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An innovative design for autonomous backup attitude control of the Gamma Ray ObservatoryThe Gamma Ray Observatory is a NASA funded three-axis stabilized spacecraft which will carry four scientific instruments to observe gamma ray phenomena. The requirement to protect the scientific mission from system failures led to the attitude control and determination system design described in this paper. The design employs nine control modes with error detection, hardware substitution, and autonomous mode switching. The system architecture evolved to eliminate cross-dependence between the primary on-board computer (OBC) and the backup control processor electronics. Cross strapping of sensors and actuators and separation of the input/output electronics ensure that a reliable set of sensors and actuators will be available for backup mode operation. The OBC software includes failure detection, hardware reconfiguration, and mode switching logic which provide the ability to autonomously transfer, upon anomaly, to a reliable backup mode. Verification of this mode transition design is done in four test programs: at the unit level, by analytical simulation, by a hybrid breadboard electronics-simulation setup, and by a flight hardware-simulation test.
Document ID
19870063289
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Tai, F.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Kascak, N.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Mclaughlin, K.
(TRW, Inc. TRW Space and Technology Group, Redondo Beach, CA, United States)
Ward, B.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1987
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 87-2601
Accession Number
87A50563
Distribution Limits
Public
Copyright
Other

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