PIG TEMPPRESS MON SEL - PRPLNT
A AND B TEMP IND 4ODEG 0 IOODEG F A AND B PRFSS IND 181 +-3 PSIA
tEMPPRESS MON SEL - HEL
A AND 8 PRESS IND PSIA
A QUANTITY IND- -- PERCENT RFMAINING
8 QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4p 2 3 (120 - 190 DFG F)
415+1 (NO BORESIGHT)-17 503-XXXXX RANGE RATE
-15 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
(LOS OF MSFN) S-BAND - SLEW 10 P = +90t Y U S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
-12 415+1 (No 8ORESIGHT)
503-XXXXX RANGE RATE
267R VFLOCITY TU BE GAINED CSI
402R OFLTA H
372R TIME CSICH
371R PREDICTED VEL 10 RE GAINED COH
263R OLT-OF-PLANE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATL
-10 COPY RANGE AND ROOT FOR 3RD CSI 8U
SORESIGH ON CSM 41b+1
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
-6
4-18
PRO F 3 BB
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY V06N86E F 06 86 DELTA VIS-LV
AGS(N86) CHART
DELTA VX(LVD
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
507+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
16 85 DELTA VS-BODY
50OR DELTA VX (NOM -0O3)
502R DELTA VZ (NOM 60)
-35 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD 407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS BODY
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS 5OOR 50IR 502R DELTA VX -DELTA VY DELTA VZ-
VERIFY PGNS RESIDUALS N85
DELTA VX(LM)
4-19
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
TPI
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO 507+0 Z-AXIS BORESIGHT
(12426) KEY 34E (TPI)
-36 RESET ET
F 06 37 - amp LOAD TIG TPI FROM DATA PAD (NOM 1250246) PRO
F 06 55 +00000 +02660E +13000 OMEGAT PRO
F 16 45 MARKS TFI -00001
-32 KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
-29 KEY V32E (MARKS = 3)
F 06 37 __ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
RESET ET
410+3 TPI SEARCH ROUTINE 307+04300 DELTA T TRANSFER
4-20
-26 310+02600 TFI TPI
303R THETA AT TPI
267R DELTA VTPI
371R DELTA VTPI + DELTA VTPF
KEY V32E (MARKS = 10)
F 06 37 _ _ _ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VIS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
TEMPIPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40ODEG TO IGODEG F A + B PRESS IND 181 +-3 PSIA
TEMPIPRESS MON SEL - HEL
A + B PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD I 4 2 3 (120 - 190 DEG F)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
RESET ET
-13 310+01300 TFI TPI
303R THETA AT TPI
-12 PRO (FINAL COMP) F 06 37 Z TIG TPIj__
4-21
TRANSMIT TIG OF TPI TO CSM-
PRO F 06 58 HP DELTA VTPI DELTA VTRF
PRO F 06 81 DELTA VS-LV
KEY V9OE (OUT-OF-PLANE)
F 06 16 1 LOAD TIG TPI FROM DATA PAD (NOM 12502461 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT
PRO F 06 81 DELTA VS-LV
COPY CSM YDOT AND LOAD NEGATIVE IN R2 N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 59 DELTA VS LOS
N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI MGA
RESET ET
PRO F 37 BB
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (12000t600)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE)
-10
-6
4-22
F 50 16 DOWNLINK COMPLETE PRO (UPDATE COMPLETE)
400+3 AGS ALIGN 400R (00000 COMPLETE)
-9 277R COPY TGT LOS ANGLE
310+00800
303R THETA AT TPI 410+4 DIRECT TRANSFER AT ET=-8 404+0 405+0 406+0 (MONITOR 470 471 4721
373R TIG TPI
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
KEY 41E (RCS THRUSTING) F 50 18 FOAl ANGLES (REQUEST MNVRI
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
-5 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUS
400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
COMPUTE TPI BU
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
4-23
1685 DELTA VS-BODY
50OR DELTA VX(NOM -115)
502R DELTA VZ(NOM 229)
-Z35 OSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS-BODY
(1250246) BURN +Z
VERIFY AGS RESIDUALS 500R 501R 502R DELTAVX DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
MCC1
KEY V76E (PGNS PULSE) PGNSMODECONT-AUTO
KEY V93E (BEFORE 1ST MARK REINITW MATRIX)
+2 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
4-24
(LOS OF MSFN) S-BAND - SLEW TO P = 90 Y = 0 S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
404+0 405+0 406+0
(MONITOR 470 471 4721
+9 277R COPY TGT LOS ANGLE
+12 PRO (COMPUTE MCC FOR TPI+15I F 06 81 DELTA VS-LV
PRO F 06 59 DELTA VS-LOS
PRO F 16 45 MKS TFI MGA
+13 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUOS
COMPUTE MCC1 BU
PRO F 37 BB
+14 KEY 41E (RCS THRUSTING) F 50 18 FOAL ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+1425 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+15 F 16 85 NULL DELTA VS
PRO F 37 BB
MCC2
KEY V76E (PGNS PULSE)
4-25
PGNS MODE CONT-AUTO
KEY V93E (BEFORE 1ST MARK REINIT W MATRIX)
+16 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
404+0 405+0 406+0 (MONITOR 470 471 47)shy
+24 277R COPY TGT LOS ANGLE
+27 PRO (COMPUTE MCC FORTPI+30) F 06 81 DELTA VS-LV
PRO F 06 59 DELIA VPS-LOS
PRO F 16 45 MKS TFI MGA
+28 277R COPY TGT LOS ANGLE
COPY R RDOT FROM TAPEMETER FOR BUS
COMPUTE MCC2 BU
F 37 BB PRO
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+2925 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+30 F 16 85 NULL DELTA VS
PRO F 37 BB
KEY OOE (P001
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
4-26
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT KEY V34E (TERMINATE)
KEY V37E47E (AVE G) F 16 83 DELTA VIS
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT VERIFY TAPE METER WITH DSKY
BRAKING GATE 30 FPS - 6000 FT 20 FPS - 3000 FT 10 FPS - 1500 FT 5 FPS - 600 FT
RENDEZVOUS
STATION KEEPING
5-1
50 ABORT PROCEDURE
This is a specific AGS nominal abort procedure due to a PGNS failure between insertion and station keeping
51
5-2
Nominal AGS Procedures
ASSUMPTIONS
AFTER INSERTION
I INSERTION COMPLETE (RFSIDUALS NULLED) g PGNS FAILURE BEFORE INSERTION 3 RAUAR NOT LOCKED ON
(UI CoNT-AGS ATlI[uUE MON-AGS(CDR) RATE ERR MON-CNPTR(LMP) ATTITUDE MON-AGS(LMP) SHFITRUN-+5 DEG X-POINTER-HI MULT RADAR IEST Sw-OFF LNb GMbL-OFF ENG ARM-OFF X-IRANSL-2 JETS DEAD BAND-MAX PGNS MODE CONT-OFF THROTJET-JET CB IMU OIR-ON HH MOVE-AUTO rRACK TTCATNANSL-ENABLE(CDR)
AL CPL-ON MODE SL-AGS RNGAL1 MON-RNbRNGRT RAIE ERR MON-RNDZ HDR(CDR) AVl CoNT(3)-PULSE AGS MODE CONT-AUTO ACA4JET-DISABLE(CDR) TTCATRANSL-DISABLE(LMP) ACA4JET-DISABLE(LMP)
bO7+U Z-AXIS BOPESIGHT 400+2 Z-AXIS STEERING PULSE TO NULL AGS ERRORS POINT Z-AXIS IN DIRECTION OF CSM MODE CONT-ATT HOLD ATT CONT(3)-MODE CONTROL O unnr - ZirF
5-3
SLEW PATE - LO
SLEW RR ANT TO OqON FUAI VERIFY MAX SIGNAL STRENGTH RH MOOE-AUTO TRACK NO TRACK LIGHT OFF -
ATT CONT(3h-PULSE
CHECK INSERTION VELOCITY WITH TAPEMETER COMPARE EAPEMETER WITH AGS STATE VECTOR DATA I
17R RANGE(NOM 2642)
440R RANGE RATE(NOM -425l)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
cSI
+3 417+1 (RADAR FILTER INITIALIZED) 41b+l (NO BOHESIGHT) b03-XXXXX RANGE RATE
+5 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGF
41b+1 CSI ROUTINE 373+o2065 CSi TIME 275+03028 TPI TIME 605+0077 COTANGENT OF LOS TO CSM 41b+1 (ONE-HALF OFBITAL-PERIOD) 411+0 HCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT
610R TIME TO CST
43 RESET ET
267R VELOCITY TO BE GAINED CSI
402R FLTA H
371R DFLTA V CDH
5-4
372R DFLTA T CSICDH
-42 415+1 (No BORESIGHT) bO6-xXXXX RANGE RATE
-40 415+1 (NO BORESIGHT)503-XXXXX RANGE RATE dORESIGHT ON CSM
415+1 316+XXXXX RANGE
-37 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE
-15 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE UORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-2 415+1 (No BOHESIGHT) bO3-XXXXX RANGF RATE
i1uR TIME TO CS
RESEF ET
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-30 COPY ROOT FOR 1ST CSI 81J
BORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-t7 415+1 (NO BORFSIGHT) 50-XXxXx RANGF RATE
267R VELOCITY TO HE GAINED CSI
402R LELTA H
371R OFLTA V COH
372R OELTA T CSICDH
-5 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 blb+XXXXX RANGE
-i2 415+1 (No BORESIGHT) 5n3-XXXXX RANGE RATE
415+1 (NO BORESIGHT)
5-5
503-XXXXX RANGF RATE
COPY Roor FOR 2NO CSI BU
bORESIGHT ON CSM 415+1 316+XXXXX RANGE
TEMPPRESS MON SEL - FUEL MAN
A AND 8 PRESS 181 +-3 PIG TEMPPRESS MON SEL - PRPLNT
A AND B TEMP IND 4ODEG 0 IOODEG F A AND B PRFSS IND 181 +-3 PSIA
tEMPPRESS MON SEL - HEL
A AND 8 PRESS IND PSIA
A QUANTITY IND- -- PERCENT RFMAINING
8 QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4p 2 3 (120 - 190 DFG F)
415+1 (NO BORESIGHT)-17 503-XXXXX RANGE RATE
-15 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
(LOS OF MSFN) S-BAND - SLEW 10 P = +90t Y U S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
-12 415+1 (No 8ORESIGHT)
503-XXXXX RANGE RATE
267R VFLOCITY TU BE GAINED CSI
402R OFLTA H
372R TIME CSICH
371R PREDICTED VEL 10 RE GAINED COH
263R OLT-OF-PLANE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATL
-10 COPY RANGE AND ROOT FOR 3RD CSI 8U
SORESIGH ON CSM 41b+1
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
4-19
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
TPI
KEY V76E (PGNS PULSE) PGNS MODE CONT-AUTO 507+0 Z-AXIS BORESIGHT
(12426) KEY 34E (TPI)
-36 RESET ET
F 06 37 - amp LOAD TIG TPI FROM DATA PAD (NOM 1250246) PRO
F 06 55 +00000 +02660E +13000 OMEGAT PRO
F 16 45 MARKS TFI -00001
-32 KEY V93E (REINIT W MATRIX WHEN MARKS = 4)
-29 KEY V32E (MARKS = 3)
F 06 37 __ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
RESET ET
410+3 TPI SEARCH ROUTINE 307+04300 DELTA T TRANSFER
4-20
-26 310+02600 TFI TPI
303R THETA AT TPI
267R DELTA VTPI
371R DELTA VTPI + DELTA VTPF
KEY V32E (MARKS = 10)
F 06 37 _ _ _ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VIS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
TEMPIPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40ODEG TO IGODEG F A + B PRESS IND 181 +-3 PSIA
TEMPIPRESS MON SEL - HEL
A + B PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD I 4 2 3 (120 - 190 DEG F)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
RESET ET
-13 310+01300 TFI TPI
303R THETA AT TPI
-12 PRO (FINAL COMP) F 06 37 Z TIG TPIj__
4-21
TRANSMIT TIG OF TPI TO CSM-
PRO F 06 58 HP DELTA VTPI DELTA VTRF
PRO F 06 81 DELTA VS-LV
KEY V9OE (OUT-OF-PLANE)
F 06 16 1 LOAD TIG TPI FROM DATA PAD (NOM 12502461 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT
PRO F 06 81 DELTA VS-LV
COPY CSM YDOT AND LOAD NEGATIVE IN R2 N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 59 DELTA VS LOS
N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI MGA
RESET ET
PRO F 37 BB
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (12000t600)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE)
