Velocity-free controllers for spacecraft attitude regulation: some further applications and results

被引:1
|
作者
Ailon, A [1 ]
Segev, R [1 ]
Grinberg, B [1 ]
Gil, M [1 ]
机构
[1] Ben Gurion Univ Negev, Dept Elect & Comp Engn, IL-84105 Beer Sheva, Israel
来源
PROCEEDINGS OF THE 2001 IEEE INTERNATIONAL CONFERENCE ON CONTROL APPLICATIONS (CCA'01) | 2001年
关键词
spacecraft; attitude regulation; velocity-free controllers; gas-jet actuators; momentum exchange actuators; time-delay;
D O I
10.1109/CCA.2001.973967
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
In this study we consider some further aspects of a velocity-free control scheme for regulating the attitude of a rigid spacecraft with gas jet and momentum exchange actuators. In particular, we consider some structural properties of the proposed controller that ensure asymptotic stability of the required attitude set-point. As shown, these properties are useful for studying stability when time-delay appears in the feedback loop.
引用
收藏
页码:799 / 804
页数:4
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