Spacecraft attitude control using magnetic actuators

被引：179
作者：
Lovera, M
Astolfi, A
机构：
[1] Politecn Milan, Dipartimento Elettr & Informat, I-20133 Milan, Italy
[2] Univ London Imperial Coll Sci Technol & Med, Dept Elect & Elect Engn, London SW7 2BT, England
来源：
AUTOMATICA | 2004年 / 40卷 / 08期
关键词：
attitude control; spacecraft magnetic control; nonlinear control; averaging theory;
D O I：
10.1016/j.automatica.2004.02.022
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
The problem of inertial pointing for a spacecraft with magnetic actuators is addressed and an almost global solution to the problem is obtained by means of static attitude and rate feedback. A local solution based on dynamic attitude feedback is also presented. Simulation results demonstrate the practical applicability of the proposed approach. (C) 2004 Published by Elsevier Ltd.
引用
收藏
页码：1405 / 1414
页数：10
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