The fault detection and accommodation (FDA) methods that can be used for digital engine control systems are presently subjected to a flight test program in the case of the F-15 fighter's F100 engine electronic controls, inducing selected faults and then evaluating the resulting digital engine control responses. In general, flight test results were found to compare well with both ground tests and predictions. It is noted that the inducement of dual-pressure failures was not feasible, since FDA logic was not designed to accommodate them.
Fault detection and accommodation testing on an F100 engine in an F-15 airplane
1985-07-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
NASA Lewis F100 engine testing
NTRS | 1984
|SAE Technical Papers | 1980
|Flight Research Using F100 Engine P680063 in the NASA F-15 Airplane
British Library Conference Proceedings | 1995
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