-10
-6
4-22
F 50 16 DOWNLINK COMPLETE PRO (UPDATE COMPLETE)
400+3 AGS ALIGN 400R (00000 COMPLETE)
-9 277R COPY TGT LOS ANGLE
310+00800
303R THETA AT TPI 410+4 DIRECT TRANSFER AT ET=-8 404+0 405+0 406+0 (MONITOR 470 471 4721
373R TIG TPI
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
KEY 41E (RCS THRUSTING) F 50 18 FOAl ANGLES (REQUEST MNVRI
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
-5 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUS
400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
COMPUTE TPI BU
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
4-23
1685 DELTA VS-BODY
50OR DELTA VX(NOM -115)
502R DELTA VZ(NOM 229)
-Z35 OSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS-BODY
(1250246) BURN +Z
VERIFY AGS RESIDUALS 500R 501R 502R DELTAVX DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
MCC1
KEY V76E (PGNS PULSE) PGNSMODECONT-AUTO
KEY V93E (BEFORE 1ST MARK REINITW MATRIX)
+2 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
4-24
(LOS OF MSFN) S-BAND - SLEW TO P = 90 Y = 0 S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
404+0 405+0 406+0
(MONITOR 470 471 4721
+9 277R COPY TGT LOS ANGLE
+12 PRO (COMPUTE MCC FOR TPI+15I F 06 81 DELTA VS-LV
PRO F 06 59 DELTA VS-LOS
PRO F 16 45 MKS TFI MGA
+13 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUOS
COMPUTE MCC1 BU
PRO F 37 BB
+14 KEY 41E (RCS THRUSTING) F 50 18 FOAL ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+1425 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+15 F 16 85 NULL DELTA VS
PRO F 37 BB
MCC2
KEY V76E (PGNS PULSE)
4-25
PGNS MODE CONT-AUTO
KEY V93E (BEFORE 1ST MARK REINIT W MATRIX)
+16 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
404+0 405+0 406+0 (MONITOR 470 471 47)shy
+24 277R COPY TGT LOS ANGLE
+27 PRO (COMPUTE MCC FORTPI+30) F 06 81 DELTA VS-LV
PRO F 06 59 DELIA VPS-LOS
PRO F 16 45 MKS TFI MGA
+28 277R COPY TGT LOS ANGLE
COPY R RDOT FROM TAPEMETER FOR BUS
COMPUTE MCC2 BU
F 37 BB PRO
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+2925 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+30 F 16 85 NULL DELTA VS
PRO F 37 BB
KEY OOE (P001
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
4-26
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT KEY V34E (TERMINATE)
KEY V37E47E (AVE G) F 16 83 DELTA VIS
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT VERIFY TAPE METER WITH DSKY
BRAKING GATE 30 FPS - 6000 FT 20 FPS - 3000 FT 10 FPS - 1500 FT 5 FPS - 600 FT
RENDEZVOUS
STATION KEEPING
5-1
50 ABORT PROCEDURE
This is a specific AGS nominal abort procedure due to a PGNS failure between insertion and station keeping
51
5-2
Nominal AGS Procedures
ASSUMPTIONS
AFTER INSERTION
I INSERTION COMPLETE (RFSIDUALS NULLED) g PGNS FAILURE BEFORE INSERTION 3 RAUAR NOT LOCKED ON
(UI CoNT-AGS ATlI[uUE MON-AGS(CDR) RATE ERR MON-CNPTR(LMP) ATTITUDE MON-AGS(LMP) SHFITRUN-+5 DEG X-POINTER-HI MULT RADAR IEST Sw-OFF LNb GMbL-OFF ENG ARM-OFF X-IRANSL-2 JETS DEAD BAND-MAX PGNS MODE CONT-OFF THROTJET-JET CB IMU OIR-ON HH MOVE-AUTO rRACK TTCATNANSL-ENABLE(CDR)
AL CPL-ON MODE SL-AGS RNGAL1 MON-RNbRNGRT RAIE ERR MON-RNDZ HDR(CDR) AVl CoNT(3)-PULSE AGS MODE CONT-AUTO ACA4JET-DISABLE(CDR) TTCATRANSL-DISABLE(LMP) ACA4JET-DISABLE(LMP)
bO7+U Z-AXIS BOPESIGHT 400+2 Z-AXIS STEERING PULSE TO NULL AGS ERRORS POINT Z-AXIS IN DIRECTION OF CSM MODE CONT-ATT HOLD ATT CONT(3)-MODE CONTROL O unnr - ZirF
5-3
SLEW PATE - LO
SLEW RR ANT TO OqON FUAI VERIFY MAX SIGNAL STRENGTH RH MOOE-AUTO TRACK NO TRACK LIGHT OFF -
ATT CONT(3h-PULSE
CHECK INSERTION VELOCITY WITH TAPEMETER COMPARE EAPEMETER WITH AGS STATE VECTOR DATA I
17R RANGE(NOM 2642)
440R RANGE RATE(NOM -425l)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
cSI
+3 417+1 (RADAR FILTER INITIALIZED) 41b+l (NO BOHESIGHT) b03-XXXXX RANGE RATE
+5 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGF
41b+1 CSI ROUTINE 373+o2065 CSi TIME 275+03028 TPI TIME 605+0077 COTANGENT OF LOS TO CSM 41b+1 (ONE-HALF OFBITAL-PERIOD) 411+0 HCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT
610R TIME TO CST
43 RESET ET
267R VELOCITY TO BE GAINED CSI
402R FLTA H
371R DFLTA V CDH
5-4
372R DFLTA T CSICDH
-42 415+1 (No BORESIGHT) bO6-xXXXX RANGE RATE
-40 415+1 (NO BORESIGHT)503-XXXXX RANGE RATE dORESIGHT ON CSM
415+1 316+XXXXX RANGE
-37 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE
-15 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE UORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-2 415+1 (No BOHESIGHT) bO3-XXXXX RANGF RATE
i1uR TIME TO CS
RESEF ET
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-30 COPY ROOT FOR 1ST CSI 81J
BORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-t7 415+1 (NO BORFSIGHT) 50-XXxXx RANGF RATE
267R VELOCITY TO HE GAINED CSI
402R LELTA H
371R OFLTA V COH
372R OELTA T CSICDH
-5 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 blb+XXXXX RANGE
-i2 415+1 (No BORESIGHT) 5n3-XXXXX RANGE RATE
415+1 (NO BORESIGHT)
5-5
503-XXXXX RANGF RATE
COPY Roor FOR 2NO CSI BU
bORESIGHT ON CSM 415+1 316+XXXXX RANGE
TEMPPRESS MON SEL - FUEL MAN
A AND 8 PRESS 181 +-3 PIG TEMPPRESS MON SEL - PRPLNT
A AND B TEMP IND 4ODEG 0 IOODEG F A AND B PRFSS IND 181 +-3 PSIA
tEMPPRESS MON SEL - HEL
A AND 8 PRESS IND PSIA
A QUANTITY IND- -- PERCENT RFMAINING
8 QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4p 2 3 (120 - 190 DFG F)
415+1 (NO BORESIGHT)-17 503-XXXXX RANGE RATE
-15 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
(LOS OF MSFN) S-BAND - SLEW 10 P = +90t Y U S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
-12 415+1 (No 8ORESIGHT)
503-XXXXX RANGE RATE
267R VFLOCITY TU BE GAINED CSI
402R OFLTA H
372R TIME CSICH
371R PREDICTED VEL 10 RE GAINED COH
263R OLT-OF-PLANE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATL
-10 COPY RANGE AND ROOT FOR 3RD CSI 8U
SORESIGH ON CSM 41b+1
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
4-20
-26 310+02600 TFI TPI
303R THETA AT TPI
267R DELTA VTPI
371R DELTA VTPI + DELTA VTPF
KEY V32E (MARKS = 10)
F 06 37 _ _ _ TIG TPI PRO
F 06 58 HP DELTA VTPI DELTA VTPF PRO
F 06 59 DELTA VIS-LOS N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI -00001
TEMPIPRESS MON SEL - FUEL MAN A + B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A + B TEMP IND 40ODEG TO IGODEG F A + B PRESS IND 181 +-3 PSIA
TEMPIPRESS MON SEL - HEL
A + B PRESS IND - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD I 4 2 3 (120 - 190 DEG F)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
RESET ET
-13 310+01300 TFI TPI
303R THETA AT TPI
-12 PRO (FINAL COMP) F 06 37 Z TIG TPIj__
4-21
TRANSMIT TIG OF TPI TO CSM-
PRO F 06 58 HP DELTA VTPI DELTA VTRF
PRO F 06 81 DELTA VS-LV
KEY V9OE (OUT-OF-PLANE)
F 06 16 1 LOAD TIG TPI FROM DATA PAD (NOM 12502461 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT
PRO F 06 81 DELTA VS-LV
COPY CSM YDOT AND LOAD NEGATIVE IN R2 N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 59 DELTA VS LOS
N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI MGA
RESET ET
PRO F 37 BB
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (12000t600)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE)
-10
-6
4-22
F 50 16 DOWNLINK COMPLETE PRO (UPDATE COMPLETE)
400+3 AGS ALIGN 400R (00000 COMPLETE)
-9 277R COPY TGT LOS ANGLE
310+00800
303R THETA AT TPI 410+4 DIRECT TRANSFER AT ET=-8 404+0 405+0 406+0 (MONITOR 470 471 4721
373R TIG TPI
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
KEY 41E (RCS THRUSTING) F 50 18 FOAl ANGLES (REQUEST MNVRI
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
-5 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUS
400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
COMPUTE TPI BU
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
4-23
1685 DELTA VS-BODY
50OR DELTA VX(NOM -115)
502R DELTA VZ(NOM 229)
-Z35 OSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS-BODY
(1250246) BURN +Z
VERIFY AGS RESIDUALS 500R 501R 502R DELTAVX DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
MCC1
KEY V76E (PGNS PULSE) PGNSMODECONT-AUTO
KEY V93E (BEFORE 1ST MARK REINITW MATRIX)
+2 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
4-24
(LOS OF MSFN) S-BAND - SLEW TO P = 90 Y = 0 S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
404+0 405+0 406+0
(MONITOR 470 471 4721
+9 277R COPY TGT LOS ANGLE
+12 PRO (COMPUTE MCC FOR TPI+15I F 06 81 DELTA VS-LV
PRO F 06 59 DELTA VS-LOS
PRO F 16 45 MKS TFI MGA
+13 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUOS
COMPUTE MCC1 BU
PRO F 37 BB
+14 KEY 41E (RCS THRUSTING) F 50 18 FOAL ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+1425 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+15 F 16 85 NULL DELTA VS
PRO F 37 BB
MCC2
KEY V76E (PGNS PULSE)
4-25
PGNS MODE CONT-AUTO
KEY V93E (BEFORE 1ST MARK REINIT W MATRIX)
+16 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
404+0 405+0 406+0 (MONITOR 470 471 47)shy
+24 277R COPY TGT LOS ANGLE
+27 PRO (COMPUTE MCC FORTPI+30) F 06 81 DELTA VS-LV
PRO F 06 59 DELIA VPS-LOS
PRO F 16 45 MKS TFI MGA
+28 277R COPY TGT LOS ANGLE
COPY R RDOT FROM TAPEMETER FOR BUS
COMPUTE MCC2 BU
F 37 BB PRO
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+2925 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+30 F 16 85 NULL DELTA VS
PRO F 37 BB
KEY OOE (P001
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
4-26
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT KEY V34E (TERMINATE)
KEY V37E47E (AVE G) F 16 83 DELTA VIS
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT VERIFY TAPE METER WITH DSKY
BRAKING GATE 30 FPS - 6000 FT 20 FPS - 3000 FT 10 FPS - 1500 FT 5 FPS - 600 FT
RENDEZVOUS
STATION KEEPING
5-1
50 ABORT PROCEDURE
This is a specific AGS nominal abort procedure due to a PGNS failure between insertion and station keeping
51
5-2
Nominal AGS Procedures
ASSUMPTIONS
AFTER INSERTION
I INSERTION COMPLETE (RFSIDUALS NULLED) g PGNS FAILURE BEFORE INSERTION 3 RAUAR NOT LOCKED ON
(UI CoNT-AGS ATlI[uUE MON-AGS(CDR) RATE ERR MON-CNPTR(LMP) ATTITUDE MON-AGS(LMP) SHFITRUN-+5 DEG X-POINTER-HI MULT RADAR IEST Sw-OFF LNb GMbL-OFF ENG ARM-OFF X-IRANSL-2 JETS DEAD BAND-MAX PGNS MODE CONT-OFF THROTJET-JET CB IMU OIR-ON HH MOVE-AUTO rRACK TTCATNANSL-ENABLE(CDR)
AL CPL-ON MODE SL-AGS RNGAL1 MON-RNbRNGRT RAIE ERR MON-RNDZ HDR(CDR) AVl CoNT(3)-PULSE AGS MODE CONT-AUTO ACA4JET-DISABLE(CDR) TTCATRANSL-DISABLE(LMP) ACA4JET-DISABLE(LMP)
bO7+U Z-AXIS BOPESIGHT 400+2 Z-AXIS STEERING PULSE TO NULL AGS ERRORS POINT Z-AXIS IN DIRECTION OF CSM MODE CONT-ATT HOLD ATT CONT(3)-MODE CONTROL O unnr - ZirF
5-3
SLEW PATE - LO
