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
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