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Page 1: AIAA/IEEE Digital Avionics Systems Conference (DASC) ; 16 : … · 2008-07-15 · KentSmith Warner Robins Air Logistics Center Gary Miyahara Hughes Aircraft Company ix. WhyEngineersShouldConsider

AIAA/IEEE]

omcs

Office ofthe Under Secretary ofDefense(Acquisition and Technology)

Hughes Aircraft CompanySensors & Communications Systems

HUGHES

McDonnell Douglas AerospaceTransport Aircraft

MCDONNELL. DOUGLAS

Volume I

UMivr;r.p ;-rVf om tjuothCK. n

INFOHMA i l(j; £ciLJiJOTHEK

Page 2: AIAA/IEEE Digital Avionics Systems Conference (DASC) ; 16 : … · 2008-07-15 · KentSmith Warner Robins Air Logistics Center Gary Miyahara Hughes Aircraft Company ix. WhyEngineersShouldConsider

TABLE OF CONTENTS

Volume I

Special Session ofGeneral Interest o. o

David R. Morgan and hen Carlson

Digital Beam Forming for Tactical o. l -1Airborne Radars

Francis Hopwood, Kevin Leahy, and Anthony Difurio

Northrop Grumman, ESSD

The New Vision for Modeling and 0.2-1

Simulation in the DoD AcquisitionProcess

William K. McQuayUSAF Wright Laboratory

JSF Affordable Avionics Study 0.3-1

J. Groat, B. Sawamura, B, Spiers, K. Driscoll, B.Hancock, L. Valid and Jerry WaldHoneywell Technology Center

Shaping the National Airspace 0.4-1

System for the 21st CenturyGregory Burke

Federal Aviation Admin. (ASD)

The Flight 2000 Avionics Suite: 0.5-1

Paving the Way to Free FlightDeborah A. Kirkman

The MITRE CorporationDavid B. Tuttle

Federal Aviation Administration

Software Engineering 1.0

Marc Pitarys, USAF WL

Legacy SoftwareChair: Kenneth Littlejohn, USAF WL

COTS Initiative* Cost of S/W for 1.1-1

Aging Avionics UpgradesWilliam A. HannaMcDonnell Douglas Aerospace

Ada 95 and Software Reuse 1.1-11

George F. Rice and Sean CorcoranLockheed Martin Tactical Aircraft SystemsDebra Leibcrman and Richard PowersTexas Instruments

Designing for Determinism: Lessons 1.1-19

Learned from Modern Real-TimeAvionics ApplicationsJonathan D. Preston and Russell B. KegleyLockheed Martin Tactical Aircraft Systems

A Comparison of Computer-Assisted 1.1-27

Software Reengineering ApproachesRichard Falcioni and Carolyn BoctlcherHughes Aircraft Company

Automated Reengineering for Legacy 1.1-35Weapon System Software

Peter G. Clark and John A. GillTASC

Dale Harper and Kenneth Littlejohn,USAF Wright Laboratory

Retrospective Exploration of Safety 1.1-43

Properties in Real-Time ConcurrentSystemsNoah Prywes, Paul Rehmet, Oleg Sokolsky and InsupLee

Computer Command and Control Company

Software Architectures and DesignTechniques

Chair: Jonathan D. Preston

Reconciling Avionics Database 1.2-1

Management with SecurityMayford B. Roark

Lockheed Martin Tactical Aircraft Systems

Experience of Applying CORBA 1.2-8

Middleware to Air Traffic ControlAutomation SystemsWen-Der JiangLockheed Martin Air Traffic

Have the 1990's Changed the 1.2-I6

"Software Surgical Team"?John H. RobbLockheed Martin Tactical Aircraft Systems

A Performance Study of the 1.2-23

Concurrency Control Algorithms for

Real-Time Avionics Databases

Ching-Shan Peng and Kwei-Jay Lin

University of California Irvine

Languages, Tools and Environments

Chair: Eli Solomon, Northrop Grumman

Advanced Real-Time Embedded 1.3-1

System Tools for IntelligentArchitectures (ARTESIA)Michael Harrelson, David Zaleta and Dan BallardReticular Systems Inc.

