DocumentCode
3218773
Title
Adaptive Backstepping Decentralized Sliding Mode Control for Low Speed Spinning Ballistic Missile
Author
Wang Zhi ; Zhou Jun ; Zhou Fengqi
Author_Institution
Coll. of Astronaut., Northwestern Polytech. Univ., Xi´an, China
fYear
2006
fDate
7-11 Aug. 2006
Firstpage
947
Lastpage
951
Abstract
The dynamics model of ballistic missile is established which spins during the first boosting phase, and its control mechanism is analyzed. Based on the backstepping algorithm, a decentralized sliding mode controller is designed to restrain external disturbances and parameter perturbations. Owing to the bound of the lumped uncertainty is difficult to obtain in advance, an adaptive law is introduced to estimate the value of the lumped uncertainty in real-time. Eventually, the numerical simulation results are given to show the effectiveness of the proposed control scheme.
Keywords
adaptive control; ballistics; decentralised control; missile control; uncertain systems; variable structure systems; adaptive backstepping decentralized sliding mode control; adaptive law; external disturbances; low speed spinning ballistic missile; parameter perturbations; Adaptive control; Algorithm design and analysis; Backstepping; Boosting; Missiles; Numerical simulation; Programmable control; Sliding mode control; Spinning; Uncertainty;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference, 2006. CCC 2006. Chinese
Conference_Location
Harbin
Print_ISBN
7-81077-802-1
Type
conf
DOI
10.1109/CHICC.2006.280814
Filename
4060667
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