H∞ and LMI attitude control design:: towards performances and robustness enhancement

被引：23

作者：

Charbonnel, C ^{[1
]}

机构：

[1] ALCATEL SPACE, F-06156 Cannes La Bocca, France

来源：

ACTA ASTRONAUTICA | 2004年 / 54卷 / 05期

关键词：

D O I：

10.1016/S0094-5765(03)00049-3

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

This paper presents a general approach for controller design for systems with large flexible appendages. Based on the H-infinity/LMI (Linear Matrix Inequality) framework, the proposed methodological guidelines allow to select an appropriate design strategy associated with its resolution technique. A powerful computer tool based on matlab allow to simplify the procedure. The results have been successfully applied during phase A studies of the Mars Sample Return project for the delicate Rendez-Vous mode, and allowed to design fully compliant control laws. (C) 2003 Elsevier Ltd. All rights reserved.

引用

页码：307 / 314

页数：8

共 10 条

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Boyd S, 1994, STUDIES APPL MATH, V15

[2] STATE-SPACE SOLUTIONS TO STANDARD H-2 AND H-INFINITY CONTROL-PROBLEMS [J].