ROBUST ATTITUDE STABILIZATION OF SPACECRAFT USING NONLINEAR QUATERNION FEEDBACK

被引：173
|
作者：
JOSHI, SM [1 ]
KELKAR, AG [1 ]
WEN, JTY [1 ]
机构：
[1] RENSSELAER POLYTECH INST,DEPT ELECT COMP & SYST ENGN,TROY,NY 12180
来源：
IEEE TRANSACTIONS ON AUTOMATIC CONTROL | 1995年 / 40卷 / 10期
关键词：
D O I：
10.1109/9.467669
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
This paper considers the problem of three-axis attitude stabilization of a rigid spacecraft. A nonlinear control law which uses the feedback of the unit quaternion and the measured angular velocities is proposed and is shown to provide global asymptotic stability, The control law does not require the knowledge of the system parameters and is, therefore, robust to modeling errors. The significance of the control law is that it can be used for large-angle maneuvers with guaranteed stability.
引用
收藏
页码：1800 / 1803
页数：4
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