Describes development and analysis of a distributed failure detection and isolation system for commuter and business aircraft. We define several candidate failure scenarios (e.g., aircraft icing, failures of control surface actuators, stuck or floating control surfaces) that are both common occurrences and amenable to improved control solutions and construct a hybrid model, suitable for simulation studies. The development of an algorithm that can reliably detect and isolate system failures with minimal disruption of normal operations constitutes the heart of the paper.
Diagnostics for active management of aircraft system failures
2001 IEEE Aerospace Conference Proceedings (Cat. No.01TH8542) ; 7 ; 7-3187 vol.7
01.01.2001
856976 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
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