Nonlinear tracking control of an underactuated spacecraft

被引：30
|
作者：
Behal, A [1 ]
Dawson, D
Zergeroglu, E
Fang, Y
机构：
[1] Clemson Univ, Dept Bioengn, Clemson, SC 29634 USA
[2] Clemson Univ, Dept Elect & Comp Engn, Clemson, SC 29634 USA
[3] OFS Fitel, Dept Controls & Software Engn, Sturbridge, MA 01566 USA
[4] Clemson Univ, Dept Elect & Comp Engn, Clemson, SC 29634 USA
来源：
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2002年 / 25卷 / 05期
关键词：
D O I：
10.2514/2.4973
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
A nonlinear controller for the attitude tracking problem for a rigid underactuated spacecraft is presented. For the reduced-order problem, the spacecraft dynamics are neglected. Simulation results for the controller demonstrated the efficacy of the proposed strategy in achieving tracking for the underactuated spacecraft.
引用
收藏
页码：979 / 985
页数：7
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