DocumentCode :
1117931
Title :
Active fault tolerant control with actuation reconfiguration
Author :
Guangjun Liu ; Dejun Wang
Author_Institution :
Dept. of Aerosp. Eng., Ryerson Univ., Toronto, Ont., Canada
Volume :
40
Issue :
3
fYear :
2004
fDate :
7/1/2004 12:00:00 AM
Firstpage :
1110
Lastpage :
1117
Abstract :
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.
Keywords :
Kalman filters; actuators; aircraft; control theory; fault location; fault tolerance; sensors; Kalman filter; active control; actuation reconfiguration; aircraft dynamic model; computation load reduction; effectiveness factor estimation; explicit algorithms; fault detection; fault isolation; fault tolerant control; faulty actuator; faulty sensor; prefault system performance; workload restraining; Actuators; Aircraft; Control systems; Fault detection; Fault tolerance; Noise measurement; Redundancy; Sensor systems; System performance; Time measurement;
fLanguage :
English
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9251
Type :
jour
DOI :
10.1109/TAES.2004.1337485
Filename :
1337485
Link To Document :
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