DocumentCode :
2752064
Title :
A novel design for robust fault diagnostic observer
Author :
Xiong, Yi ; Saif, Mehrdad
Author_Institution :
Sch. of Eng. Sci., Simon Fraser Univ., Burnaby, BC, Canada
Volume :
1
fYear :
1998
fDate :
1998
Firstpage :
592
Abstract :
A new approach for the design of robust fault diagnostic observers is proposed in this article. The design is carried out through transformation of the system into its special coordinate basis (SCB) form, and with the aid of loop transfer recovery (LTR) like techniques. Furthermore, simple necessary and sufficient conditions for existence of perfect disturbance decoupled residual are presented. The proposed design approach offers computational simplicity and unifies approaches using eigenstructure assignment and unknown input observer design. Finally, an example dealing with sensor and actuator failure diagnosis of a vertical takeoff and landing- (VTOL) aircraft is given to illustrate the proposed approach
Keywords :
computational complexity; eigenstructure assignment; fault diagnosis; observers; LTR; SCB form; VTOL aircraft; actuator failure diagnosis; computational simplicity; eigenstructure assignment; loop transfer recovery; necessary and sufficient conditions; perfect disturbance decoupled residual; robust fault diagnostic observer; sensor failure diagnosis; special coordinate basis form; unknown input observer design; Air safety; Aircraft; Fault detection; Fault diagnosis; Observers; Redundancy; Robustness; Sensor systems; State estimation; Uncertainty;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Decision and Control, 1998. Proceedings of the 37th IEEE Conference on
Conference_Location :
Tampa, FL
ISSN :
0191-2216
Print_ISBN :
0-7803-4394-8
Type :
conf
DOI :
10.1109/CDC.1998.760743
Filename :
760743
Link To Document :
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