Robust reliable control for autonomous spacecraft rendezvous with limited-thrust

被引：27

作者：

Yang, Xuebo ^{[1
]}

Gao, Huijun ^{[1
]}

机构：

[1] Harbin Inst Technol, Res Inst Intelligent Control & Syst, Harbin 150080, Peoples R China

来源：

AEROSPACE SCIENCE AND TECHNOLOGY | 2013年 / 24卷 / 01期

基金：

中国国家自然科学基金;

关键词：

Limited-thrust; Reliable control; Spacecraft rendezvous; DISCRETE-TIME-SYSTEMS; H-INFINITY-CONTROL; FEEDBACK CONTROL; ORBITAL TRANSFER; STABILIZATION; GUIDANCE; DESIGN;

D O I：

10.1016/j.ast.2011.11.003

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

This paper investigates the problem of robust reliable control for the spacecraft rendezvous with limited-thrust. Based on the Clohessy-Wiltshire (C-W) equations and by considering the uncertainties and the possible failures, the dynamic model for spacecraft rendezvous is proposed, and the orbital transfer control problem is transformed into a stabilization problem. Then, by a Lyapunov approach, the existence conditions for admissible controllers are formulated in the form of linear matrix inequalities (LMIs), and the controller design is cast into a convex feasibility problem subject to LMI constraints. With the obtained controllers, the rendezvous can be accomplished with the limited-thrust in spite of the possible thruster failures. The effectiveness of the proposed approach is illustrated by simulation examples. (C) 2011 Elsevier Masson SAS. All rights reserved.

引用

页码：161 / 168

页数：8

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