DocumentCode :
404551
Title :
Adaptive output feedback actuator failure compensation for a class of state-dependent nonlinear systems
Author :
Tang, Xidong ; Tao, Gang ; Joshi, Suresh M.
Author_Institution :
Dept. of Electr. & Comput. Eng., Virginia Univ., Charlottesville, VA, USA
Volume :
2
fYear :
2003
fDate :
9-12 Dec. 2003
Firstpage :
1681
Abstract :
This paper develops an adaptive output feedback control scheme for a class of nonlinear systems with state-dependent nonlinearities in the presence of unknown actuator failures. A robust backstepping feedback control law is derived to effectively handle the state estimation error due to such uncertain nonlinearities. An adaptive actuator failure compensation scheme is designed to ensure closed-loop signal boundedness and desired output tracking performance. An application to controlling the angle of attack of a nonlinear aircraft model in the presence of elevator segment failures is studied and simulation results are presented to illustrate the effectiveness of the adaptive actuator failure compensation design.
Keywords :
actuators; adaptive control; aircraft control; closed loop systems; control nonlinearities; control system synthesis; failure analysis; feedback; nonlinear control systems; robust control; state estimation; adaptive output feedback actuator failure compensation; adaptive output feedback control; closed-loop signal boundedness; elevator segment failures; nonlinear aircraft model; output tracking performance; robust backstepping feedback control law; state estimation error; state-dependent nonlinear systems; state-dependent nonlinearities; Actuators; Adaptive control; Backstepping; Control nonlinearities; Control systems; Nonlinear control systems; Nonlinear systems; Output feedback; Programmable control; Robust control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Decision and Control, 2003. Proceedings. 42nd IEEE Conference on
ISSN :
0191-2216
Print_ISBN :
0-7803-7924-1
Type :
conf
DOI :
10.1109/CDC.2003.1272854
Filename :
1272854
Link To Document :
بازگشت