SLEW RR ANT TO OqON FUAI VERIFY MAX SIGNAL STRENGTH RH MOOE-AUTO TRACK NO TRACK LIGHT OFF -
ATT CONT(3h-PULSE
CHECK INSERTION VELOCITY WITH TAPEMETER COMPARE EAPEMETER WITH AGS STATE VECTOR DATA I
17R RANGE(NOM 2642)
440R RANGE RATE(NOM -425l)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
cSI
+3 417+1 (RADAR FILTER INITIALIZED) 41b+l (NO BOHESIGHT) b03-XXXXX RANGE RATE
+5 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGF
41b+1 CSI ROUTINE 373+o2065 CSi TIME 275+03028 TPI TIME 605+0077 COTANGENT OF LOS TO CSM 41b+1 (ONE-HALF OFBITAL-PERIOD) 411+0 HCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT
610R TIME TO CST
43 RESET ET
267R VELOCITY TO BE GAINED CSI
402R FLTA H
371R DFLTA V CDH
5-4
372R DFLTA T CSICDH
-42 415+1 (No BORESIGHT) bO6-xXXXX RANGE RATE
-40 415+1 (NO BORESIGHT)503-XXXXX RANGE RATE dORESIGHT ON CSM
415+1 316+XXXXX RANGE
-37 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE
-15 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE UORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-2 415+1 (No BOHESIGHT) bO3-XXXXX RANGF RATE
i1uR TIME TO CS
RESEF ET
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-30 COPY ROOT FOR 1ST CSI 81J
BORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-t7 415+1 (NO BORFSIGHT) 50-XXxXx RANGF RATE
267R VELOCITY TO HE GAINED CSI
402R LELTA H
371R OFLTA V COH
372R OELTA T CSICDH
-5 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 blb+XXXXX RANGE
-i2 415+1 (No BORESIGHT) 5n3-XXXXX RANGE RATE
415+1 (NO BORESIGHT)
5-5
503-XXXXX RANGF RATE
COPY Roor FOR 2NO CSI BU
bORESIGHT ON CSM 415+1 316+XXXXX RANGE
TEMPPRESS MON SEL - FUEL MAN
A AND 8 PRESS 181 +-3 PIG TEMPPRESS MON SEL - PRPLNT
A AND B TEMP IND 4ODEG 0 IOODEG F A AND B PRFSS IND 181 +-3 PSIA
tEMPPRESS MON SEL - HEL
A AND 8 PRESS IND PSIA
A QUANTITY IND- -- PERCENT RFMAINING
8 QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4p 2 3 (120 - 190 DFG F)
415+1 (NO BORESIGHT)-17 503-XXXXX RANGE RATE
-15 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
(LOS OF MSFN) S-BAND - SLEW 10 P = +90t Y U S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
-12 415+1 (No 8ORESIGHT)
503-XXXXX RANGE RATE
267R VFLOCITY TU BE GAINED CSI
402R OFLTA H
372R TIME CSICH
371R PREDICTED VEL 10 RE GAINED COH
263R OLT-OF-PLANE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATL
-10 COPY RANGE AND ROOT FOR 3RD CSI 8U
SORESIGH ON CSM 41b+1
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
4-21
TRANSMIT TIG OF TPI TO CSM-
PRO F 06 58 HP DELTA VTPI DELTA VTRF
PRO F 06 81 DELTA VS-LV
KEY V9OE (OUT-OF-PLANE)
F 06 16 1 LOAD TIG TPI FROM DATA PAD (NOM 12502461 PRO
F 06 90 Y YDOT PSI N90 CSM
YDOT
PRO F 06 81 DELTA VS-LV
COPY CSM YDOT AND LOAD NEGATIVE IN R2 N81
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
PRO F 06 59 DELTA VS LOS
N59
DELTA V FA
DELTA V RL
DELTA V DU
PRO F 16 45 MKS TFI MGA
RESET ET
PRO F 37 BB
KEY V47E (INITIALIZE AGS) F 06 16 GET OF AGS 0 TIME (12000t600)
TELEMETRY PCM SW-HI 414+1 UPDATE AGS PRO
414R (00000 COMPLETE)
-10
-6
4-22
F 50 16 DOWNLINK COMPLETE PRO (UPDATE COMPLETE)
400+3 AGS ALIGN 400R (00000 COMPLETE)
-9 277R COPY TGT LOS ANGLE
310+00800
303R THETA AT TPI 410+4 DIRECT TRANSFER AT ET=-8 404+0 405+0 406+0 (MONITOR 470 471 4721
373R TIG TPI
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
KEY 41E (RCS THRUSTING) F 50 18 FOAl ANGLES (REQUEST MNVRI
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
-5 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUS
400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
COMPUTE TPI BU
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
4-23
1685 DELTA VS-BODY
50OR DELTA VX(NOM -115)
502R DELTA VZ(NOM 229)
-Z35 OSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS-BODY
(1250246) BURN +Z
VERIFY AGS RESIDUALS 500R 501R 502R DELTAVX DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
MCC1
KEY V76E (PGNS PULSE) PGNSMODECONT-AUTO
KEY V93E (BEFORE 1ST MARK REINITW MATRIX)
+2 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
4-24
(LOS OF MSFN) S-BAND - SLEW TO P = 90 Y = 0 S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
404+0 405+0 406+0
(MONITOR 470 471 4721
+9 277R COPY TGT LOS ANGLE
+12 PRO (COMPUTE MCC FOR TPI+15I F 06 81 DELTA VS-LV
PRO F 06 59 DELTA VS-LOS
PRO F 16 45 MKS TFI MGA
+13 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUOS
COMPUTE MCC1 BU
PRO F 37 BB
+14 KEY 41E (RCS THRUSTING) F 50 18 FOAL ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+1425 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+15 F 16 85 NULL DELTA VS
PRO F 37 BB
MCC2
KEY V76E (PGNS PULSE)
4-25
PGNS MODE CONT-AUTO
KEY V93E (BEFORE 1ST MARK REINIT W MATRIX)
+16 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
404+0 405+0 406+0 (MONITOR 470 471 47)shy
+24 277R COPY TGT LOS ANGLE
+27 PRO (COMPUTE MCC FORTPI+30) F 06 81 DELTA VS-LV
PRO F 06 59 DELIA VPS-LOS
PRO F 16 45 MKS TFI MGA
+28 277R COPY TGT LOS ANGLE
COPY R RDOT FROM TAPEMETER FOR BUS
COMPUTE MCC2 BU
F 37 BB PRO
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+2925 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+30 F 16 85 NULL DELTA VS
PRO F 37 BB
KEY OOE (P001
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
4-26
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT KEY V34E (TERMINATE)
KEY V37E47E (AVE G) F 16 83 DELTA VIS
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT VERIFY TAPE METER WITH DSKY
BRAKING GATE 30 FPS - 6000 FT 20 FPS - 3000 FT 10 FPS - 1500 FT 5 FPS - 600 FT
RENDEZVOUS
STATION KEEPING
5-1
50 ABORT PROCEDURE
This is a specific AGS nominal abort procedure due to a PGNS failure between insertion and station keeping
51
5-2
Nominal AGS Procedures
ASSUMPTIONS
AFTER INSERTION
I INSERTION COMPLETE (RFSIDUALS NULLED) g PGNS FAILURE BEFORE INSERTION 3 RAUAR NOT LOCKED ON
(UI CoNT-AGS ATlI[uUE MON-AGS(CDR) RATE ERR MON-CNPTR(LMP) ATTITUDE MON-AGS(LMP) SHFITRUN-+5 DEG X-POINTER-HI MULT RADAR IEST Sw-OFF LNb GMbL-OFF ENG ARM-OFF X-IRANSL-2 JETS DEAD BAND-MAX PGNS MODE CONT-OFF THROTJET-JET CB IMU OIR-ON HH MOVE-AUTO rRACK TTCATNANSL-ENABLE(CDR)
AL CPL-ON MODE SL-AGS RNGAL1 MON-RNbRNGRT RAIE ERR MON-RNDZ HDR(CDR) AVl CoNT(3)-PULSE AGS MODE CONT-AUTO ACA4JET-DISABLE(CDR) TTCATRANSL-DISABLE(LMP) ACA4JET-DISABLE(LMP)
bO7+U Z-AXIS BOPESIGHT 400+2 Z-AXIS STEERING PULSE TO NULL AGS ERRORS POINT Z-AXIS IN DIRECTION OF CSM MODE CONT-ATT HOLD ATT CONT(3)-MODE CONTROL O unnr - ZirF
5-3
SLEW PATE - LO
SLEW RR ANT TO OqON FUAI VERIFY MAX SIGNAL STRENGTH RH MOOE-AUTO TRACK NO TRACK LIGHT OFF -
ATT CONT(3h-PULSE
CHECK INSERTION VELOCITY WITH TAPEMETER COMPARE EAPEMETER WITH AGS STATE VECTOR DATA I
17R RANGE(NOM 2642)
440R RANGE RATE(NOM -425l)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
cSI
+3 417+1 (RADAR FILTER INITIALIZED) 41b+l (NO BOHESIGHT) b03-XXXXX RANGE RATE
+5 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGF
41b+1 CSI ROUTINE 373+o2065 CSi TIME 275+03028 TPI TIME 605+0077 COTANGENT OF LOS TO CSM 41b+1 (ONE-HALF OFBITAL-PERIOD) 411+0 HCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT
610R TIME TO CST
43 RESET ET
267R VELOCITY TO BE GAINED CSI
402R FLTA H
371R DFLTA V CDH
5-4
372R DFLTA T CSICDH
-42 415+1 (No BORESIGHT) bO6-xXXXX RANGE RATE
-40 415+1 (NO BORESIGHT)503-XXXXX RANGE RATE dORESIGHT ON CSM
415+1 316+XXXXX RANGE
-37 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE
-15 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE UORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-2 415+1 (No BOHESIGHT) bO3-XXXXX RANGF RATE
i1uR TIME TO CS
RESEF ET
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-30 COPY ROOT FOR 1ST CSI 81J
BORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-t7 415+1 (NO BORFSIGHT) 50-XXxXx RANGF RATE
267R VELOCITY TO HE GAINED CSI
402R LELTA H
371R OFLTA V COH
372R OELTA T CSICDH
-5 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 blb+XXXXX RANGE
-i2 415+1 (No BORESIGHT) 5n3-XXXXX RANGE RATE
415+1 (NO BORESIGHT)
5-5
503-XXXXX RANGF RATE
COPY Roor FOR 2NO CSI BU
bORESIGHT ON CSM 415+1 316+XXXXX RANGE
TEMPPRESS MON SEL - FUEL MAN
A AND 8 PRESS 181 +-3 PIG TEMPPRESS MON SEL - PRPLNT
A AND B TEMP IND 4ODEG 0 IOODEG F A AND B PRFSS IND 181 +-3 PSIA
tEMPPRESS MON SEL - HEL
A AND 8 PRESS IND PSIA
A QUANTITY IND- -- PERCENT RFMAINING
8 QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4p 2 3 (120 - 190 DFG F)
415+1 (NO BORESIGHT)-17 503-XXXXX RANGE RATE
-15 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
(LOS OF MSFN) S-BAND - SLEW 10 P = +90t Y U S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
-12 415+1 (No 8ORESIGHT)
503-XXXXX RANGE RATE
267R VFLOCITY TU BE GAINED CSI
402R OFLTA H
372R TIME CSICH
371R PREDICTED VEL 10 RE GAINED COH
263R OLT-OF-PLANE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATL
-10 COPY RANGE AND ROOT FOR 3RD CSI 8U
SORESIGH ON CSM 41b+1
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
-6
4-22
F 50 16 DOWNLINK COMPLETE PRO (UPDATE COMPLETE)
400+3 AGS ALIGN 400R (00000 COMPLETE)
-9 277R COPY TGT LOS ANGLE
310+00800
303R THETA AT TPI 410+4 DIRECT TRANSFER AT ET=-8 404+0 405+0 406+0 (MONITOR 470 471 4721
373R TIG TPI
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
KEY 41E (RCS THRUSTING) F 50 18 FOAl ANGLES (REQUEST MNVRI
ENTR (BYPASS MNVR)
16 85 DELTA VS-BODY
KEY VO6NB6E DELTA VS-LV F 06 86 DELTA VS-LV
AGS(N86) CHART
DELTA VX(LV)
DELTA VY(LV)
DELTA VZ(LV)
KEY RELEASE
-5 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUS
400+2 Z-AXIS STEERING 410+5 EXTERNAL DELTA V 450 451 452 LOAD 407+0 ROTATE EXTERNAL DELTA V RF
COMPUTE TPI BU
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
4-23
1685 DELTA VS-BODY
50OR DELTA VX(NOM -115)
502R DELTA VZ(NOM 229)
-Z35 OSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS-BODY
(1250246) BURN +Z
VERIFY AGS RESIDUALS 500R 501R 502R DELTAVX DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
MCC1
KEY V76E (PGNS PULSE) PGNSMODECONT-AUTO
KEY V93E (BEFORE 1ST MARK REINITW MATRIX)
+2 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
4-24
(LOS OF MSFN) S-BAND - SLEW TO P = 90 Y = 0 S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
404+0 405+0 406+0
(MONITOR 470 471 4721
+9 277R COPY TGT LOS ANGLE
+12 PRO (COMPUTE MCC FOR TPI+15I F 06 81 DELTA VS-LV
PRO F 06 59 DELTA VS-LOS
PRO F 16 45 MKS TFI MGA
+13 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUOS
COMPUTE MCC1 BU
PRO F 37 BB
+14 KEY 41E (RCS THRUSTING) F 50 18 FOAL ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+1425 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+15 F 16 85 NULL DELTA VS
PRO F 37 BB
MCC2
