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Development and testing of advanced redundancy management methods for the F-8 DFBW aircraftA reliable aircraft sensor failure detection and identification (FDI) technique is presented. The technique exploits the kinematic and dynamic relationships that exist between variables measured by dissimilar sensors to identify failures in the sensors. The method is applied to management of dual redundant sensors on the NASA F-8 digital fly-by-wire (DFBW) research aircraft.
Document ID
19790030963
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Deyst, J. (Draper (Charles Stark) Lab., Inc. Cambridge, MA, United States)
Deckert, J. (Draper (Charles Stark) Lab., Inc. Cambridge, MA, United States)
Desai, M. (Charles Stark Draper Laboratory, Inc. Cambridge, Mass., United States)
Willsky, A. (MIT Cambridge, Mass., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1977
Subject Category
Aircraft Stability And Control
Meeting Information
Meeting: Conference on Decision and Control, and Symposium on Adaptive Processes, 16th, and Special Symposium on Fuzzy Set Theory and Applications
Location: New Orleans, LA
Start Date: December 7, 1977
End Date: December 9, 1977
Accession Number
79A14976
Funding Number(s)
CONTRACT_GRANT: NAS4-2409
Distribution Limits
Public
Copyright
Other

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