DocumentCode
2848922
Title
Finite-time attitude control for bank-to-turn missiles
Author
Wang, Zhao ; Li, Shihua ; Fei, Shumin
Author_Institution
Coll. of Inf. & Control Eng., China Univ. of Pet., Dongying, China
fYear
2010
fDate
26-28 May 2010
Firstpage
2019
Lastpage
2024
Abstract
The design of a continuous finite-time controller for bank-to-turn(BTT) missiles is considered in this work. The proposed controller allows that roll rate and angle of attack can track the desired commands in finite-time with sideslip angle maintained in a small degree range. Based on input/output(I/O) feedback linearizaiton technique and finite-time stability results for homogenous system, a continuous finite-time controller is proposed. Compared with asymptotically stable systems, finite-time stable systems offer better robustness and disturbance rejection properties. Computer simulation results are presented to validate the effectiveness of our method.
Keywords
asymptotic stability; attitude control; continuous time systems; linearisation techniques; missile control; state feedback; asymptotically stable system; bank-to-turn missiles; continuous finite time controller; disturbance rejection property; feedback linearizaiton technique; finite time attitude control; finite time stability; homogenous system; Automatic control; Control engineering; Control systems; Design automation; Educational institutions; Linear feedback control systems; Missiles; Output feedback; Petroleum; Stability; Attitude Control; BTT Missiles; Finite-time Control;
fLanguage
English
Publisher
ieee
Conference_Titel
Control and Decision Conference (CCDC), 2010 Chinese
Conference_Location
Xuzhou
Print_ISBN
978-1-4244-5181-4
Electronic_ISBN
978-1-4244-5182-1
Type
conf
DOI
10.1109/CCDC.2010.5498889
Filename
5498889
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