DocumentCode :
3017727
Title :
Development and testing of advanced redundancy management methods for the F-8 DFBW aircrapt
Author :
Deyst, J. ; Deckert, J. ; Desai, M. ; Willsky, A.
Author_Institution :
Charles Stark Draper Laboratory, Cambridge, Massachusetts
fYear :
1977
fDate :
7-9 Dec. 1977
Firstpage :
309
Lastpage :
315
Abstract :
A reliable aircraft sensor failure detection and identification (FDI) technique is presented. The technique exploits the kinetic 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 flyby-wire (DFBW) research aircraft.
Keywords :
Aerospace control; Aircraft; Detectors; Fault detection; Instruments; Laboratories; Redundancy; Robustness; Sequential analysis; Testing;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Decision and Control including the 16th Symposium on Adaptive Processes and A Special Symposium on Fuzzy Set Theory and Applications, 1977 IEEE Conference on
Conference_Location :
New Orleans, LA, USA
Type :
conf
DOI :
10.1109/CDC.1977.271590
Filename :
4045860
Link To Document :
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