DocumentCode :
1477408
Title :
Brief paper state-feedback gain design for a class of relay control systems
Author :
Su, Jien-Yin ; Tie, Lin ; Wang, Xiang-Hua ; Cai, K.-Y.
Author_Institution :
Dept. of Autom. Control, Beijing Univ. of Aeronaut. & Astronaut., Beijing, China
Volume :
5
Issue :
2
fYear :
2011
Firstpage :
409
Lastpage :
419
Abstract :
In this paper, an approach to design state-feedback gain is proposed for a class of relay control systems. The resulting controller can drive states of the systems to desired limit cycles. The design consists of two steps. First, the form of the state-feedback gain is proposed. It is proved that each gain in the proposed form can guarantee the existence and stability of a limit cycle. Then, by an exact method, the value of state-feedback gain is chosen to obtain the limit cycle with prescribed characteristics. In order to demonstrate the effectiveness, the proposed approach is applied to the attitude control of a torpedo. Simulation results show that the designed relay controller drives the state of the torpedo to a limit cycle with desired amplitude and frequency.
Keywords :
attitude control; control system synthesis; missiles; relay control; state feedback; attitude control; relay control system; stability; state feedback gain design; torpedo;
fLanguage :
English
Journal_Title :
Control Theory & Applications, IET
Publisher :
iet
ISSN :
1751-8644
Type :
jour
DOI :
10.1049/iet-cta.2009.0472
Filename :
5735537
Link To Document :
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