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Fault-Tolerant Software For Flight ControlReport discusses design and testing of redundant control system for F-8 digital fly-by-wire airplane. Outstanding feature of system is fault-tolerant software (REBUS) residing in primary digital computers. Transition to operation on backup software smooth.
Document ID
19880000370
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Deets, Dwain A. (NASA Ames Research Center, Moffett Field, Calif.)
Lock, Wilton P. (NASA Ames Research Center, Moffett Field, Calif.)
Megna, Vincent A. (Charles Stark Draper Laboratory)
Date Acquired
August 13, 2013
Publication Date
July 1, 1988
Publication Information
Publication: NASA Tech Briefs
Volume: 12
Issue: 7
ISSN: 0145-319X
Subject Category
Electronic Systems
Report/Patent Number
ARC-11763
Accession Number
88B10370
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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