DocumentCode :
2297143
Title :
Design of FDI system for the nonlinear control system
Author :
Zhou, Jing ; Zhu, Xun
Author_Institution :
Sch. of Math. & Comput. Sci., Jianghan Univ., Wuhan, China
fYear :
2012
fDate :
6-8 July 2012
Firstpage :
2935
Lastpage :
2938
Abstract :
Contrary to the parameter-depended uncertainty system, the order of the linear matrix inequalities is reduced, then the RPRO fault detection and fault isolated filters are constructed. Then a RPRO fault isolation filter is designed for occurrence of both actuator fault and sensor fault in the aerocraft´s closed-loop control system, and fault diagnosis system is structured based on the fault isolation filters. Through the output of the fault diagnosis system, we can alarm the fault timely and the advantages of this approach are highlighted.
Keywords :
actuators; aircraft control; closed loop systems; fault diagnosis; filtering theory; linear matrix inequalities; nonlinear control systems; uncertain systems; FDI system design; RPRO fault detection; RPRO fault isolation filter; actuator fault; aerocraft closed-loop control system; fault diagnosis system; fault isolated filters; linear matrix inequality; nonlinear control system; parameter-depended uncertainty system; sensor fault; Actuators; Fault detection; Fault diagnosis; Mathematical model; Uncertainty; Vectors; RPRO; bias fault; fault detection and isolation; feature points; parameter-depended system;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Intelligent Control and Automation (WCICA), 2012 10th World Congress on
Conference_Location :
Beijing
Print_ISBN :
978-1-4673-1397-1
Type :
conf
DOI :
10.1109/WCICA.2012.6358372
Filename :
6358372
Link To Document :
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