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1 SPIE – June 25, 2004 The Details….

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The Details…. Previous Focus Tracking Curves. Previous Focus Tracking Curves. Temperature Sensor Locations. T F1. T F5. T SR. T F3. T F4. T F2. T H3. T B2. T H2. T E2. T B1. T B3. T B4. T B5. T E1. T A4. T A2. T A3. T A1. Structural Temperatures. Focus Model. Gravity - PowerPoint PPT Presentation

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Page 1: The Details…

1SPIE – June 25, 2004

The Details….

Page 2: The Details…

2SPIE – June 25, 2004

Previous Focus Tracking Curves

Page 3: The Details…

3SPIE – June 25, 2004

Previous Focus Tracking Curves

Page 4: The Details…

4SPIE – June 25, 2004

Temperature Sensor Locations

TSR

TF1

TF4

TF5

TF3

TF2

TH2

TH3 TB2

TB1 TB3

TB5

TB4

TE1

TE2

TA3

TA1

TA2

TA4

Page 5: The Details…

5SPIE – June 25, 2004

Structural Temperatures

Page 6: The Details…

6SPIE – June 25, 2004

Focus Model

• Gravity

• SR-Primary

• VFA-Primary

• HFA

• BUS

Page 7: The Details…

7SPIE – June 25, 2004

Elevation Model

• Gravity

• BUS

• HFA

• VFA

• Alidade

Page 8: The Details…

8SPIE – June 25, 2004

Azimuth Model

• Gravity

• Alidade

• HFA

• BUS

• VFA

Page 9: The Details…

9SPIE – June 25, 2004

Optimization

• Focus optimization using pseudo-inverse for LSE solution

• Coupled Az and El gravity models (AN, AW constraint)– Gradient descent

Page 10: The Details…

10SPIE – June 25, 2004

• 100 x 110 m section of a parent parabola 208 m in diameter• Cantilevered feed arm is at focus of the parent parabola

Unblocked Aperture

Page 11: The Details…

11SPIE – June 25, 2004

Telescope Structure and Optics

Page 12: The Details…

12SPIE – June 25, 2004

Development Phases

Actual schedule:

Phase I: ??

Phase IIa (26GHz) Spring 2003

Page 13: The Details…

13SPIE – June 25, 2004

High Frequency Environmental Envelope

Page 14: The Details…

14SPIE – June 25, 2004

Pointing Accuracy, 5° C Gradient, 5° El

Loral Tech Memo 52 Table 2-20 El=5, T=5,Vw=0,Sun Az=180

Error Sources El Errors (arcsec) X-El Errors (arcsec)Repeatable Nonrepeatable Repeatable Nonrepeatable

Mechanical AlignmentsRF/El Axes Orthogonality 0.0 0.0El/Az Axes Orthogonality 0.0 5.2Az Axis Verticality 5.0 0.4Structural DeformationsReflectorWindThermal Gradient 0.3AlidadeWind Thermal Gradient 11.5Servo and Drive 0.9 0.3MiscellaneousEl Bearing Wobble 1.0 0.4 0.1 0.0Az Bearing Wobble 1.0 0.4 0.1 0.0Encoder Accuracy 1.2 1.2Encoder Coupling 1.8 2.1Encoder Referencing 10.0 10.0RSS Subtotals 11.3 12.1 11.3 2.4

Page 15: The Details…

15SPIE – June 25, 2004

Pointing

Page 16: The Details…

16SPIE – June 25, 2004

Focus

Page 17: The Details…

17SPIE – June 25, 2004

Data Quality

Jack Scan

Gaussian Fits (Az, El, Focus)

Polarization (LCP – RCP)

Direction (Forward – Backward)

Page 18: The Details…

18SPIE – June 25, 2004

Data Quality: Pointing (LCP – RCP)

Page 19: The Details…

19SPIE – June 25, 2004

Structural Temperature Sensors

• 19 locations, 0.2C interchangeable accuracy, 0.01C resolution, 1Hz, range –35 to 40C. (actual accuracy is ~0.1C, temp control of conversion elex)