KEY V76E (PGNS PULSE)
4-25
PGNS MODE CONT-AUTO
KEY V93E (BEFORE 1ST MARK REINIT W MATRIX)
+16 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
404+0 405+0 406+0 (MONITOR 470 471 47)shy
+24 277R COPY TGT LOS ANGLE
+27 PRO (COMPUTE MCC FORTPI+30) F 06 81 DELTA VS-LV
PRO F 06 59 DELIA VPS-LOS
PRO F 16 45 MKS TFI MGA
+28 277R COPY TGT LOS ANGLE
COPY R RDOT FROM TAPEMETER FOR BUS
COMPUTE MCC2 BU
F 37 BB PRO
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+2925 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+30 F 16 85 NULL DELTA VS
PRO F 37 BB
KEY OOE (P001
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
4-26
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT KEY V34E (TERMINATE)
KEY V37E47E (AVE G) F 16 83 DELTA VIS
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT VERIFY TAPE METER WITH DSKY
BRAKING GATE 30 FPS - 6000 FT 20 FPS - 3000 FT 10 FPS - 1500 FT 5 FPS - 600 FT
RENDEZVOUS
STATION KEEPING
5-1
50 ABORT PROCEDURE
This is a specific AGS nominal abort procedure due to a PGNS failure between insertion and station keeping
51
5-2
Nominal AGS Procedures
ASSUMPTIONS
AFTER INSERTION
I INSERTION COMPLETE (RFSIDUALS NULLED) g PGNS FAILURE BEFORE INSERTION 3 RAUAR NOT LOCKED ON
(UI CoNT-AGS ATlI[uUE MON-AGS(CDR) RATE ERR MON-CNPTR(LMP) ATTITUDE MON-AGS(LMP) SHFITRUN-+5 DEG X-POINTER-HI MULT RADAR IEST Sw-OFF LNb GMbL-OFF ENG ARM-OFF X-IRANSL-2 JETS DEAD BAND-MAX PGNS MODE CONT-OFF THROTJET-JET CB IMU OIR-ON HH MOVE-AUTO rRACK TTCATNANSL-ENABLE(CDR)
AL CPL-ON MODE SL-AGS RNGAL1 MON-RNbRNGRT RAIE ERR MON-RNDZ HDR(CDR) AVl CoNT(3)-PULSE AGS MODE CONT-AUTO ACA4JET-DISABLE(CDR) TTCATRANSL-DISABLE(LMP) ACA4JET-DISABLE(LMP)
bO7+U Z-AXIS BOPESIGHT 400+2 Z-AXIS STEERING PULSE TO NULL AGS ERRORS POINT Z-AXIS IN DIRECTION OF CSM MODE CONT-ATT HOLD ATT CONT(3)-MODE CONTROL O unnr - ZirF
5-3
SLEW PATE - LO
SLEW RR ANT TO OqON FUAI VERIFY MAX SIGNAL STRENGTH RH MOOE-AUTO TRACK NO TRACK LIGHT OFF -
ATT CONT(3h-PULSE
CHECK INSERTION VELOCITY WITH TAPEMETER COMPARE EAPEMETER WITH AGS STATE VECTOR DATA I
17R RANGE(NOM 2642)
440R RANGE RATE(NOM -425l)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
cSI
+3 417+1 (RADAR FILTER INITIALIZED) 41b+l (NO BOHESIGHT) b03-XXXXX RANGE RATE
+5 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGF
41b+1 CSI ROUTINE 373+o2065 CSi TIME 275+03028 TPI TIME 605+0077 COTANGENT OF LOS TO CSM 41b+1 (ONE-HALF OFBITAL-PERIOD) 411+0 HCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT
610R TIME TO CST
43 RESET ET
267R VELOCITY TO BE GAINED CSI
402R FLTA H
371R DFLTA V CDH
5-4
372R DFLTA T CSICDH
-42 415+1 (No BORESIGHT) bO6-xXXXX RANGE RATE
-40 415+1 (NO BORESIGHT)503-XXXXX RANGE RATE dORESIGHT ON CSM
415+1 316+XXXXX RANGE
-37 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE
-15 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE UORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-2 415+1 (No BOHESIGHT) bO3-XXXXX RANGF RATE
i1uR TIME TO CS
RESEF ET
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-30 COPY ROOT FOR 1ST CSI 81J
BORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-t7 415+1 (NO BORFSIGHT) 50-XXxXx RANGF RATE
267R VELOCITY TO HE GAINED CSI
402R LELTA H
371R OFLTA V COH
372R OELTA T CSICDH
-5 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 blb+XXXXX RANGE
-i2 415+1 (No BORESIGHT) 5n3-XXXXX RANGE RATE
415+1 (NO BORESIGHT)
5-5
503-XXXXX RANGF RATE
COPY Roor FOR 2NO CSI BU
bORESIGHT ON CSM 415+1 316+XXXXX RANGE
TEMPPRESS MON SEL - FUEL MAN
A AND 8 PRESS 181 +-3 PIG TEMPPRESS MON SEL - PRPLNT
A AND B TEMP IND 4ODEG 0 IOODEG F A AND B PRFSS IND 181 +-3 PSIA
tEMPPRESS MON SEL - HEL
A AND 8 PRESS IND PSIA
A QUANTITY IND- -- PERCENT RFMAINING
8 QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4p 2 3 (120 - 190 DFG F)
415+1 (NO BORESIGHT)-17 503-XXXXX RANGE RATE
-15 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
(LOS OF MSFN) S-BAND - SLEW 10 P = +90t Y U S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
-12 415+1 (No 8ORESIGHT)
503-XXXXX RANGE RATE
267R VFLOCITY TU BE GAINED CSI
402R OFLTA H
372R TIME CSICH
371R PREDICTED VEL 10 RE GAINED COH
263R OLT-OF-PLANE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATL
-10 COPY RANGE AND ROOT FOR 3RD CSI 8U
SORESIGH ON CSM 41b+1
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
4-23
1685 DELTA VS-BODY
50OR DELTA VX(NOM -115)
502R DELTA VZ(NOM 229)
-Z35 OSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
F 16 85 DELTA VS-BODY
(1250246) BURN +Z
VERIFY AGS RESIDUALS 500R 501R 502R DELTAVX DELTA VY DELTA VZ
VERIFY PGNS RESIDUALS
N85
DELTA VX(LM)
DELTA VY(LM)
DELTA VZ(LM)
PRO F 37 BB
MCC1
KEY V76E (PGNS PULSE) PGNSMODECONT-AUTO
KEY V93E (BEFORE 1ST MARK REINITW MATRIX)
+2 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
4-24
(LOS OF MSFN) S-BAND - SLEW TO P = 90 Y = 0 S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
404+0 405+0 406+0
(MONITOR 470 471 4721
+9 277R COPY TGT LOS ANGLE
+12 PRO (COMPUTE MCC FOR TPI+15I F 06 81 DELTA VS-LV
PRO F 06 59 DELTA VS-LOS
PRO F 16 45 MKS TFI MGA
+13 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUOS
COMPUTE MCC1 BU
PRO F 37 BB
+14 KEY 41E (RCS THRUSTING) F 50 18 FOAL ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+1425 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+15 F 16 85 NULL DELTA VS
PRO F 37 BB
MCC2
KEY V76E (PGNS PULSE)
4-25
PGNS MODE CONT-AUTO
KEY V93E (BEFORE 1ST MARK REINIT W MATRIX)
+16 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
404+0 405+0 406+0 (MONITOR 470 471 47)shy
+24 277R COPY TGT LOS ANGLE
+27 PRO (COMPUTE MCC FORTPI+30) F 06 81 DELTA VS-LV
PRO F 06 59 DELIA VPS-LOS
PRO F 16 45 MKS TFI MGA
+28 277R COPY TGT LOS ANGLE
COPY R RDOT FROM TAPEMETER FOR BUS
COMPUTE MCC2 BU
F 37 BB PRO
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+2925 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+30 F 16 85 NULL DELTA VS
PRO F 37 BB
KEY OOE (P001
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
4-26
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT KEY V34E (TERMINATE)
KEY V37E47E (AVE G) F 16 83 DELTA VIS
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT VERIFY TAPE METER WITH DSKY
BRAKING GATE 30 FPS - 6000 FT 20 FPS - 3000 FT 10 FPS - 1500 FT 5 FPS - 600 FT
RENDEZVOUS
STATION KEEPING
5-1
50 ABORT PROCEDURE
This is a specific AGS nominal abort procedure due to a PGNS failure between insertion and station keeping
51
5-2
Nominal AGS Procedures
ASSUMPTIONS
AFTER INSERTION
I INSERTION COMPLETE (RFSIDUALS NULLED) g PGNS FAILURE BEFORE INSERTION 3 RAUAR NOT LOCKED ON
(UI CoNT-AGS ATlI[uUE MON-AGS(CDR) RATE ERR MON-CNPTR(LMP) ATTITUDE MON-AGS(LMP) SHFITRUN-+5 DEG X-POINTER-HI MULT RADAR IEST Sw-OFF LNb GMbL-OFF ENG ARM-OFF X-IRANSL-2 JETS DEAD BAND-MAX PGNS MODE CONT-OFF THROTJET-JET CB IMU OIR-ON HH MOVE-AUTO rRACK TTCATNANSL-ENABLE(CDR)
AL CPL-ON MODE SL-AGS RNGAL1 MON-RNbRNGRT RAIE ERR MON-RNDZ HDR(CDR) AVl CoNT(3)-PULSE AGS MODE CONT-AUTO ACA4JET-DISABLE(CDR) TTCATRANSL-DISABLE(LMP) ACA4JET-DISABLE(LMP)
bO7+U Z-AXIS BOPESIGHT 400+2 Z-AXIS STEERING PULSE TO NULL AGS ERRORS POINT Z-AXIS IN DIRECTION OF CSM MODE CONT-ATT HOLD ATT CONT(3)-MODE CONTROL O unnr - ZirF
5-3
SLEW PATE - LO
SLEW RR ANT TO OqON FUAI VERIFY MAX SIGNAL STRENGTH RH MOOE-AUTO TRACK NO TRACK LIGHT OFF -
ATT CONT(3h-PULSE
CHECK INSERTION VELOCITY WITH TAPEMETER COMPARE EAPEMETER WITH AGS STATE VECTOR DATA I
17R RANGE(NOM 2642)
440R RANGE RATE(NOM -425l)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
cSI
+3 417+1 (RADAR FILTER INITIALIZED) 41b+l (NO BOHESIGHT) b03-XXXXX RANGE RATE
+5 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGF
41b+1 CSI ROUTINE 373+o2065 CSi TIME 275+03028 TPI TIME 605+0077 COTANGENT OF LOS TO CSM 41b+1 (ONE-HALF OFBITAL-PERIOD) 411+0 HCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT
610R TIME TO CST
43 RESET ET
267R VELOCITY TO BE GAINED CSI
402R FLTA H
371R DFLTA V CDH
5-4
372R DFLTA T CSICDH
-42 415+1 (No BORESIGHT) bO6-xXXXX RANGE RATE
-40 415+1 (NO BORESIGHT)503-XXXXX RANGE RATE dORESIGHT ON CSM
415+1 316+XXXXX RANGE
-37 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE
-15 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE UORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-2 415+1 (No BOHESIGHT) bO3-XXXXX RANGF RATE
i1uR TIME TO CS
RESEF ET
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-30 COPY ROOT FOR 1ST CSI 81J
BORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-t7 415+1 (NO BORFSIGHT) 50-XXxXx RANGF RATE
267R VELOCITY TO HE GAINED CSI
402R LELTA H
371R OFLTA V COH
372R OELTA T CSICDH
-5 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 blb+XXXXX RANGE
-i2 415+1 (No BORESIGHT) 5n3-XXXXX RANGE RATE
415+1 (NO BORESIGHT)
5-5
503-XXXXX RANGF RATE
COPY Roor FOR 2NO CSI BU
bORESIGHT ON CSM 415+1 316+XXXXX RANGE
TEMPPRESS MON SEL - FUEL MAN
A AND 8 PRESS 181 +-3 PIG TEMPPRESS MON SEL - PRPLNT
A AND B TEMP IND 4ODEG 0 IOODEG F A AND B PRFSS IND 181 +-3 PSIA
tEMPPRESS MON SEL - HEL
A AND 8 PRESS IND PSIA
A QUANTITY IND- -- PERCENT RFMAINING
8 QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4p 2 3 (120 - 190 DFG F)
415+1 (NO BORESIGHT)-17 503-XXXXX RANGE RATE
-15 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
(LOS OF MSFN) S-BAND - SLEW 10 P = +90t Y U S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
-12 415+1 (No 8ORESIGHT)
503-XXXXX RANGE RATE
267R VFLOCITY TU BE GAINED CSI
402R OFLTA H
372R TIME CSICH
371R PREDICTED VEL 10 RE GAINED COH
263R OLT-OF-PLANE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATL
-10 COPY RANGE AND ROOT FOR 3RD CSI 8U
SORESIGH ON CSM 41b+1
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
4-24
(LOS OF MSFN) S-BAND - SLEW TO P = 90 Y = 0 S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
404+0 405+0 406+0
(MONITOR 470 471 4721
+9 277R COPY TGT LOS ANGLE
+12 PRO (COMPUTE MCC FOR TPI+15I F 06 81 DELTA VS-LV
PRO F 06 59 DELTA VS-LOS
PRO F 16 45 MKS TFI MGA
+13 277R COPY TGT LOS ANGLE
COPY R ROOT FROM TAPE METER FOR BUOS
COMPUTE MCC1 BU
PRO F 37 BB
+14 KEY 41E (RCS THRUSTING) F 50 18 FOAL ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+1425 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+15 F 16 85 NULL DELTA VS
PRO F 37 BB
MCC2
KEY V76E (PGNS PULSE)
4-25
PGNS MODE CONT-AUTO
KEY V93E (BEFORE 1ST MARK REINIT W MATRIX)
+16 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
404+0 405+0 406+0 (MONITOR 470 471 47)shy
+24 277R COPY TGT LOS ANGLE
+27 PRO (COMPUTE MCC FORTPI+30) F 06 81 DELTA VS-LV
PRO F 06 59 DELIA VPS-LOS
PRO F 16 45 MKS TFI MGA
+28 277R COPY TGT LOS ANGLE
