Spacecraft fault tolerance: The Magellan experienceInterplanetary and earth orbiting missions are now imposing unique fault tolerant requirements upon spacecraft design. Mission success is the prime motivator for building spacecraft with fault tolerant systems. The Magellan spacecraft had many such requirements imposed upon its design. Magellan met these requirements by building redundancy into all the major subsystem components and designing the onboard hardware and software with the capability to detect a fault, isolate it to a component, and issue commands to achieve a back-up configuration. This discussion is limited to fault protection, which is the autonomous capability to respond to a fault. The Magellan fault protection design is discussed, as well as the developmental and flight experiences and a summary of the lessons learned.
Document ID
19950048808
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kasuda, Rick (Martin Marietta, Denver, CO US, United States)
Packard, Donna Sexton (Martin Marietta, Denver, CO US, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Publication Information
Publisher: American Astronautical Society (Advances in the Astronautical Sciences, Vol. 81)
ISSN: 0065-3438
Subject Category
Computer Programming And Software
Report/Patent Number
ISSN: 0065-3438
Accession Number
95A80407
Distribution Limits
Public
Copyright
Other
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Related Records
IDRelationTitle19950048790Collected WorksGuidance and control, 1993; Annual Rocky Mountain Guidance and Control Conference, 16th, Keystone, CO, Feb. 6-10, 199319950048790Collected WorksGuidance and control, 1993; Annual Rocky Mountain Guidance and Control Conference, 16th, Keystone, CO, Feb. 6-10, 1993