• Design documentation:– PTCS Wiki (AntennaInstrumentation) – PTCS Project Note PTCS/PN12

• Accuracy tested in lab:– Solar/convective loading– Selected unit-to-unit accuracy, repeatability– Electronics temperature range

• RFI mitigated, ESD protected• Two thermistor failures, forensics with YSI• Integrated into M&C • First cut pointing, focus predictive algorithms tested

Page 20: The Details…

20SPIE – June 25, 2004

Focus Model Tests

• Wind < 2.5 m/s• 15° < elevation < 85° • 9/5 is NCP • 11/20 is all-sky• Excludes 1000-1800• Graphs show thermal

contributions only

Page 21: The Details…

21SPIE – June 25, 2004

Elevation Model Test

Page 22: The Details…

22SPIE – June 25, 2004

Elevation Model Test

Page 23: The Details…

23SPIE – June 25, 2004

Azimuth Model

Term Coefficient Min-Max Significance Parameter

M1 5.5862 4.0 22.4 Alidade M2 -8.0331 2.7 21.3 HFAM3 -1.6289 2.4 3.8 BUSM4 1.3683 2.0 2.8 VFAM5 3.4124 0.0 0.0 CA, d(0,0)M6 1.3223 0.7 1.0 NPAE, b(0,1)M7 3.5152 0.9 3.0 IA, d(0,1)M8 -2.4960 1.9 4.8 AW, b(1,1)M9 -1.3360 1.8 2.5 AN, a(1,1)

Page 24: The Details…

24SPIE – June 25, 2004

Azimuth Model Estimation

= 3.9

Page 25: The Details…

25SPIE – June 25, 2004

Azimuth Model Test

Page 26: The Details…

26SPIE – June 25, 2004

Azimuth Model Test

Page 27: The Details…

27SPIE – June 25, 2004

Holography Results

Page 28: The Details…

Finite Element Model Predictions

Page 29: The Details…

29SPIE – June 25, 2004

Efficiency and Beam Shape

Page 30: The Details…

30SPIE – June 25, 2004

Requirements for high-frequency observing

Page 31: The Details…

31SPIE – June 25, 2004

Requirements for high-frequency observing

Page 32: The Details…

32SPIE – June 25, 2004

Pointing Accuracy, 6 m/s wind

Error Sources El Errors (arcsec) X-El Errors (arcsec)Repeatable Nonrepeatable Repeatable Nonrepeatable

Mechanical AlignmentsRF/El Axes Orthogonality 0.0 0.0El/Az Axes Orthogonality 0.0 35.3Az Axis Verticality 5.0 2.9Structural DeformationsReflectorWind 10.5Thermal Gradient AlidadeWind 1.5Thermal Gradient Servo and Drive 0.9 0.3MiscellaneousEl Bearing Wobble 1.0 0.4 0.6 0.2Az Bearing Wobble 1.0 0.4 0.6 0.2Encoder Accuracy 1.2 1.2Encoder Coupling 1.8 1.7Encoder Referencing 10.0 8.1RSS Subtotals 11.3 12.3 36.4 2.1

Page 33: The Details…

33SPIE – June 25, 2004

Architecture of current GBT Observing System

Page 34: The Details…

34SPIE – June 25, 2004

Architecture of HFOS

Page 35: The Details…

35SPIE – June 25, 2004

Architecture of PCS

Page 36: The Details…

36SPIE – June 25, 2004

Telescope Structure and Optics

•Optics: 110 m x 100 m of a 208 m parent paraboloid•Effective diameter: 100 m•Offaxis feedarm

•Elevation Limit: 5degrees•Slew Rates: Azimuth – 40deg/min; Elevation – 20deg/min•Main Reflector: 2209 actuated panels with 68 m rms.

•Total surface: rms 400 m•FWHM Beamwidth: 740"/f(Ghz)•Prime Focus: Retractable boom•Gregorian Focus:

•8-m subreflector with 6-degrees of freedom•Rotating Turret with 8 receiver bays