Sliding mode control using modified Rodrigues parameters

被引：172
|
作者：
Crassidis, JL [1 ]
Markley, FL [1 ]
机构：
[1] NASA,GODDARD SPACE FLIGHT CTR,GUIDANCE NAV & CONTROL BRANCH,GREENBELT,MD 20771
来源：
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 1996年 / 19卷 / 06期
关键词：
D O I：
10.2514/3.21798
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
A control technique based on sliding mode (variable structure) control using the modified Rodrigues parameters is applied to attitude pointing. The technique makes rotations of up to 360 degrees possible and the parameters used form a minimal parameterization. Computer simulations show that the new algorithm can accurately control the attitude of a spacecraft for large angle maneuvers.
引用
收藏
页码：1381 / 1383
页数：3
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