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Intelligent Automatic Fault Detection for Actuator Failures in Aircraft

โœ Scribed by Lo, C.H.; Fung, E.H.K.; Wong, Y.K.


Book ID
115535151
Publisher
Institute of Electrical and Electronics Engineers
Year
2009
Tongue
English
Weight
592 KB
Volume
5
Category
Article
ISSN
1551-3203

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Multiple model adaptive estimation (MMAE) methods have been incorporated into the design of a #ight control system for the variable in-#ight stability test aircraft (VISTA) F-16, providing it with the capability to detect and compensate for sensor and control surface/actuator failures. The algorithm