Attitude control of missile via Fliess expansion and model predictive control

Author

Qiao, Yupeng ; Yang, Baoqing ; Cheng, Daizhan

Author_Institution

Inst. of Syst. Sci., Chinese Acad. of Sci., Beijing

fYear

2008

fDate

25-27 June 2008

Firstpage

1527

Lastpage

1532

Abstract

This paper considers the attitude control of missile. We convert the problem into an output tracking one of nonlinear systems via control with finite admissible values. First, the Fliess functional expansion is used to describe the outputs. Then under piece-wise admissible value control and the quadratic criteria, the optimal control is obtained using model predictive control. The method developed is used to the attitude control of missile. Simulation results show the effectiveness of the proposed method.

Keywords

attitude control; missile control; nonlinear control systems; predictive control; Fliess expansion; attitude control; finite admissible values; missile control; model predictive control; nonlinear systems; optimal control; piece-wise admissible value control; quadratic criteria; Automation; Control systems; Intelligent control; Missiles; Nonlinear control systems; Optimal control; Predictive control; Predictive models; Sampling methods; Uncertainty; Attitude control of missile; Fliess functional expansion; Model predictive control;

fLanguage

English

Publisher

ieee

Conference_Titel

Intelligent Control and Automation, 2008. WCICA 2008. 7th World Congress on

Conference_Location

Chongqing

Print_ISBN

978-1-4244-2113-8

Electronic_ISBN

978-1-4244-2114-5

Type

conf

DOI

10.1109/WCICA.2008.4593146

Filename

4593146