DocumentCode :
3390912
Title :
Intelligent adaptive Control and Simulation for a Spin Missile
Author :
Xiaozhu, Xie ; Zaozhen, Liu ; Zhilin, Luo
Author_Institution :
Dept. of Inf. Eng., Acad. of Armored Force Eng., Beijing
fYear :
2008
fDate :
10-12 Oct. 2008
Firstpage :
647
Lastpage :
651
Abstract :
This paper proposed a new intelligent controller for a spin missile with uncertainty and unknown parameter. The spin missile controller expression with undetermined parameters can be acquired by using adaptive backstepping design idea, and the controller parameters are optimized online by using genetic algorithm. By using this new method proposed in this paper, not only the stability of the spin missile control system can be acquired more easily but also the dynamic behavior of the spin missile system is good. The simulation shows that the controller is valid.
Keywords :
adaptive control; control nonlinearities; control system synthesis; genetic algorithms; intelligent control; missile control; stability; uncertain systems; adaptive backstepping design; genetic algorithm; intelligent adaptive control; optimization controller design; spin missile control system; stability; uncertain system; Adaptive control; Algorithm design and analysis; Backstepping; Design optimization; Genetic algorithms; Intelligent control; Missiles; Programmable control; Stability; Uncertainty;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
System Simulation and Scientific Computing, 2008. ICSC 2008. Asia Simulation Conference - 7th International Conference on
Conference_Location :
Beijing
Print_ISBN :
978-1-4244-1786-5
Electronic_ISBN :
978-1-4244-1787-2
Type :
conf
DOI :
10.1109/ASC-ICSC.2008.4675440
Filename :
4675440
Link To Document :
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