Leveraging an Avionics Support 1.3-9

Environment for Shared Applicationto Multiple Platforms

Kent SmithWarner Robins Air Logistics Center

Gary MiyaharaHughes Aircraft Company

ix

Page 3: AIAA/IEEE Digital Avionics Systems Conference (DASC) ; 16 : … · 2008-07-15 · KentSmith Warner Robins Air Logistics Center Gary Miyahara Hughes Aircraft Company ix. WhyEngineersShouldConsider

Why Engineers Should Consider 1.3-16

Formal MethodsC. Michael HollowayNASA Langley Research Center

Integrating System Engineering 1.3-23

Software Tools

Edward Y. Chow

Hughes Aircraft Company

Software Testing, Validation and

CertificationChair: Minerva Rodriguez, Hughes Aircraft

Real-Time Checkers: Built-in-Test for 1.4-1

Mission-Critical Software

David C. Shreve, D. Joel Mellema and

Carolyn B. Boettcher

Hughes Aircraft Company

Application of Some Explicit 1.4-9

Formulas for the Matrix Exponentialin Linear Systems SoftwareValidation

Dr. Thomas H. Kerr III

TeK Associates

Haywood S. Satz

Spacecraft Systems 2.0

David M. Barnett

Multi-Chip Module (MCM) Implementationfor Spacecraft

ChairJim Lyke, Phillips Lab and Glenn

Forman, GE CRD

Fast and Flexible Development of 2.1-1

Multichip Modules for Space andOther High-Reliability ApplicationsJeffrey Banker and Jeremy BuckinghamPico Systems, Inc.

Robert Caffrey, Harry Shaw and Ann Garrison

NASA Goddard Space Flight Center

Recent Progress in Space-Based 2.1-7

Micro-Controller DesignKeith AveryNichols Research CorporationDavid R. Alexander

Mission Research Corporation

Employing Radiation Hardness by 2.1-15

Design Techniques with Commercial

Integrated Circuit Processes

David G. Mavis and David R. AlexanderMission Research Corporation

Design and Fabrication of a Tri-C30 2.1-23

Multichip Module Building Block

Jim StaggsNichols FederalJimSmithMission Research Corporation

Developing Plug-and-Play Spacecraft 2.1-28

Systems: NASA Goddard SpaceFlight Center's (GSFC) EssentialServices Node (ESN)Robert Caffrey and Harry Shaw

NASA Goddard Space Flight CenterLeon WagnerFORTH Inc.

Single Chip Fault Tolerant Clock for 2.1 -3 6

Integrated Modular Avionics

T. Kien TruongBoeing Commercial Airplane Group

Micro-science: Instrument Needsfor the

Next Generation ofSmall SpacecraftChairs: Dr. Sue Smrekar and Chris Stevens, JPL

A Distributed Spacecraft Thermal 2.2-1

Control Architecture Using the Dallas

Semiconductor MicroLAN Products

Douglas W. CaldwellJet Propulsion Laboratory

Space Mission Applications of 2.2-9

Chemical Microsensors

Dr. Bruce H. Weiller

Aerospace Corporation

Miniature Magnetic Resonance 2.2-14

SpectrometersSoon SamKim, Narayan R. Mysoor, Steven R. Carnesand Christopher T. UlmerUlmer Systems, Inc.