COPY R RDOT FROM TAPEMETER FOR BUS
COMPUTE MCC2 BU
F 37 BB PRO
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+2925 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+30 F 16 85 NULL DELTA VS
PRO F 37 BB
KEY OOE (P001
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
4-26
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT KEY V34E (TERMINATE)
KEY V37E47E (AVE G) F 16 83 DELTA VIS
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT VERIFY TAPE METER WITH DSKY
BRAKING GATE 30 FPS - 6000 FT 20 FPS - 3000 FT 10 FPS - 1500 FT 5 FPS - 600 FT
RENDEZVOUS
STATION KEEPING
5-1
50 ABORT PROCEDURE
This is a specific AGS nominal abort procedure due to a PGNS failure between insertion and station keeping
51
5-2
Nominal AGS Procedures
ASSUMPTIONS
AFTER INSERTION
I INSERTION COMPLETE (RFSIDUALS NULLED) g PGNS FAILURE BEFORE INSERTION 3 RAUAR NOT LOCKED ON
(UI CoNT-AGS ATlI[uUE MON-AGS(CDR) RATE ERR MON-CNPTR(LMP) ATTITUDE MON-AGS(LMP) SHFITRUN-+5 DEG X-POINTER-HI MULT RADAR IEST Sw-OFF LNb GMbL-OFF ENG ARM-OFF X-IRANSL-2 JETS DEAD BAND-MAX PGNS MODE CONT-OFF THROTJET-JET CB IMU OIR-ON HH MOVE-AUTO rRACK TTCATNANSL-ENABLE(CDR)
AL CPL-ON MODE SL-AGS RNGAL1 MON-RNbRNGRT RAIE ERR MON-RNDZ HDR(CDR) AVl CoNT(3)-PULSE AGS MODE CONT-AUTO ACA4JET-DISABLE(CDR) TTCATRANSL-DISABLE(LMP) ACA4JET-DISABLE(LMP)
bO7+U Z-AXIS BOPESIGHT 400+2 Z-AXIS STEERING PULSE TO NULL AGS ERRORS POINT Z-AXIS IN DIRECTION OF CSM MODE CONT-ATT HOLD ATT CONT(3)-MODE CONTROL O unnr - ZirF
5-3
SLEW PATE - LO
SLEW RR ANT TO OqON FUAI VERIFY MAX SIGNAL STRENGTH RH MOOE-AUTO TRACK NO TRACK LIGHT OFF -
ATT CONT(3h-PULSE
CHECK INSERTION VELOCITY WITH TAPEMETER COMPARE EAPEMETER WITH AGS STATE VECTOR DATA I
17R RANGE(NOM 2642)
440R RANGE RATE(NOM -425l)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
cSI
+3 417+1 (RADAR FILTER INITIALIZED) 41b+l (NO BOHESIGHT) b03-XXXXX RANGE RATE
+5 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGF
41b+1 CSI ROUTINE 373+o2065 CSi TIME 275+03028 TPI TIME 605+0077 COTANGENT OF LOS TO CSM 41b+1 (ONE-HALF OFBITAL-PERIOD) 411+0 HCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT
610R TIME TO CST
43 RESET ET
267R VELOCITY TO BE GAINED CSI
402R FLTA H
371R DFLTA V CDH
5-4
372R DFLTA T CSICDH
-42 415+1 (No BORESIGHT) bO6-xXXXX RANGE RATE
-40 415+1 (NO BORESIGHT)503-XXXXX RANGE RATE dORESIGHT ON CSM
415+1 316+XXXXX RANGE
-37 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE
-15 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE UORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-2 415+1 (No BOHESIGHT) bO3-XXXXX RANGF RATE
i1uR TIME TO CS
RESEF ET
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-30 COPY ROOT FOR 1ST CSI 81J
BORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-t7 415+1 (NO BORFSIGHT) 50-XXxXx RANGF RATE
267R VELOCITY TO HE GAINED CSI
402R LELTA H
371R OFLTA V COH
372R OELTA T CSICDH
-5 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 blb+XXXXX RANGE
-i2 415+1 (No BORESIGHT) 5n3-XXXXX RANGE RATE
415+1 (NO BORESIGHT)
5-5
503-XXXXX RANGF RATE
COPY Roor FOR 2NO CSI BU
bORESIGHT ON CSM 415+1 316+XXXXX RANGE
TEMPPRESS MON SEL - FUEL MAN
A AND 8 PRESS 181 +-3 PIG TEMPPRESS MON SEL - PRPLNT
A AND B TEMP IND 4ODEG 0 IOODEG F A AND B PRFSS IND 181 +-3 PSIA
tEMPPRESS MON SEL - HEL
A AND 8 PRESS IND PSIA
A QUANTITY IND- -- PERCENT RFMAINING
8 QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4p 2 3 (120 - 190 DFG F)
415+1 (NO BORESIGHT)-17 503-XXXXX RANGE RATE
-15 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
(LOS OF MSFN) S-BAND - SLEW 10 P = +90t Y U S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
-12 415+1 (No 8ORESIGHT)
503-XXXXX RANGE RATE
267R VFLOCITY TU BE GAINED CSI
402R OFLTA H
372R TIME CSICH
371R PREDICTED VEL 10 RE GAINED COH
263R OLT-OF-PLANE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATL
-10 COPY RANGE AND ROOT FOR 3RD CSI 8U
SORESIGH ON CSM 41b+1
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
4-25
PGNS MODE CONT-AUTO
KEY V93E (BEFORE 1ST MARK REINIT W MATRIX)
+16 KEY 35E (TPM PRE-THRUST) F 16 45 MKS TFI -00001
404+0 405+0 406+0 (MONITOR 470 471 47)shy
+24 277R COPY TGT LOS ANGLE
+27 PRO (COMPUTE MCC FORTPI+30) F 06 81 DELTA VS-LV
PRO F 06 59 DELIA VPS-LOS
PRO F 16 45 MKS TFI MGA
+28 277R COPY TGT LOS ANGLE
COPY R RDOT FROM TAPEMETER FOR BUS
COMPUTE MCC2 BU
F 37 BB PRO
KEY 41E (RCS THRUSTING) F 50 18 FDAI ANGLES (REQUEST MNVR)
ENTR (BYPASS MNVR) 16 85 DELTA VS-BODY
+2925 DSKY BLANKS
KEY V77E (ATT HOLD) PGNS MODE CONT-ATT HOLD AGS MODE CONT-ATT HOLD
407+1 FREEZE EXTERNAL DELTA V
+30 F 16 85 NULL DELTA VS
PRO F 37 BB
KEY OOE (P001
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
4-26
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT KEY V34E (TERMINATE)
KEY V37E47E (AVE G) F 16 83 DELTA VIS
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT VERIFY TAPE METER WITH DSKY
BRAKING GATE 30 FPS - 6000 FT 20 FPS - 3000 FT 10 FPS - 1500 FT 5 FPS - 600 FT
RENDEZVOUS
STATION KEEPING
5-1
50 ABORT PROCEDURE
This is a specific AGS nominal abort procedure due to a PGNS failure between insertion and station keeping
51
5-2
Nominal AGS Procedures
ASSUMPTIONS
AFTER INSERTION
I INSERTION COMPLETE (RFSIDUALS NULLED) g PGNS FAILURE BEFORE INSERTION 3 RAUAR NOT LOCKED ON
(UI CoNT-AGS ATlI[uUE MON-AGS(CDR) RATE ERR MON-CNPTR(LMP) ATTITUDE MON-AGS(LMP) SHFITRUN-+5 DEG X-POINTER-HI MULT RADAR IEST Sw-OFF LNb GMbL-OFF ENG ARM-OFF X-IRANSL-2 JETS DEAD BAND-MAX PGNS MODE CONT-OFF THROTJET-JET CB IMU OIR-ON HH MOVE-AUTO rRACK TTCATNANSL-ENABLE(CDR)
AL CPL-ON MODE SL-AGS RNGAL1 MON-RNbRNGRT RAIE ERR MON-RNDZ HDR(CDR) AVl CoNT(3)-PULSE AGS MODE CONT-AUTO ACA4JET-DISABLE(CDR) TTCATRANSL-DISABLE(LMP) ACA4JET-DISABLE(LMP)
bO7+U Z-AXIS BOPESIGHT 400+2 Z-AXIS STEERING PULSE TO NULL AGS ERRORS POINT Z-AXIS IN DIRECTION OF CSM MODE CONT-ATT HOLD ATT CONT(3)-MODE CONTROL O unnr - ZirF
5-3
SLEW PATE - LO
SLEW RR ANT TO OqON FUAI VERIFY MAX SIGNAL STRENGTH RH MOOE-AUTO TRACK NO TRACK LIGHT OFF -
ATT CONT(3h-PULSE
CHECK INSERTION VELOCITY WITH TAPEMETER COMPARE EAPEMETER WITH AGS STATE VECTOR DATA I
17R RANGE(NOM 2642)
440R RANGE RATE(NOM -425l)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
cSI
+3 417+1 (RADAR FILTER INITIALIZED) 41b+l (NO BOHESIGHT) b03-XXXXX RANGE RATE
+5 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGF
41b+1 CSI ROUTINE 373+o2065 CSi TIME 275+03028 TPI TIME 605+0077 COTANGENT OF LOS TO CSM 41b+1 (ONE-HALF OFBITAL-PERIOD) 411+0 HCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT
610R TIME TO CST
43 RESET ET
267R VELOCITY TO BE GAINED CSI
402R FLTA H
371R DFLTA V CDH
5-4
372R DFLTA T CSICDH
-42 415+1 (No BORESIGHT) bO6-xXXXX RANGE RATE
-40 415+1 (NO BORESIGHT)503-XXXXX RANGE RATE dORESIGHT ON CSM
415+1 316+XXXXX RANGE
-37 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE
-15 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE UORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-2 415+1 (No BOHESIGHT) bO3-XXXXX RANGF RATE
i1uR TIME TO CS
RESEF ET
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-30 COPY ROOT FOR 1ST CSI 81J
BORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-t7 415+1 (NO BORFSIGHT) 50-XXxXx RANGF RATE
267R VELOCITY TO HE GAINED CSI
402R LELTA H
371R OFLTA V COH
372R OELTA T CSICDH
-5 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 blb+XXXXX RANGE
-i2 415+1 (No BORESIGHT) 5n3-XXXXX RANGE RATE
415+1 (NO BORESIGHT)
5-5
503-XXXXX RANGF RATE
COPY Roor FOR 2NO CSI BU
bORESIGHT ON CSM 415+1 316+XXXXX RANGE
TEMPPRESS MON SEL - FUEL MAN
A AND 8 PRESS 181 +-3 PIG TEMPPRESS MON SEL - PRPLNT
A AND B TEMP IND 4ODEG 0 IOODEG F A AND B PRFSS IND 181 +-3 PSIA
tEMPPRESS MON SEL - HEL
A AND 8 PRESS IND PSIA
A QUANTITY IND- -- PERCENT RFMAINING
8 QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4p 2 3 (120 - 190 DFG F)
415+1 (NO BORESIGHT)-17 503-XXXXX RANGE RATE
-15 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
(LOS OF MSFN) S-BAND - SLEW 10 P = +90t Y U S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
-12 415+1 (No 8ORESIGHT)
503-XXXXX RANGE RATE
267R VFLOCITY TU BE GAINED CSI
402R OFLTA H
372R TIME CSICH
371R PREDICTED VEL 10 RE GAINED COH
263R OLT-OF-PLANE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATL
-10 COPY RANGE AND ROOT FOR 3RD CSI 8U
SORESIGH ON CSM 41b+1
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
4-26
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT KEY V34E (TERMINATE)
KEY V37E47E (AVE G) F 16 83 DELTA VIS
V63E (RR SELF TEST) F 04 12 00004 00001
PRO
F 16 72 TRUN SHFT PRO
F 16 78 R RDOT VERIFY TAPE METER WITH DSKY
BRAKING GATE 30 FPS - 6000 FT 20 FPS - 3000 FT 10 FPS - 1500 FT 5 FPS - 600 FT
RENDEZVOUS
STATION KEEPING
5-1
50 ABORT PROCEDURE
This is a specific AGS nominal abort procedure due to a PGNS failure between insertion and station keeping
51
5-2
Nominal AGS Procedures
ASSUMPTIONS
AFTER INSERTION
I INSERTION COMPLETE (RFSIDUALS NULLED) g PGNS FAILURE BEFORE INSERTION 3 RAUAR NOT LOCKED ON
(UI CoNT-AGS ATlI[uUE MON-AGS(CDR) RATE ERR MON-CNPTR(LMP) ATTITUDE MON-AGS(LMP) SHFITRUN-+5 DEG X-POINTER-HI MULT RADAR IEST Sw-OFF LNb GMbL-OFF ENG ARM-OFF X-IRANSL-2 JETS DEAD BAND-MAX PGNS MODE CONT-OFF THROTJET-JET CB IMU OIR-ON HH MOVE-AUTO rRACK TTCATNANSL-ENABLE(CDR)
AL CPL-ON MODE SL-AGS RNGAL1 MON-RNbRNGRT RAIE ERR MON-RNDZ HDR(CDR) AVl CoNT(3)-PULSE AGS MODE CONT-AUTO ACA4JET-DISABLE(CDR) TTCATRANSL-DISABLE(LMP) ACA4JET-DISABLE(LMP)
bO7+U Z-AXIS BOPESIGHT 400+2 Z-AXIS STEERING PULSE TO NULL AGS ERRORS POINT Z-AXIS IN DIRECTION OF CSM MODE CONT-ATT HOLD ATT CONT(3)-MODE CONTROL O unnr - ZirF
5-3
SLEW PATE - LO
SLEW RR ANT TO OqON FUAI VERIFY MAX SIGNAL STRENGTH RH MOOE-AUTO TRACK NO TRACK LIGHT OFF -
ATT CONT(3h-PULSE
CHECK INSERTION VELOCITY WITH TAPEMETER COMPARE EAPEMETER WITH AGS STATE VECTOR DATA I
17R RANGE(NOM 2642)
440R RANGE RATE(NOM -425l)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
cSI
+3 417+1 (RADAR FILTER INITIALIZED) 41b+l (NO BOHESIGHT) b03-XXXXX RANGE RATE
+5 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGF
41b+1 CSI ROUTINE 373+o2065 CSi TIME 275+03028 TPI TIME 605+0077 COTANGENT OF LOS TO CSM 41b+1 (ONE-HALF OFBITAL-PERIOD) 411+0 HCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT
610R TIME TO CST
43 RESET ET
267R VELOCITY TO BE GAINED CSI
402R FLTA H
371R DFLTA V CDH
5-4
372R DFLTA T CSICDH
-42 415+1 (No BORESIGHT) bO6-xXXXX RANGE RATE
-40 415+1 (NO BORESIGHT)503-XXXXX RANGE RATE dORESIGHT ON CSM
415+1 316+XXXXX RANGE
-37 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE
