DocumentCode
2223393
Title
A Nonlinear Geometric Fault Detection and Isolation Approach for Almost-Lighter-Than-Air-Vehicles
Author
Meskin, N. ; Jiang, T. ; Sobhani, E. ; Khorasani, K. ; Rabbath, C.A.
Author_Institution
Dept. of Electr. & Comput. Eng., Concordia Univ., Montreal, QC
fYear
2007
fDate
1-3 Oct. 2007
Firstpage
1073
Lastpage
1078
Abstract
In this paper, the problem of actuator fault detection and isolation (FDI) for almost-lighter-than-air-vehicles (ALTAVs) is investigated using a nonlinear geometric approach. Due to the particular dynamics of the ALTAV, six detection filters are designed for FDI of the four input channels of the ALTAV. Four of the detection filters are designed such that each input channel affects only one of the actuators and the other two detection filters are affected by the corresponding two input channels. Using an appropriate combination of detection filters, one may detect and isolate the faults in all the input channels associated with single as well as simultaneous multiple actuators faults. Numerous simulation results demonstrate and show the excellent performance of the designed nonlinear detection filters.
Keywords
actuators; aircraft control; fault diagnosis; nonlinear control systems; almost-lighter-than-air-vehicles; fault isolation; multiple actuators faults; nonlinear geometric fault detection; six detection filters; Actuators; Control systems; Electrical fault detection; Fault detection; Fault diagnosis; Filters; Nonlinear control systems; Nonlinear systems; Research and development; Unmanned aerial vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Applications, 2007. CCA 2007. IEEE International Conference on
Conference_Location
Singapore
Print_ISBN
978-1-4244-0442-1
Electronic_ISBN
978-1-4244-0443-8
Type
conf
DOI
10.1109/CCA.2007.4389376
Filename
4389376
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