This paper presents an integrated approach to fault detection, isolation, and fault tolerant control (FTC). In the proposed approach a constrained Kalman filter based fault detection and isolation (FDI) method (Larson et al., 2002) is modified to reduce its computation load and then applied to detect and isolate a faulty actuator or sensor. Explicit algorithms are derived to estimate the effectiveness factor of a detected faulty actuator or sensor. Furthermore, a design concept of actuation reconfiguration is proposed and implemented in the derived control scheme to restrain the workload of a faulty actuator while recovering the prefault system performance. Simulation results on an aircraft dynamic model have demonstrated the effectiveness of the proposed method.
Active fault tolerant control with actuation reconfiguration
IEEE Transactions on Aerospace and Electronic Systems ; 40 , 3 ; 1110-1117
2004-07-01
334057 byte
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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