DocumentCode :
3546199
Title :
Actuator fault diagnosis based fuzzy multiple model structure for moving systems
Author :
Zheng, Zhiqiang ; Yuan, Haiwen ; Yang, Hao ; Yang, Qinghua
Author_Institution :
Sch. of Autom. Sci. & Electr. Eng., Beihang Univ., Beijing, China
fYear :
2009
fDate :
16-19 Aug. 2009
Abstract :
In this paper, the fuzzy multiple model scheme is proposed based on a suitable combination of Takagi-Sugeno(T-S) fuzzy model and multiple model technique for actuator failure. The non-linear system is described by T-S fuzzy model. Based on multiple model structure for locally linearized models, an adaptive observer approach is studied. The fuzzy adaptive observer is described by a fuzzy fusion of all locally adaptive observers. We developed an adaptive approach to estimate the unknown parameters on-line, so that the fault can be found when the fuzzy adaptive observer model matches the system and the lock-in-place fault can be estimate accurately. Numerical simulation results on an aircraft example show satisfactory performance of the proposed algorithm.
Keywords :
actuators; aerospace control; aircraft; fault diagnosis; fuzzy systems; numerical analysis; observers; Takagi-Sugeno fuzzy model; actuator fault diagnosis; flight control system; fuzzy adaptive observer model; fuzzy multiple model structure; lock-in-place fault; numerical simulation; Actuators; Aerospace control; Aircraft; Control systems; Fault diagnosis; Fault tolerant systems; Fuzzy systems; Instruments; Nonlinear dynamical systems; Space technology; T-S fuzzy model; fuzzy adaptive observer; fuzzy multiple model;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Electronic Measurement & Instruments, 2009. ICEMI '09. 9th International Conference on
Conference_Location :
Beijing
Print_ISBN :
978-1-4244-3863-1
Electronic_ISBN :
978-1-4244-3864-8
Type :
conf
DOI :
10.1109/ICEMI.2009.5274734
Filename :
5274734
Link To Document :
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