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Fault detection and accommodation testing on an F100 engine in an F-15 airplaneThe 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.
Document ID
19850058679
Document Type
Conference Paper
Authors
Myers, L. P. (NASA Flight Research Center Edwards, CA, United States)
Baer-Riedhart, J. L. (NASA Flight Research Center Edwards, CA, United States)
Maxwell, M. D. (United Technologies Corp. Pratt and Whitney Aircraft Group, West Palm Beach, FL, United States)
Date Acquired
August 12, 2013
Publication Date
July 1, 1985
Subject Category
AIRCRAFT PROPULSION AND POWER
Report/Patent Number
AIAA PAPER 85-1294
Distribution Limits
Public
Copyright
Other