LPV design for a space vehicle attitude control benchmark problem

Author

Gao, Rui ; Ohtsubo, Kazuhisa ; Kajiwara, Hiroyuki

Author_Institution

Kyushu Univ., Fukuoka-Shi, Japan

Volume

2

fYear

2003

fDate

4-6 Aug. 2003

Firstpage

1461

Abstract

This paper is concerned with the design of quaternion-based, attitude tracking controller for a rigid spacecraft under a large angle maneuver. A new design technique is proposed, which is based on the decomposition of kinematics control and dynamics control, using linear parameter-varying (LPV) synthesis framework. The proposed LPV controllers ensure asymptotic attitude tracking. In addition, this two-step LPV design greatly reduce the computation effort than that of standard LPV synthesis. Non-linear simulation demonstrates the effectiveness of the proposed method.

Keywords

asymptotic stability; attitude control; control system synthesis; kinematics; linear systems; nonlinear control systems; space vehicles; tracking; vehicle dynamics; asymptotic attitude tracking; asymptotic attitude tracking controller; benchmark problem; control system synthesis; dynamics control decomposition; kinematics control decomposition; linear parameter varying controller design; linear parameter varying synthesis; nonlinear simulation; quaternion based controller design; rigid spacecraft; space vehicle attitude control;

fLanguage

English

Publisher

ieee

Conference_Titel

SICE 2003 Annual Conference

Conference_Location

Fukui, Japan

Print_ISBN

0-7803-8352-4

Type

conf

Filename

1324186