DocumentCode :
3550943
Title :
A model reference robust control and its application to autopilot control law design
Author :
Wenhan, Dong ; Xiuxia, Sun ; Yan, Lin ; Qingrong, Zhang
Author_Institution :
Inst. of Eng., Airforce Eng. Univ., Xi´´an, China
fYear :
2005
fDate :
8-10 June 2005
Firstpage :
2670
Abstract :
In this paper, a new model reference robust control (MRRC) scheme is proposed and is applied to autopilot control law design. By using our scheme, both the tracking performance and the control effort can be improved significantly. The simulation results of a pitch-attitude-hold autopilot design show that, even with the existence of plant uncertainty, nonlinear disturbance and unmodeled dynamics, the steady-state error of the step response is no more than 0.3 percent of the final value and, the amplitude of the control signal is only about 35 percent of that by using the traditional zero-pole placement control scheme.
Keywords :
aircraft control; attitude control; control nonlinearities; control system synthesis; robust control; step response; uncertain systems; autopilot control law design; model reference robust control; nonlinear disturbance; pitch-attitude-hold autopilot design; plant uncertainty; steady-state error; step response; unmodeled dynamics; Aerodynamics; Algorithm design and analysis; Automatic control; Control system synthesis; Design engineering; Nonlinear control systems; Robust control; Signal design; Sun; Uncertainty;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 2005. Proceedings of the 2005
ISSN :
0743-1619
Print_ISBN :
0-7803-9098-9
Electronic_ISBN :
0743-1619
Type :
conf
DOI :
10.1109/ACC.2005.1470371
Filename :
1470371
Link To Document :
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