Klaus Halbach

Jet Propulsion Laboratory

Design and Development of High 2.2-24

Capacity Spaceborne MemoryModules in the High DensityInterconnect (HDI) Technology for

Tropical Rainfall Measuring Mission

(TRMM)Jack McCabeNASA Goddard Space Flight CenterDan Dalton, Jackson & Tull

Jim LykePhilips Laboratory

Interaction Between Electronics and

Packaging in Small SpacecraftChairs: Saverio D'Agostino and John Olivas,

JPL

Multifunctional Structures 2.3-1

Technology Experiment on DeepSpace 1 Mission

David M. Barnett and Suraj P. Rawal

Lockheed Martin

Towards an Ultra-High Density 2.3-8

Interconnect (UHDI) TechnologyVikram Krishnamurthy, J. Rose, R. Saia, K. Durocher

GE - Corporate Research and Development

X

Page 4: AIAA/IEEE Digital Avionics Systems Conference (DASC) ; 16 : … · 2008-07-15 · KentSmith Warner Robins Air Logistics Center Gary Miyahara Hughes Aircraft Company ix. WhyEngineersShouldConsider

Efficient Heterogenous Three- 2.3-13

Dimensional Packaging at a SystemLevel

Jim LykePhilips Laboratory/VTMI

Low Profde DC-DC Power 2.3-21

Converter for 3-D Electronics

AssemblyC.S. Korman, S. Ramakrishnan, R. Steigerwald, R.Fisher, W. Bicknell, W. Hennessy, R. WojnarowskiGE - Corporate Research and DevelopmentA. Peczalski and S. BaierHoneywell Technology Center

Integrated Avionics 3.0

Erv Ulbrich, The Boeing Company

Commercial SystemsChair: Steve Grothe, Honeywell, Inc

Controlled Flight Into Terrain and 3.1-1the Enhanced Ground ProximityWarning SystemBarry C. Breen

AlliedSignal Commercial Avionics Systems

The Next Step Towards Enhanced 3.1-8

Situational AwarenessErwin UlbrichMcDonnell Douglas

Boeing 777 Airplane Information 3.1-21

Management System OperationalExperienceBrian Aleksa and Joseph Carter

Honeywell, Inc.

ADS-B/CDTI Capabilities for Near 3.1-28Term Deployment: Some EarlyResults

Anand Mundra, James J. Cieplak, David A. Domino,Baltazar O. Olmos and Hans P. StassenThe MITRE Corporation

MEMS Application in Tactical 3.1-36

Aircraft SystemsEdward. L. Safford III

Lockheed Martin Tactical Aircraft Systems

Military SystemsChair: Ken Jongsma, Honeywell, inc

Avionics Architecture Study for Air 3.2-1

Mobility Command Aircraft

Brian E. White

The MITRE Corporation

Phenomenology of Integrated 3.2-8Avionics and the Currently FieldedAircraft Market

Mark MingesUSAF WL/AAMI

Incremental Avionics Upgrades for 3.2-15

Legacy Aircraft

James Nelson

Northrop Grumman Corporation

Structured Definition ofModular 3.2-24

Avionics Architectures UsingBlueprintsAntonio Marchetto

Alenia Aeronautica

Enhanced Fault Management for 3.2-32

Future IMA SystemsGeoff W. Wilcock

Defense Evaluation & Research Agency (DERA)

Avionics Network SystemsChair: Rick Stevens, Lockheed Martin

The ACE Family of Mil-STD-1553 3.3-1

Terminals Gets SmallerSteven Friedman

ILC Data Devices Corporation

Trade Study Report for Commercial 3.3-5Candidates in an Embedded Avionics

Unified Network

Timothy P. BoggessLockheed Martin - Sanders

Optical Communication for 3.3-12Advanced Avionics SystemsRick C. Stevens and Gerald F. SauterLockheed Martin TDS

Ritch A. SelfridgeAmphenol Aerospace

Open SystemsChair: Lt Col Glen Logan

Open Systems Ada Technology 3.4-1Demonstration ProgramDon C. Winter and Brian D. RestThe Boeing Company

Open Systems Architecture for 3.4-8

Integrated RF Electronics

Dean C. HooksMcDonnell Douglas CoBarry A. Rich

Sanders, A Lockheed Martin Company

Test and Assessment 4.0

Steve Runo, Teledyne Controls

Susceptibility ofAircraft Avionics

Chair: Gerry Fuller, Veda, Inc

Further Analysis of CV-580 and B- 4.1-1

727 aircraft RF Coupling ExperimentData

R. Wayne Devereux and Gerald L. Fuller

Veda, Inc.

