DocumentCode :
2393949
Title :
Reliable control system design against feedback failures with applications to aircraft control
Author :
Zhao, Qing ; Jiang, Jin
Author_Institution :
Dept. of Electr. Eng., Univ. of Western Ontario, London, Ont., Canada
fYear :
1996
fDate :
15-18 Sep 1996
Firstpage :
994
Lastpage :
999
Abstract :
A novel method is presented to synthesize a reliable controller for multivariable systems possessing actuator redundancies. The designed controller will be able to guarantee the stability of the closed-loop system and to maintain an acceptable performance in the event of actuator failures. The method is based on robust pole region assignment techniques with the help of a pre-compensator to modify the dynamic characteristics of the redundant actuator control channels. The effectiveness of this method has been verified on an aircraft bank control system design. The results indicate that the proposed design method is indeed very effective in achieving the closed-loop system integrity in the presence of actuator failures
Keywords :
aircraft control; closed loop systems; control system synthesis; feedback; multivariable control systems; pole assignment; reliability; robust control; actuator failures; actuator redundancies; aircraft bank control; closed-loop system; feedback failures; multivariable systems; redundant actuator control channels; reliable control system design; robust pole region assignment techniques; Actuators; Aircraft; Control system synthesis; Control systems; Feedback; MIMO; Maintenance; Redundancy; Robust control; Stability;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Applications, 1996., Proceedings of the 1996 IEEE International Conference on
Conference_Location :
Dearborn, MI
Print_ISBN :
0-7803-2975-9
Type :
conf
DOI :
10.1109/CCA.1996.559051
Filename :
559051
Link To Document :
بازگشت