Report 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.
Fault-Tolerant Software For Flight Control
NASA Tech Briefs ; 12 , 7
1988-07-01
Sonstige
Keine Angabe
Englisch
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