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
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