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AFTI/F-16 flight test results and lessonsThe advanced fighter technology integration (AFTI) F-16 aircraft is a highly complex digital flight control system integrated with advanced avionics and cockpit. The use of dissimilar backup modes if the primary system fails requires the designer to trade off system simplicity and capability. The tradeoff is evident in the AFTI/F-16 aircraft with its limited stability and fly by wire digital flight control systems when a generic software failure occurs the backup or normal mode must provide equivalent envelop protection during the transition to degraded flight control. The complexity of systems like the AFTI/F-16 system defines a second design issue, which is divided into two segments: (1) the effect on testing, (2) and the pilot's ability to act correctly in the limited time available for cockpit decisions. The large matrix of states possible with the AFTI/F-16 flight control system illustrates the difficulty of both testing the system and choosing real time pilot actions. The third generic issue is the possible reductions in the user's reliability expectations where false single channel information can be displayed at the pilot vehicle interface while the redundant set remains functional.
Document ID
19840007091
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ishmael, S. D.
(NASA Ames Research Center Moffett Field, CA, United States)
Mcmonagle, D. R.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 4, 2013
Publication Date
October 1, 1983
Subject Category
Aircraft Stability And Control
Report/Patent Number
H1206
NAS 1.15:84920
NASA-TM-84920
Report Number: H1206
Report Number: NAS 1.15:84920
Report Number: NASA-TM-84920
Meeting Information
Meeting: Symp. of the Soc. of Exptl. Test Pilots
Location: Beverly Hills, CA
Country: United States
Start Date: September 28, 1983
End Date: October 1, 1983
Accession Number
84N15159
Funding Number(s)
PROJECT: RTOP 533-02-61
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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