Raymond SchillingerFAA Technical Center

xi

Page 5: AIAA/IEEE Digital Avionics Systems Conference (DASC) ; 16 : … · 2008-07-15 · KentSmith Warner Robins Air Logistics Center Gary Miyahara Hughes Aircraft Company ix. WhyEngineersShouldConsider

EMI From Sources in the Cargo Bay 4.1-9

Anthony Cerino

FAA Technical Center

Gerald Fuller and R. Wayne Devereux

Veda, Inc.

Electromagnetic Susceptibility of 4.1-17

Installed Avionics

R. Wayne Devereux and Gerald L. Fuller

Veda, Inc.

Ray SchillingerFAA Technical Center

Using a Decision Analysis Tool for 4.1-25

Assessing Tradeoffs of HardeningCommercial Aircraft Against New E3Threats

R. Wayne Devereux

Veda Inc.

Open-Loop HIRF Experiments 4.1-33

Performed on a Fault Tolerant FlightControl ComputerDaniel M. KoppenNASA Langley Research Center

Closed-Loop HIRF Experiments 4.1-40

Performed on a Fault Tolerant FlightControl ComputerCeleste Belcastro

NASA Langley Research Center

Electromagnetic Testing ofAircraft and

Systems; Testing Techniques and Test

Facilities

Chair: Dr. Celeste Belcastro, NASA LRC

Wide Band Modulation of Conducted 4.2-1

Susceptibility SignalsKenneth A. BrezinskiNaval Air Warfare Center

On Field-to-Wire Coupling Versus 4.2-9

Conducted Injection TechniquesKen Javor

Sverdmp Technology

The NASA High Intensity Radiated 4.2-17

Fields LaboratoryReuben A. Williams

NASA Langley Research Center

A Proposed HIRF Test Facility for 4.2-22

Aircraft TestingDiane R. KempfNaval Air Warfare Center

Recent Developments Relevant to 4.2-26

Implementation of a Hybrid TEMCell/Reverberation Chamber HIRFTest FacilityT. H. Lehman, Gustav J. Freyer and M.L. Crawford

Science & Engineering Associates, Inc.

Michael O. Hatfield

Naval Surface Warfare Center

Electromagnetic Mitigation EngineeringChair: Bill Larsen FAA/ARC

Statistical Study of the Distance of 4.3

Closest Approach of Aircraft to

Ground Based Emitters

Dr. James R. Elliott and Dr. Rodney A. Perela

Electro Magnetic Applications, Inc.

Computing Platform Architectures 4.3

for Robust Operation in the Presence

of Lightning and Other

Electromagnetic ThreatsRichard Hess

Honeywell Inc.

Assessment of Analytical Codes for 4.3

Use in Modeling Aircraft OnboardEMI Threats

R. Wayne Devereux, Gerald L. Fuller and Bruce

Archambeault

Veda, Inc.

Fiber Optic Backplane for Reducing 4.3

HIRF Effects in Fault Tolerant

Computing Platforms

Mahyar MalekpourNASA Langley Research Center

Safety Assessment and Fault AnalysisChair: John Dalton, Boeing Commercial

Boeing's Safety Assessment Processes 4.4

for Commercial Airplane DesignsJeff Hasson

Boeing Commercial Airplane GroupDavid CrottyScitor Corporation

The Application of Failure Mode and 4.4

Effect Analysis for Software in DigitalFly Control SystemsHao ChunpingChinese Academy of Space TechnologyLi Peiqiong and Yao YipingUniversity of Aeronautics and Astronautics China

Test Methods and Facilities

Chairs: Keyur Patel, JPL and Tom McCarthy,

Boeing Commercial

Data Analysis System for the F-16 4.5

Galen F. Atkinson and Stewart C. Austin

Lockheed Martin TAS

Deep Space One Basebody Control: 4.5

Validating the Data Path from

Computer to Thruster

Paula J. Pingree, C. Frank Leang and Ralph R. Basilio

Jet Propulsion Laboratory

The TSTAR Autonomy Test Tool 4.5

Kirk Reinholtz and Dan Dvorak

Jet Propulsion Laboratory

xii

Page 6: AIAA/IEEE Digital Avionics Systems Conference (DASC) ; 16 : … · 2008-07-15 · KentSmith Warner Robins Air Logistics Center Gary Miyahara Hughes Aircraft Company ix. WhyEngineersShouldConsider

