Co-ordinated attitude control of multi-satellite systems

被引：93

作者：

Kang, W ^{[1
]}

Yeh, HH

机构：

[1] USN, Postgrad Sch, Dept Math, Monterey, CA 93943 USA

[2] AFRL, VACA, Wright Patterson AFB, OH 45433 USA

来源：

INTERNATIONAL JOURNAL OF ROBUST AND NONLINEAR CONTROL | 2002年 / 12卷 / 2-3期

关键词：

Attitude stabilization - Attitude tracking - Coordinate attitude control - Multiple satellite systems - Perceptive frame;

D O I：

10.1002/rnc.682

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

An overview is given on three issues concerning the co-ordinated attitude control of multiple satellite systems: (i) optimal control for attitude stabilization and attitude tracking; (ii) coordination strategies of multiple satellites; (iii) co-ordinated controller design to implement coordination strategies. The nonlinear H∞ attitude controller is proposed to stabilize a satellite at a desired attitude. Simulations show that the co-ordinated controller is able to significantly reduce the error of relative attitude between satellites caused by slowly varying disturbances of the individual satellites.

引用

页码：185 / 205

页数：21