Explicit feedbacks stabilizing the attitude of a rigid spacecraft with two control torques

被引:95
|
作者
Coron, JM
Kerai, EY
机构
[1] Ecl. Normale Sup. de Cachan, Ctr. Mathematiques de Leurs Applic., URA 1611, 94235 Cachan Cedex
关键词
attitude control; stabilization;
D O I
10.1016/0005-1098(95)00194-8
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
We construct explicit time-varying feedbacks that locally asymptotically stabilize the attitude of a rigid spacecraft with two controls. Copyright (C) 1996 Elsevier Science Ltd.
引用
收藏
页码:669 / 677
页数:9
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