-15 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE UORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-2 415+1 (No BOHESIGHT) bO3-XXXXX RANGF RATE
i1uR TIME TO CS
RESEF ET
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-30 COPY ROOT FOR 1ST CSI 81J
BORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-t7 415+1 (NO BORFSIGHT) 50-XXxXx RANGF RATE
267R VELOCITY TO HE GAINED CSI
402R LELTA H
371R OFLTA V COH
372R OELTA T CSICDH
-5 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 blb+XXXXX RANGE
-i2 415+1 (No BORESIGHT) 5n3-XXXXX RANGE RATE
415+1 (NO BORESIGHT)
5-5
503-XXXXX RANGF RATE
COPY Roor FOR 2NO CSI BU
bORESIGHT ON CSM 415+1 316+XXXXX RANGE
TEMPPRESS MON SEL - FUEL MAN
A AND 8 PRESS 181 +-3 PIG TEMPPRESS MON SEL - PRPLNT
A AND B TEMP IND 4ODEG 0 IOODEG F A AND B PRFSS IND 181 +-3 PSIA
tEMPPRESS MON SEL - HEL
A AND 8 PRESS IND PSIA
A QUANTITY IND- -- PERCENT RFMAINING
8 QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4p 2 3 (120 - 190 DFG F)
415+1 (NO BORESIGHT)-17 503-XXXXX RANGE RATE
-15 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
(LOS OF MSFN) S-BAND - SLEW 10 P = +90t Y U S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
-12 415+1 (No 8ORESIGHT)
503-XXXXX RANGE RATE
267R VFLOCITY TU BE GAINED CSI
402R OFLTA H
372R TIME CSICH
371R PREDICTED VEL 10 RE GAINED COH
263R OLT-OF-PLANE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATL
-10 COPY RANGE AND ROOT FOR 3RD CSI 8U
SORESIGH ON CSM 41b+1
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
5-1
50 ABORT PROCEDURE
This is a specific AGS nominal abort procedure due to a PGNS failure between insertion and station keeping
51
5-2
Nominal AGS Procedures
ASSUMPTIONS
AFTER INSERTION
I INSERTION COMPLETE (RFSIDUALS NULLED) g PGNS FAILURE BEFORE INSERTION 3 RAUAR NOT LOCKED ON
(UI CoNT-AGS ATlI[uUE MON-AGS(CDR) RATE ERR MON-CNPTR(LMP) ATTITUDE MON-AGS(LMP) SHFITRUN-+5 DEG X-POINTER-HI MULT RADAR IEST Sw-OFF LNb GMbL-OFF ENG ARM-OFF X-IRANSL-2 JETS DEAD BAND-MAX PGNS MODE CONT-OFF THROTJET-JET CB IMU OIR-ON HH MOVE-AUTO rRACK TTCATNANSL-ENABLE(CDR)
AL CPL-ON MODE SL-AGS RNGAL1 MON-RNbRNGRT RAIE ERR MON-RNDZ HDR(CDR) AVl CoNT(3)-PULSE AGS MODE CONT-AUTO ACA4JET-DISABLE(CDR) TTCATRANSL-DISABLE(LMP) ACA4JET-DISABLE(LMP)
bO7+U Z-AXIS BOPESIGHT 400+2 Z-AXIS STEERING PULSE TO NULL AGS ERRORS POINT Z-AXIS IN DIRECTION OF CSM MODE CONT-ATT HOLD ATT CONT(3)-MODE CONTROL O unnr - ZirF
5-3
SLEW PATE - LO
SLEW RR ANT TO OqON FUAI VERIFY MAX SIGNAL STRENGTH RH MOOE-AUTO TRACK NO TRACK LIGHT OFF -
ATT CONT(3h-PULSE
CHECK INSERTION VELOCITY WITH TAPEMETER COMPARE EAPEMETER WITH AGS STATE VECTOR DATA I
17R RANGE(NOM 2642)
440R RANGE RATE(NOM -425l)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
cSI
+3 417+1 (RADAR FILTER INITIALIZED) 41b+l (NO BOHESIGHT) b03-XXXXX RANGE RATE
+5 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGF
41b+1 CSI ROUTINE 373+o2065 CSi TIME 275+03028 TPI TIME 605+0077 COTANGENT OF LOS TO CSM 41b+1 (ONE-HALF OFBITAL-PERIOD) 411+0 HCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT
610R TIME TO CST
43 RESET ET
267R VELOCITY TO BE GAINED CSI
402R FLTA H
371R DFLTA V CDH
5-4
372R DFLTA T CSICDH
-42 415+1 (No BORESIGHT) bO6-xXXXX RANGE RATE
-40 415+1 (NO BORESIGHT)503-XXXXX RANGE RATE dORESIGHT ON CSM
415+1 316+XXXXX RANGE
-37 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE
-15 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE UORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-2 415+1 (No BOHESIGHT) bO3-XXXXX RANGF RATE
i1uR TIME TO CS
RESEF ET
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-30 COPY ROOT FOR 1ST CSI 81J
BORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-t7 415+1 (NO BORFSIGHT) 50-XXxXx RANGF RATE
267R VELOCITY TO HE GAINED CSI
402R LELTA H
371R OFLTA V COH
372R OELTA T CSICDH
-5 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 blb+XXXXX RANGE
-i2 415+1 (No BORESIGHT) 5n3-XXXXX RANGE RATE
415+1 (NO BORESIGHT)
5-5
503-XXXXX RANGF RATE
COPY Roor FOR 2NO CSI BU
bORESIGHT ON CSM 415+1 316+XXXXX RANGE
TEMPPRESS MON SEL - FUEL MAN
A AND 8 PRESS 181 +-3 PIG TEMPPRESS MON SEL - PRPLNT
A AND B TEMP IND 4ODEG 0 IOODEG F A AND B PRFSS IND 181 +-3 PSIA
tEMPPRESS MON SEL - HEL
A AND 8 PRESS IND PSIA
A QUANTITY IND- -- PERCENT RFMAINING
8 QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4p 2 3 (120 - 190 DFG F)
415+1 (NO BORESIGHT)-17 503-XXXXX RANGE RATE
-15 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
(LOS OF MSFN) S-BAND - SLEW 10 P = +90t Y U S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
-12 415+1 (No 8ORESIGHT)
503-XXXXX RANGE RATE
267R VFLOCITY TU BE GAINED CSI
402R OFLTA H
372R TIME CSICH
371R PREDICTED VEL 10 RE GAINED COH
263R OLT-OF-PLANE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATL
-10 COPY RANGE AND ROOT FOR 3RD CSI 8U
SORESIGH ON CSM 41b+1
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
51
5-2
Nominal AGS Procedures
ASSUMPTIONS
AFTER INSERTION
I INSERTION COMPLETE (RFSIDUALS NULLED) g PGNS FAILURE BEFORE INSERTION 3 RAUAR NOT LOCKED ON
(UI CoNT-AGS ATlI[uUE MON-AGS(CDR) RATE ERR MON-CNPTR(LMP) ATTITUDE MON-AGS(LMP) SHFITRUN-+5 DEG X-POINTER-HI MULT RADAR IEST Sw-OFF LNb GMbL-OFF ENG ARM-OFF X-IRANSL-2 JETS DEAD BAND-MAX PGNS MODE CONT-OFF THROTJET-JET CB IMU OIR-ON HH MOVE-AUTO rRACK TTCATNANSL-ENABLE(CDR)
AL CPL-ON MODE SL-AGS RNGAL1 MON-RNbRNGRT RAIE ERR MON-RNDZ HDR(CDR) AVl CoNT(3)-PULSE AGS MODE CONT-AUTO ACA4JET-DISABLE(CDR) TTCATRANSL-DISABLE(LMP) ACA4JET-DISABLE(LMP)
bO7+U Z-AXIS BOPESIGHT 400+2 Z-AXIS STEERING PULSE TO NULL AGS ERRORS POINT Z-AXIS IN DIRECTION OF CSM MODE CONT-ATT HOLD ATT CONT(3)-MODE CONTROL O unnr - ZirF
5-3
SLEW PATE - LO
SLEW RR ANT TO OqON FUAI VERIFY MAX SIGNAL STRENGTH RH MOOE-AUTO TRACK NO TRACK LIGHT OFF -
ATT CONT(3h-PULSE
CHECK INSERTION VELOCITY WITH TAPEMETER COMPARE EAPEMETER WITH AGS STATE VECTOR DATA I
17R RANGE(NOM 2642)
440R RANGE RATE(NOM -425l)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
cSI
+3 417+1 (RADAR FILTER INITIALIZED) 41b+l (NO BOHESIGHT) b03-XXXXX RANGE RATE
+5 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGF
41b+1 CSI ROUTINE 373+o2065 CSi TIME 275+03028 TPI TIME 605+0077 COTANGENT OF LOS TO CSM 41b+1 (ONE-HALF OFBITAL-PERIOD) 411+0 HCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT
610R TIME TO CST
43 RESET ET
267R VELOCITY TO BE GAINED CSI
402R FLTA H
371R DFLTA V CDH
5-4
372R DFLTA T CSICDH
-42 415+1 (No BORESIGHT) bO6-xXXXX RANGE RATE
-40 415+1 (NO BORESIGHT)503-XXXXX RANGE RATE dORESIGHT ON CSM
415+1 316+XXXXX RANGE
-37 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE
-15 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE UORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-2 415+1 (No BOHESIGHT) bO3-XXXXX RANGF RATE
i1uR TIME TO CS
RESEF ET
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-30 COPY ROOT FOR 1ST CSI 81J
BORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-t7 415+1 (NO BORFSIGHT) 50-XXxXx RANGF RATE
267R VELOCITY TO HE GAINED CSI
402R LELTA H
371R OFLTA V COH
372R OELTA T CSICDH
-5 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 blb+XXXXX RANGE
-i2 415+1 (No BORESIGHT) 5n3-XXXXX RANGE RATE
415+1 (NO BORESIGHT)
5-5
503-XXXXX RANGF RATE
COPY Roor FOR 2NO CSI BU
bORESIGHT ON CSM 415+1 316+XXXXX RANGE
TEMPPRESS MON SEL - FUEL MAN
A AND 8 PRESS 181 +-3 PIG TEMPPRESS MON SEL - PRPLNT
A AND B TEMP IND 4ODEG 0 IOODEG F A AND B PRFSS IND 181 +-3 PSIA
tEMPPRESS MON SEL - HEL
A AND 8 PRESS IND PSIA
A QUANTITY IND- -- PERCENT RFMAINING
8 QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4p 2 3 (120 - 190 DFG F)
415+1 (NO BORESIGHT)-17 503-XXXXX RANGE RATE
-15 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
(LOS OF MSFN) S-BAND - SLEW 10 P = +90t Y U S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
-12 415+1 (No 8ORESIGHT)
503-XXXXX RANGE RATE
267R VFLOCITY TU BE GAINED CSI
402R OFLTA H
372R TIME CSICH
371R PREDICTED VEL 10 RE GAINED COH
263R OLT-OF-PLANE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATL
-10 COPY RANGE AND ROOT FOR 3RD CSI 8U
SORESIGH ON CSM 41b+1
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
5-3
SLEW PATE - LO
SLEW RR ANT TO OqON FUAI VERIFY MAX SIGNAL STRENGTH RH MOOE-AUTO TRACK NO TRACK LIGHT OFF -
ATT CONT(3h-PULSE
CHECK INSERTION VELOCITY WITH TAPEMETER COMPARE EAPEMETER WITH AGS STATE VECTOR DATA I
17R RANGE(NOM 2642)
440R RANGE RATE(NOM -425l)
SUITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
cSI
+3 417+1 (RADAR FILTER INITIALIZED) 41b+l (NO BOHESIGHT) b03-XXXXX RANGE RATE
+5 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGF
41b+1 CSI ROUTINE 373+o2065 CSi TIME 275+03028 TPI TIME 605+0077 COTANGENT OF LOS TO CSM 41b+1 (ONE-HALF OFBITAL-PERIOD) 411+0 HCS ENGINES 623+0 Z-AXIS PARALLEL TO CSM ORBIT
610R TIME TO CST
43 RESET ET
267R VELOCITY TO BE GAINED CSI
402R FLTA H
371R DFLTA V CDH
5-4
372R DFLTA T CSICDH
-42 415+1 (No BORESIGHT) bO6-xXXXX RANGE RATE
-40 415+1 (NO BORESIGHT)503-XXXXX RANGE RATE dORESIGHT ON CSM
415+1 316+XXXXX RANGE
-37 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE
-15 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE UORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-2 415+1 (No BOHESIGHT) bO3-XXXXX RANGF RATE
i1uR TIME TO CS
RESEF ET
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-30 COPY ROOT FOR 1ST CSI 81J
BORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-t7 415+1 (NO BORFSIGHT) 50-XXxXx RANGF RATE
267R VELOCITY TO HE GAINED CSI
402R LELTA H
371R OFLTA V COH
372R OELTA T CSICDH
-5 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 blb+XXXXX RANGE
-i2 415+1 (No BORESIGHT) 5n3-XXXXX RANGE RATE
415+1 (NO BORESIGHT)
5-5
503-XXXXX RANGF RATE
COPY Roor FOR 2NO CSI BU
bORESIGHT ON CSM 415+1 316+XXXXX RANGE
TEMPPRESS MON SEL - FUEL MAN
A AND 8 PRESS 181 +-3 PIG TEMPPRESS MON SEL - PRPLNT
A AND B TEMP IND 4ODEG 0 IOODEG F A AND B PRFSS IND 181 +-3 PSIA
tEMPPRESS MON SEL - HEL
A AND 8 PRESS IND PSIA
A QUANTITY IND- -- PERCENT RFMAINING
8 QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4p 2 3 (120 - 190 DFG F)
415+1 (NO BORESIGHT)-17 503-XXXXX RANGE RATE
-15 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
(LOS OF MSFN) S-BAND - SLEW 10 P = +90t Y U S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
-12 415+1 (No 8ORESIGHT)
503-XXXXX RANGE RATE
267R VFLOCITY TU BE GAINED CSI
402R OFLTA H
372R TIME CSICH
371R PREDICTED VEL 10 RE GAINED COH
263R OLT-OF-PLANE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATL
-10 COPY RANGE AND ROOT FOR 3RD CSI 8U
SORESIGH ON CSM 41b+1
