DocumentCode :
486547
Title :
Reachable Outputs in Systems with Bounded Parameter Uncertainties: Application to Failure Detection
Author :
Horak, Dan T. ; Goblirsch, David M.
Author_Institution :
Bendix Aerospace Technology Center, 9140 Old Annapolis Road, Columbia, Maryland 21045
fYear :
1986
fDate :
18-20 June 1986
Firstpage :
301
Lastpage :
308
Abstract :
A method for computing the intervals in which the outputs of a linear multivariable dynamic system with bounded parameter uncertainties and noise must lie has been developed. It utilizes Pontryagin´s Maximum Principle and is recursive. Because of its computational efficiency it can be executed in real time and used for system and sensor failure detection in systems with parameter uncertainties. Failures are detected by testing if the measured outputs lie outside the computed intervals, indicating that the system cannot be described by the given model and the specified parameter uncertainty bounds. The method is illustrated by application to the longitudinal dynamics of the AFTI F-16 aircraft.
Keywords :
Aerodynamics; Aerospace control; Aircraft navigation; Computational efficiency; Condition monitoring; Power system modeling; Real time systems; Robustness; Uncertain systems; Uncertainty;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 1986
Conference_Location :
Seattle, WA, USA
Type :
conf
Filename :
4788952
Link To Document :
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