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