Automated Computer Aided 4.5-21

Diagnosis and SimulationAli Abou-Khalil and Mark A. BoydNASA Ames Research CenterSabina JosephWest Virginia University

Sensors and Computing Resources s. o

Larry On, NavMar

RF andEO/IR SensorsChairs: Harvey Sokoloff, NAWC and Dr.

Joseph Yang, Northrop Grumman

An Open System Architecture for 5.1-1

Integrated RF SystemsRay Brousseau

Lockheed Martin- SandersDean R. Huffman, Northrop GrummanHal Abercrombie, Harris CorpDennis L. Hoffman; Rockwell Avionics & Comm

Spencer Coleman, Lockheed Martin TAS

Electro-Optical Sensors Overview 5.1 - 7

Fred I. Crawford

Hughes Aircraft Company

Processing Requirements for the First 5.1-15

Electro-Optic System of the Twenty-First CenturyWilliam F.O'Neil

Northrop Grumman Corporation

Passive Millimeter Wave Imaging 5.1-23

Sensor Enhanced Vision SystemAlberto OrtizThe Boeing Company

Future NASA Spaceborne SAR 5.1-31Missions

Jeffrey E. Hilland, Frederick V. Stuhr, AnthonyFreeman, David Imel, Yuhsyen Shen, Rolando L.

Jordan, and Edward R. CaroJet Propulsion Laboratory

Processors

Chair: Laurence Hart, NAWC

Design and Implementation of 5.2-1

Network Services that Provide End-

to-End QoS in ATM-Based Real-

Time Environments

Chao-Ju Jennifer Hou Ching-Chih Han, Hung-YingTyan, Bin Wang, and Yi Ye

the Ohio State University

Scalable Open Architectures Project 5.2-10

(SOAP): Avionics Evolution from

Federated to Open SystemsJuris Ozols

Computing Devices Int'l

Object Request Broker Software 5.2

Technology: Applications in an

Advanced Open Systems AvionicsArchitectureRobert Pedersen

Computing Devices Int'l

A Minimalist Hardware Architecture 5.2

for Using Commercial

Microcontrollers in SpaceDoug W. Caldwell

Jet Propulsion LaboratoryDavid A. RennelsUCLA

Data Fusion

Chair: Robert Carson, Northrop Grumman

Learning Attributes for Situational 5.3

Awareness in the Landing of anAutonomous AirplaneLt. Erik P. Blasch

USAF WL/AACF

Fusion of IFF and Radar Data 5.3Robert R. Carson, Jr. Michael P. Meyer and Douglas J.Peters

Northrop Grumman Norden Systems

Adaptive Interacting Multiple Model 5.3

Tracking of Maneuvering TargetsDr. Jeffery R. LayneUSAF WL/AACFUditha C. PiyasenaUSAF Academy

Visualization TechnologyChair: Christof Heithecker, NAWC

3D Object to 2D Image Invariance 5.4

Technology for Visualization

Problems

Scott D. Kushnier and Dr. Robert M. WilliamsNaval Air Warfare Center

Airborne Tactical Information 5.4

Management System SyntheticEnvironment Demonstration

Dr. Lyle Reibling and Mark StorerGDE Systems, Inc.

Roger LoganNAVAIR PMA-233

Dave Churchman

Boeing Defense & Space Grp

Maritime Avionics Subsystems and 5.4

Technologies: Advanced Graphicsand Data Fusion

Floyd Adagio and Nicholas Babiak

Cambridge Research Associates

Kenneth BollingerDefense Micro-Electronic ActivityCharles CaposellNaval Air Systems Command

xiii