Fliess Expansion-Based Bang-Bang Control Design and Its Application to Attitude Control of Missile

Author

Yao, Yu ; Yang, Baoqing ; He, Fenghua ; Cheng, Daizhan

Author_Institution

Harbin Inst. of Technol.

Volume

1

fYear

0

fDate

0-0 0

Firstpage

188

Lastpage

192

Abstract

Motivated by the attitude control of missile, we consider the tracking problem of nonlinear systems via finite value control. First, the Fliess expansion is used to describe the outputs. Using piecewise finite value control and the quadratic criteria, the optimal control is obtained. Then for certain model uncertainty, the model predictive control is considered. On line predicted uncertain parameters are used to update the system´s dynamics. The method developed is used to the control of missile. Simulation results show the effectiveness of the proposed method

Keywords

attitude control; bang-bang control; control system synthesis; missile control; nonlinear control systems; optimal control; piecewise linear techniques; predictive control; tracking; uncertain systems; Fliess expansion-based bang-bang control design; attitude control; missile control; model predictive control; model predictive tracking control; model uncertainty; nonlinear systems; optimal control; piecewise finite value control; Bang-bang control; Control systems; Missiles; Nonlinear control systems; Nonlinear systems; Optimal control; Predictive control; Predictive models; Sampling methods; Uncertainty; Fliess functional expansion; Nonlinear system; model predictive tracking control;

fLanguage

English

Publisher

ieee

Conference_Titel

Intelligent Control and Automation, 2006. WCICA 2006. The Sixth World Congress on

Conference_Location

Dalian

Print_ISBN

1-4244-0332-4

Type

conf

DOI

10.1109/WCICA.2006.1712298

Filename

1712298