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
5-4
372R DFLTA T CSICDH
-42 415+1 (No BORESIGHT) bO6-xXXXX RANGE RATE
-40 415+1 (NO BORESIGHT)503-XXXXX RANGE RATE dORESIGHT ON CSM
415+1 316+XXXXX RANGE
-37 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE
-15 415+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE UORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-2 415+1 (No BOHESIGHT) bO3-XXXXX RANGF RATE
i1uR TIME TO CS
RESEF ET
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-30 COPY ROOT FOR 1ST CSI 81J
BORESIGHT ON CSM 415+1 31b+XXXXX RANGF
-t7 415+1 (NO BORFSIGHT) 50-XXxXx RANGF RATE
267R VELOCITY TO HE GAINED CSI
402R LELTA H
371R OFLTA V COH
372R OELTA T CSICDH
-5 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 blb+XXXXX RANGE
-i2 415+1 (No BORESIGHT) 5n3-XXXXX RANGE RATE
415+1 (NO BORESIGHT)
5-5
503-XXXXX RANGF RATE
COPY Roor FOR 2NO CSI BU
bORESIGHT ON CSM 415+1 316+XXXXX RANGE
TEMPPRESS MON SEL - FUEL MAN
A AND 8 PRESS 181 +-3 PIG TEMPPRESS MON SEL - PRPLNT
A AND B TEMP IND 4ODEG 0 IOODEG F A AND B PRFSS IND 181 +-3 PSIA
tEMPPRESS MON SEL - HEL
A AND 8 PRESS IND PSIA
A QUANTITY IND- -- PERCENT RFMAINING
8 QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4p 2 3 (120 - 190 DFG F)
415+1 (NO BORESIGHT)-17 503-XXXXX RANGE RATE
-15 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
(LOS OF MSFN) S-BAND - SLEW 10 P = +90t Y U S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
-12 415+1 (No 8ORESIGHT)
503-XXXXX RANGE RATE
267R VFLOCITY TU BE GAINED CSI
402R OFLTA H
372R TIME CSICH
371R PREDICTED VEL 10 RE GAINED COH
263R OLT-OF-PLANE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATL
-10 COPY RANGE AND ROOT FOR 3RD CSI 8U
SORESIGH ON CSM 41b+1
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
5-5
503-XXXXX RANGF RATE
COPY Roor FOR 2NO CSI BU
bORESIGHT ON CSM 415+1 316+XXXXX RANGE
TEMPPRESS MON SEL - FUEL MAN
A AND 8 PRESS 181 +-3 PIG TEMPPRESS MON SEL - PRPLNT
A AND B TEMP IND 4ODEG 0 IOODEG F A AND B PRFSS IND 181 +-3 PSIA
tEMPPRESS MON SEL - HEL
A AND 8 PRESS IND PSIA
A QUANTITY IND- -- PERCENT RFMAINING
8 QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4p 2 3 (120 - 190 DFG F)
415+1 (NO BORESIGHT)-17 503-XXXXX RANGE RATE
-15 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
(LOS OF MSFN) S-BAND - SLEW 10 P = +90t Y U S-BAND - FWD (OR AFT) S-BAND - ON VOICE BU BIOMED OFF
-12 415+1 (No 8ORESIGHT)
503-XXXXX RANGE RATE
267R VFLOCITY TU BE GAINED CSI
402R OFLTA H
372R TIME CSICH
371R PREDICTED VEL 10 RE GAINED COH
263R OLT-OF-PLANE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATL
-10 COPY RANGE AND ROOT FOR 3RD CSI 8U
SORESIGH ON CSM 41b+1
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
-7
5-6
316+XXXXX RANEF
COMPUTE CSI BU
415+1 NO FORESIGHT bo3-XXXXX RANGE RATE
(TRANSMIT CSI DATA TO CSM) VHF A XMfR - VOICE VHF B XMTR - DATA VHF B RCVR - OFF
TELEMETY PCM - LO
-b 415+1 NO BORESIGHT 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
277R THETA SET ORDEAL
317R RANGE
440R -_ RANGE RATE
507+1 Z-AxIS DLTA V 400+0 ATT HOLD 41U+b EXrERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
450 451 452 407+0 ROTATE EXTERNAL DELTA V HF
NULL FRROR SIGNALS WITH AGS PULSE
TRANSMIT TGT DELTA VtS TO CSM AND SYNC COUNTDOWN
bO2R DFLTA VZ (NOM 501)
-20 UEADaAND-MIN (DEFLECT RHC OUT OF UETENT) AGS MODE CON1-ATf HOLD ATT CONT(3)-MOOE CONT
407+1 FREEZE EXTERNAL UFLTA V
SET ET CoUNTING UP AT ZERO
(c2i2627) UURN +Z
NULL DELTA VS
VERIFY AGS RESIDUALS 500R 501R 502R OELTA VX_ DELTA VY DELTA VZ
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
5-7
CDH
ATT CONT(3)-PULSE AGS MODE CONT-ALITO bO7+U Z-AXIS RORESIGHT 400+2 Z-AXIS STEERING
+) 410+2 CDH ROUTINE
(VHF RANGING WITH CSM) vHF A XMTR - VOICERNG VHF 8 XMTR - OFF vHF B HCVR - ON 1ELEMFTRY PCM - HI
411+0 THRUST ALONG 2-BODY AXI
373R (NOM 2b44) 310R TIME TO COH
-b2 RESET ET
423R DFSIRED ALT RATE AT C1H
402R DELTA H
45OR DFLTA VX
452R DELTA VZ 623+U Z-AXIS PARALLEL TO CSM PLANF
417+1 (RADAR FILTER INITIALIZEO) -bo 415+1 (NO BORESIGHT)
bO3-XXXXX RANGE RATE bORESIGHr ON CSM
415+1 316+XXXXx RANGE
-47 415+1 (No BONESIGHT) bO3-xXXXX RANGF RATE
-45 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 - J16+XXXXX RANGF
-42 415+1 (No BORESiGHT) 503-XXXXX RANGEiRATE
-40 415+1 (No BORESIGHT) 503-XXXX0 X RANGE RATE
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
5-8
BORESIGHT ON CSM 415+1 Jl+XXXXX RANGF
PLANE CHANGE
415+1 (No BORESI6HT)
503-XXXXX RANGE RATE
-36 cOPY ROOT FOR 1ST CDH BLI
-35 UORESIGHT ON CSM qlb+X j16+XXXXX RANGE
b07+1 Z-AXIS DELTA V
400+0 ATT HOLD 410+b EX[ERNAL DELTA V (COPY YDOT FROM CSM AND LOAD NEGATIVE IN U51)
450+0 4fl 52+0 407+0 ROTATE EXTERNAL DELTA V RF
NULL FRRUR SIGNALS wITH AGS PULSE
-2u UEADtANO-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONI-ATI HOLD AT CONT(3)-MODF CONT
407+1 FREEZE FXIERNAL DELTA V
-i0 NULL DELTA VS
ATT CONT(3v)-PULSE AGS MODE CONT-AULTO 507+0 Z-AXIS ROPESIGHT 400+2 Z-AXIS SIFERINb
410+2 CDH ROUTINE
373R (NUM 2b44)
31UR TIME TO CDh
423R DFSIRED ALT RAlF Al CDH
402R DELTA H
45OR DELTA VX
452R DELTA VZ
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
5-9
417+1 (RADAR FILTER INITIALIZFD) -27 415+1 (No BORESIGT)
503-XXXXX RANGE RATE
-25 415+1 (No BORESIGHT) 503-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 31+XXXXX RANGE
(AoS OF MSFN) S-ANO- SLEw TO P __ p Y ACQUIRE HGA LOCK ON VOICE - tUVOICE -- VOICE VERIFY VOICEP ILM BIOMED - LEFT (OR RIGHT)
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-23 COPY ROOT FOR 2ND CDH 81)
TEMPPRESS MON SEL - FUEL MAN A AND B PRESS 181 +-3 PSIG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP INU 40DEG TO lODEG F A AND B PRFSS IND II +-3 PSIA
rEMPPRESS MON SEL - HEL
A AND B PRESS INO - PSIA
A QUANTITY IND PERCENT REMAINING
B QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD Ip 4t 2p 3 (120 -
SUITCABIN PRESS - NOR OLYCOL TEMPPRESS - NOR
02H20 QUANTITY - NOMINAL
-20 415+1 (NO BORFSIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM 415+1 316+XXXXX RANGE
-17 415+1 (NO BORESIGHT) 503-XxxxX RANGE RATE
-15 41b+1 (NO BORESIGHT) bO3-XXXXX RANGE RATE BORESIGH[ ON CSM 415+1 316+XXXXX RANGE
-12 415+1 (NO BORESIGHT) 503-XXXXX RANGE RATE
190 DFO F)
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
5-10
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
-10 COPY ROOT FOR 3RD CDH BUi
8ORESIGHT ON CSM 415+1 ib+XXXXX RANGE
COMPUTE CDH bLU
-7 415+1 NO BORESIGHT b03-XXXXX RANGE RATE
-b 415+1 NO BORESIGHT b03-xXxXX RANGE RATE bORESIGHI ON CSM
415+1 316+XXXXX RANGE
277R SET ORDEAL
THETA
317R NANGE
U4R - RANGE RATE
bO+l A-AXIS DELTA V 400+0 ATT HOLD 410+5 EXTERNAL DELTA V (LOAD SOLUTION TO BE EXFCUTED)
bull450 461 452 407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
IRANSMIT TGT DELTA VIS TO CSM AND SYNC COUNTDOWN
50OR DELTA VX (NOM -03)
502R UELTA VZ (NOM b0)
-2u UEADBAND-MIN
(DEFLECT RHC OUT OF DETFNT) AGS MODE CON7-ATr HOLD ATT CONT(3)-MODF CONT
407+1 FREEZE EXTERNAL DELTA V
SET ET COUNTING UP AT ZERO
(1242425) NULL DELTA VS
VERIFY AGS RESIDUALS
50OR 501H 502R
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
-30
5-11
+
62
-27
-es
-22
-21
DELTA VX- DELTA VY DELTA-VZ__-
TPI
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
bO7+u Z-AXIS PQPESIGHT 400+2 Z-AXIS STEERING
417+1 (RADAR FILTER INITIALIJFO) 41b+1 (No BORESIGHT) 503-XXXXX RANGE RATE
410+6 TPX SEARCH iOUTINE 307+U4300 DELTA T TRANSFER 310+03400 TFT TPI
303R _THFTA AT TPI
410+4 (WHEN 301 = 2660 DEG)
310R TFI TPI
xESET ET
267R DELTA V TPI
371R DELTA V TFI + DELTA V TPF
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (NO BORFSIGHT) b03-XXXXX RANGF RATE BORESIGH[ ON CSM 415+1 31b+XXXXX RANGE
41b+l (No BORESIGHT) 503-XXXXX RANGE RATE
415+1 (No BORESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 316+XXXXX RANGE
41b+ (NO BORESIGHT) 503-XXXXX RANGE RATE
410+3 TPI SEARCH ROUTINF 307+04300 DELTA T TRANSFER shy
310+02100 TFI TPI
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
5-12
303R THETA AT TPI 410+4 (WHEN 303 = 266u DEG)
310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V 1PI + DELTA V TPF
-20 415+1 (NO BORFSIGHT) bO3-XXXXX RANGE RATE BORESIGHT ON CSM
415+1 316+XXXXX RANGE
-17 415+1 (No BORESIGHT) bO3-XXXXX RANGE RATE
TEMPPRESS MON FEL - FUEL MAN A AND B PRFSS 191 +-3 PSLG
TEMPPRESS MON SEL - PRPLNT A AND B TEMP IND 4ODEG TO lOUDEG F A AND B PRESS IND 181 +-3 PSIA
TEMPPRESS MON SEL - HEL
A AND B PRESS IND PSIA
A QUANTIrY IND PERCENT REMAINING
b QUANTITY IND PERCENT REMAINING TEMP MON SEL RCS QUAD 1 4t 2p 3 (120 - l)O UFG F)
SLIITCABIN PRESS - NOR GLYCOL TEMPPRESS - NOR 02H20 QUANTITY - NOMINAL
-15 415+1 (NO BOkESIGHT) 503-XXXXX RANGE RATE bORESIGHT ON CSM
415+1 lb+XXXXX RANbF
-12 41b+i (NO BORESIGHT)503-XXXx RANGE RATE
410+3 TPI SEARCH ROUTINE 07+04300 DELTA T TRANSFER
-11 310+U110o TFT TPI
303R THF A AT FPl 410+4 (WHEN 303 = 2660 DEG)
277R THETA SET ORDEAL
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
-7
5-13
t310R TFI TPI
RESET ET
267R DELTA V TPI
371R DELTA V TPI + DELTA V TPF
TRANSMIT TIG OF rpi To CSM
-9 77R COPy TGT LOS ANGLE
415+1 NO BORESIGHT b3-XXXXX RANGE RATE
404+0 40b+O 406+0 (MONITOR 470 471 472)
415+1 NO BORESIGHT 503-XXXXX RANGE RATE
-b 277R COPY TGT LOS ANGLE
COPY Rp RDOT FROM TAPE METER FORRUS
bORESIGHr ON CSM 415+1 31b+XXXXX RANGE
373R TIG TPI
e67R DELTA V TPL
LOMPUTE rPI BtI
371R DELTA V TPI +DELTA V TPF
b07+1 Z-AXIS DELTA V 400+0 ATT HOLD 410+b EXTERNAL DELTA V (LOAD SOLUTION TO BE EXECUTED
45u 451 452 shy407+0 ROTATE EXTERNAL DELTA V RF
NULL ERROR SIGNALS WITH AGS PULSE
COPY CSM TPI SOLUTION AND SYNC COUNTDOWN WITH CSM
bOOR DELTA VX (NOM -11b)
502R DELTA VZ (NOM 22g)
-20 DEADBAND-MIN (DEFLECT RHC OUT OF DETENT) AGS MODE CONT-ATT HOLD ATT CONT(3)-MODE CONT
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
1 5-14
407+1 FREEZE EXTERNAL UELTA v
SET ET COUNTING UP AT ZERO
(125U246) bURN +Z
vERIFY AcS RESIDUALS bOUR 501R 502R
ELTA VX DEETA VY DELTA VZ_
MCCI
ATT CONT(3)-PULSE AGS MODE CONI-AUTO
507+0 Z-AXIS PORESIGHT 400+2 Z-AXIS STEERING
(LOS OF MsFN) S-BAND - SLEW 1o P = +90t Y = 0 S-bAND - FWD (OR AFT) S-BAND - ON VOICE BU bIOMED OFF
q0+o 405+0 406+0
+9 277R COPY TGI LOS ANbLE
+13 277R COPY TGT LOS ANGLE
COPy Pr ROOT FROM TAPE MLTER FOR PUS
COMPUTE MCCI RU
+144U DEAORANu-MIN (DEFLECT RHC OUT OF DETFNT) AGS MODE CONT-ATr HOLD ATT CONT(3)-MODF CONr
400+0 ATr HOLD 470R 471R 472R
+15 NULL DELTA V S
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
5-15
MCC2
ATT CONT(3)-PULSE AGS MODE CONT-AUTO
404+0 40b+O 406+0
+24 277R COPy TGT LOS ANGLE
+e8 277R COPY TGT LOS ANGLE
COPY Rf HOO FROM TAPF METER FOR BUIS
