Global magnetic attitude control of spacecraft

被引：9
|
作者：
Lovera, M [1 ]
Astolfi, A [1 ]
机构：
[1] Politecn Milan, Dipartimento Elettron & Informaz, I-20133 Milan, Italy
来源：
2004 43RD IEEE CONFERENCE ON DECISION AND CONTROL (CDC), VOLS 1-5 | 2004年
关键词：
D O I：
10.1109/CDC.2004.1428641
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 and of dynamic attitude feedback. Simulation results demonstrate the practical applicability of the proposed approach.
引用
收藏
页码：267 / 272
页数：6
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