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
来源：
AUTOMATICA | 1996年 / 32卷 / 05期
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
相关论文
共 40 条
[1]   COMMENTS ON THE STABILIZABILITY OF THE ANGULAR VELOCITY OF A RIGID BODY [J].
AEYELS, D ;
SZAFRANSKI, M .
SYSTEMS & CONTROL LETTERS, 1988, 10 (01) :35-39
[2]   STABILIZATION BY SMOOTH FEEDBACK OF THE ANGULAR VELOCITY OF A RIGID BODY [J].
AEYELS, D .
SYSTEMS & CONTROL LETTERS, 1985, 6 (01) :59-63
[3]  
[Anonymous], 1967, DIFFERENTIAL EQUATIO
[4]  
[Anonymous], 1994, J MATH SYSTEMS ESTIM
[5]   STABILIZATION WITH RELAXED CONTROLS [J].
ARTSTEIN, Z .
NONLINEAR ANALYSIS-THEORY METHODS & APPLICATIONS, 1983, 7 (11) :1163-1173
[6]  
BONNARD B, 1982, RAIRO-AUTOM-SYST ANA, V16, P85
[7]  
BROCKETT RW, DIFFERENTIAL GEOMETR, P181
[8]   ON THE ATTITUDE STABILIZATION OF RIGID SPACECRAFT [J].
BYRNES, CI ;
ISIDORI, A .
AUTOMATICA, 1991, 27 (01) :87-95
[9]   NEW RESULTS AND EXAMPLES IN NONLINEAR FEEDBACK STABILIZATION [J].
BYRNES, CI ;
ISIDORI, A .
SYSTEMS & CONTROL LETTERS, 1989, 12 (05) :437-442
[10]  
BYRNES CI, 1988, LECTURE NOTES CONTRO, V105, P48
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