COMPUTE MCC2 RU
+294U DEADBANU-MIN (DEFLFCT RHC OUT OF DETENT) AGS MODE cONI-Air HOLD ATT CONT(3)-MODF CONT
470R 471R 472R
+30 NULL DELTA V S
ATT CONT(3)-PULSE VERIFY TAPE MEIFR WITH A(S
LOS CONTROL
BRAKING bATE 30 FPS - bOO0 FT 20 FPS - 3O0 FT
iu FPS - 1500 f b FPS - 600 FT
RENDEZVOUS
STATION KEEPING
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
60 ONBOARD RENDEZVOUS CHARTS
Charts 61 thru 66 are the nominal onboard rendezvous charts for Mission G
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
RI Fl R2 F2 R3 F3 R3 F4 CHART 6 1
-240 0 2473 -1400 2547 -700 724 120 0 152 -2410 2484 -1410 2566 -710 73 4 1210 155 CSI BACKUP TABLE -2420 -2430
2494 2505
-1420 -143 0
2584 2602
-720 -730
74 4 75 5
1220 1230
157 159
MISSION G
-2440 -2450 -2460
2515 2525 2536
-1440 -1450 -1460
2621 2639 265 7
-740 -750 -760
765 775 786
1240 1250 1260
161 163 165
TIME (Min)
NOMINAL
-2470 -2480
2546 2557
-1470 -1480
2676 269 4
-770 -780
79 6 806
1270 1280
167 169
-30 Ri (-2833)
-2490 -2500
2567 2578
-149 0 -1500
271 3 2731
-790 -80 0
817 827
1290 130 0
17 1 173
-20 R2 (-1739)
-2510 -2520
2588 2599
-1510 -1520
2749 276 8
-810 -82 0
837 848
131 0 1320
175 177
-10 R3 (- 940)
-2530 -2540
2609 2620
-1530 -1540
2786 2804
-830 -840
858 869
1330 134 0
179 181
-10 R3 (1541)
-2550 -256 0
2630 2641
-1550 -1560
2823 2841
-850 -860
879 889
135 0 1360
184 186
Fl (2930) -257 0 -258 0
2651 2662
-157 0 -158 0
2860 2878
-870 -880
900 910
137 0 1380
188 190
+F3 (972)
-259 0 -2600
2672 2683
-1690 -160 0
2897 2915
-89 0 -900
920 931
1390 1400
192 19 4
(3902)
-2610 -2620
2693 2704
-1610 -1620
2934 295 2
-91 0 -920
941 95 2
141 0 1420
196 198
-F2 (-3173)
-2630 -264 0
2714 272 5
-1630 -1640
2970 2989
-930 -940
962 972
1430 1440
200 202
( 729)
-2650 -2660
273 5 2746
-1650 -1660
300 7 3026
-95 0 -960
983 993
145 0 1460
205 207
-F4 (- 224)
-2670 -2680
2757 2767
-1670 -1680
3044 3063
-970 -980
1004 1014
147 0 1480
209 211
(505)
-2690 -2700
2778 2788
-169 0 -1700
3081 310 0
-990 -1000
1024 1035
1490 1500
21 3 215
+ VCSI ( 00)
-2710 -2720
2799 2810
-1710 -172 0
311 9 3137
-1010 -1020
1045 1056
151 0 1520
217 219
VCSI 5(605)
-2730 2820 -1730 315 6 -1030 106 6 1530 221 -2740 2831 -174 0 3174 -1040 1077 1540 22 4 -2750 2842 -1750 3193 -1050 1087 155 0 226 -2760 2852 -1760 321 1 -1060 1097 1560 228 -2770 2863 -1770 323 0 -1070 110 8 1570 230 -2780 2874 -1780 3249 -1080 1118 158 0 232 -2790 -2800
2884 2895
-1790 -1800
3267 328 6
-1090 -1100
1129 1139
1590 160 0
23 4 236
PREPARED by FPrBOPS
-2810 290 6 -1810 330 4 -1110 115 0 1610 238 MISSION APOLLO 11 MAY 16 1969
6-2
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
LHART 6 1
RI Fl R2 F2 R3 F3 R3 F4
-2820 -2830
2916 2927
-1820 -1830
332 3 3342
-1120 -1130
116 0 1170
16201630
240242
-2840 -2850
2938 2948
-184 0 -1850
336 0 3379
-1140 -1160
1181 1191
1640 165 0
245 24 7
-2860 2959 -1860 3398 -116 0 120 2 166 0 249 -287 0 2970 -1870 3416 -1170 1212 167 0 251 -2880 2981 -1880 3435 -1180 1223 168 0 2b3 -2890 -2900
2992 3002
-189 0 -190 0
3454 347 2
-1190 -120 0
123 3 1244
16901700
25 5257
-2910 3013 -1910 3491 -1210 125 4 1710 259 -292 0 3024 -1920 351 0 -1220 1265 1720 261
-2930 3035 -1930 352 9 -1230 1275 1730 263 -2940 -2950
3046 3056
-1940 -195 0
354 7 356 6
-1240 -125 0
128 6 129 6
17401750
265267 -3 -1
-2960 3067 -1960 3585 -126 0 130 7 1760 269 -2970 307 8 -1970 3604 -127 0 131 7 1770 27 1 -2980 308 9 -1980 3622 -128 0 132 8 178 0 27 3 -2990 310 0 -1990 3641 -129 0 1338 179 0 27 5 -3000 3111 -200 0 3660 -130 0 134 9 1800 277 -3010 3122 -201 0 367 9 -131 0 1359 181 0 279 -3020 3132 -2020 3698 -1320 1370 182 0 281 -3030 314 3 -2030 3716 -1330 1380 183 0 283
-3040 315 4 -2040 3735 -1340 1391 1840 285 -3050 3165 -2050 3754 -135 0 140 1 185 0 28 7 -3060 3176 -2060 3773 -1360 1412 1860 28 9 -3070 3187 -2070 3792 -137 0 1422 1870 291 -3080 3198 -2080 3811 -1380 1433 1880 293 -3090 3209 -2090 3830 -1390 1443 1890 295 TIQ TpI -3100 3220 -2100 3849 -1400 145 4 1900 29 7 -3110 3231 -2110 3868 -1410 1464 1910 299 - TIG TPI -3120 324 2 -212 0 3887 -142 0 1475 1920 301 -3130 325 3 -2130 390 5 -1430 1485 1930 303 AT -3140 3264 -2140 392 4 -144 0 149 6 1940 305 -3150 3275 -2150 3943 -145 0 1507 1950 307 - NOM AT - 1 3521 -3160 3286 -2160 3962 -146 0 1517 1960 309 -3170 3297 -217 0 3981 -1470 1528 1970 310 6AT -3180 3308 -2180 4000 -1480 1538 1980 312 -3190 331 9 -2190 4019 -1490 1549 199 0 314 AVCSI -3200 3330 -2200 4038 -1500 1559 200 0 316 -3210 334 1 -2210 405 7 -151 0 1570 2010 318 Prepared by FPrBOPS -3220 335 3 -2220 4077 -1520 1581 2020 32 0 -3230 3364 -2230 409 6 -1530 159 1 2030 322 MISSION APOLLO 11 MAY 16 1969
6-3
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
ROOT X1 Z1 X2 Z2 X3 Z3 CHART 6 2
-75 297 526 306 132 0 9 79 2 -76 301 534 310 1339 9 803 -77 -78
305 308
543 551
313 317
1359 1379
9
9 815 826
CDH BACKUP TABLE MISSION G
-79 312 559 321 1399 9 838 -80 -81 -82
316 320 324
568 576 584
325 328 332
1418 1438 1458
9
9
9
849 861 872
TIME (MIN)
NOMINAL
-83 -84
327 331
593 601
336 339
1478 1498
8
8 884 896
-36 Rl (-12221)
-85 -86
335 339
610 618
343 347
1518 1538
8
8 907 919
-23 R2 (-122 68)
-87 342 627 35 0 1559 8 931 -10 R3 (-12287) -88 346 63 5 35 4 1579 8 942 -89 350 644 358 1599 8 954 -90 -91
354 357
653 661
361 365
1619 1640
8
8 966 978
VX- X1 472
-92 361 670 369 1660 8 989 +X3 01 -93 365 679 372 1681 7 1001 -94 -95
369 372
688 696
376 380
170o 1722
7
7 1013 1025
( 473
-96 -97
376 38 0
705 714
383 387
1742 1763
7
7 1037 1049
-X2 ( -477 -98 383 723 390 1784 7 1061 vx[ j ( 0 4 FPS -99 387 732 394 1805 6 1073 -100 -101 -102
391 395 398
741 750 759
39 8 401 405
1826 1847 186 7
6
6
6
1085 1097 1109
VZ Z2 (2313
-103 -104
402 406
768 777
408 412
1889 1910
6
6 1121 1133
-z ( -948
-105 -106 -107 -108
409 413 417 420
786 795 804 814
415 419 422 426
1931 1952 1973 1994
5
5
5
5
1145 1157 1169 1182
-Z3
( 1365
(-1365
-109 424 823 429 2016 5 1194 vzl 00 FPS -110 428 832 433 2037 4 1206 -111 431 842 436 2059 4 1218 -112 435 851 440 208 0 4 1230 -113 439 860 443 2102 4 1243 -114 44 2 870 447 2123 4 1255 -115 -116
446 450
879 889
450 454
2145 216 7
3
3 1267 1280
PREPARED BY FPRBOPS
-117 453 898 457 2188 3 1292 MISSION APOLLO 11 MAY 16 1969
6-4
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
CHART 6 2
RDOT X1 Zi X2 Z2 X3 Z3
-118 457 908 46 1 221 0 3 1305 -119 46 1 917 46 4 2232 2 1317 -120 464 927 467 2254 2 1329 -121 46 8 936 471 2276 2 134 2 -122 471 946 474 2298 2 135 4 -123 475 956 478 2320 1 1367 -124 479 965 481 2342 1 1379 -125 482 975 48 4 2364 1 1392 -126 436 985 48 8 2386 0 1405 -127 489 99 5 49 1 2409 0 141 7 -128 49 3 1005 495 2431 -0 1430 -129 497 1015 498 2453 - 0 144 3 -130 500 1024 501 2476 - 1 1455 -131 504 1034 505 2498 -1 146 8 -132 507 1044 508 2521 -1 1481 -133 511 1054 511 254 4 -2 1493 -134 515 1064 514 256 6 -2 1506 -135 518 1074 518 2589 -2 151 9 -136 522 1085 521 2612 - 3 153 2 -137 525 1095 524 2634 -3 154 5 -138 529 1105 52 8 2657 -3 1558 -139 532 1115 53 1 2680 -4 157 0 -140 536 1125 534 2703 -4 158 3 -141 53 9 1136 53 7 2726 -4 1596 -142 543 1146 541 2749 - 5 1609 -143 546 1156 544 2772 -5 1622 -144 550 116 6 547 2796 -5 1635 -145 553 117 7 550 2819 -6 1648 -146 557 1187 553 2842 -6 1661 -147 561 1198 557 2865 -7 1674 -148 56 4 1208 560 2889 -7 1688 -149 568 1219 563 2912 - 7 1701 -150 571 1229 566 2936 - 8 1714 -151 575 124 0 569 2959 -8 1727 -152 578 125 0 57 3 2983 -9 1740 -153 582 1261 576 300 7 -9 1753 -154 585 1272 579 3030 - 9 1767 -155 588 1282 582 3054 -10 1780 -156 592 1293 585 3078 -10 179 3 -157 595 1304 58 8 3102 -11 1807 PREPARED BY FPRBOPS -158 599 131 5 59 1 3126 -11 182 0 -159 602 1326 594 3150 -1 2 1833 MISSION APOLLO 11 MAY 16 1969
6-5
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
G MISSION TERMINAL PHASE INITIATION PREPARED BY FPRBOPS CHART 6 3
_5 -
(N69)
22 24 R 5 19 54
RREQ
3818 R 5 --AR __
1 9
112 3 246
X36
25
A N69
-
+ + am
----- -
uC
21
80 90 100 110 120 130 140 LMISSION
150 160 170 18010 APOLLO 11 NAY 16 1969
15 0 2 30 35 40 45
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
PREPARED BY FPRBOPSA
013 4328 R
09- _ 37 24
Ao - 604
PNGS(N59) CSM(N59)
id
G MISSION FIRST MIDCOURSE CORRECTION
RREQ 104 5
1723 R13 - 104 5
tR 0 0
CHARTS AT H U -i
L
500133 A
A 232 a
48
8360 7 80 9 I0
44
I0 12 13 10 1
-A
4 0
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
G MISSION SECOND MIDCOURSE CORRECTION
PREPARED BY FPRBOPS CHART 65
628
624-77 41
66 22
R234
RREQ 3 R28
52 4 52 4
00 - -__
___11 19
PNGS(N59) CSM(N59) CHARTS AT
a28
620 30 40 50 60 70 80 90 100 ho 8 9 I I 2 1 m A
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
PREPARED BY FPRBOPS G MISSION RELATIVE REFERENCE TRAJECTORY - CHlART 6 6
Time (MIN) 18 20 22 24 26 28 30 32 34 36 38 40
9 (DEG) 52 6 56 9 61 5 67 0 72 1 77 5 84 2 90 8 97 5 104 3 Ill 3 118 3
R (NM) 12 9 11 2 9 6 8 2 6 9 5 8 4 8 3 9 3 1 2 3 1 6 0 95
R (fps) 91 83 75 68 60 54 48 43 39 36 35 33
1800 10 2030 1 14 I 1
S TIME 506
BR RNOT
3IE
0
0shy
0 ISO PLOIMY116
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969
7-1
70 REFERENCES
71 Mission Requirements SA-506CSM-l07LM-5 GType Mission Lunar Landing data 17 April 1969
72 Apollo Mission G Spacecraft Operational Trajectory Volume 1 MSC Internal Note No 69-FM-98 dated 12 May 1969
73 Pixley P T F Rendezvous Navigation Mission Techniques Panel Meeting Memo No 69-FM46-l07 dated 17 April 1969
74 Tindall H W Lunar Rendezvous Mission Techniques Memo No 68-PA-T-219A Dated 15 October 1968
75 Guidance System Operations Plan for Manned LM Earth Orbital and Lunar Missions Using Program Luminary 1A Section Four PGNCS Operational Modes Revision 1 dated April 1969
76 GAP Assemble Revision 097 of AGS Program Luminary by NASA 2021112-041 dated 11 April 1969
77 Grega S P LM Rendezvous Procedures D Mission Final Revision A dated 31 January 1969
78 Hutchins J E LM Rendezvous Procedures F Mission Final Revision A dated 28 April 1969
79 Apollo 11 Flight Plan AS-506CSM-107LM-5 Flight Planning Branch Flight Crew Support Division dated 15 April 1969
710 Apollo Mission Techniques Mission F and G Rendezvous Volume 1 dated 28 February 1969
711 Apollo LM-5 Flight Crew GampN Dictionary Guidance and Control Section Spacecraft Systems Branch Flight Crew Suport Division dated 25 April 1969
712 Apollo 11 Flight Mission Rules SA-506CSM-107LM-5 Flight Control Division dated 16 April 1969
713 LMAGS Operating Manual Flight Program 6 TRW Document I1176-6033-TOOO dated 6 April 1969
714 CSMLM Spacecraft Operational Data Book Volumes II III amp IV LM Data Book SNA-8-D-027 with Revisions through 2 April 1969