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