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Development and flight test experiences with a flight-crucial digital control systemEngineers and scientists in the advanced fighter technology integration (AFTI) F-16 program investigated the integration of emerging technologies into an advanced fighter aircraft. AFTI's three major technologies included: flight-crucial digital control, decoupled aircraft flight control, and integration of avionics, flight control, and pilot displays. In addition to investigating improvements in fighter performance, researchers studied the generic problems confronting the designers of highly integrated flight-crucial digital control. An overview is provided of both the advantages and problems of integration digital control systems. Also, an examination of the specification, design, qualification, and flight test life-cycle phase is provided. An overview is given of the fault-tolerant design, multimoded decoupled flight control laws, and integrated avionics design. The approach to qualifying the software and system designs is discussed, and the effects of design choices on system qualification are highlighted.
Document ID
19890014956
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Mackall, Dale A.
(NASA Flight Research Center Edwards, CA, United States)
Date Acquired
September 5, 2013
Publication Date
November 1, 1988
Subject Category
Aircraft Stability And Control
Report/Patent Number
H-1344
NAS 1.60:2857
NASA-TP-2857
Report Number: H-1344
Report Number: NAS 1.60:2857
Report Number: NASA-TP-2857
Accession Number
89N24327
Funding Number(s)
PROJECT: RTOP 999-12-08
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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