Attitude stabilization of an under-actuated rigid spacecraft via logic-based switching control

被引：0
|
作者：
He, Feng-Hua [1 ]
Ma, Ke-Mao [1 ]
Yao, Yu [1 ]
机构：
[1] Harbin Inst Technol, Control & Simulat Ctr, Harbin 150080, Peoples R China
来源：
PROCEEDINGS OF 2008 INTERNATIONAL CONFERENCE ON MACHINE LEARNING AND CYBERNETICS, VOLS 1-7 | 2008年
关键词：
attitude stabilization; under-actuated spacecraft; hybrid feedback control;
D O I：
10.1109/ICMLC.2008.4620719
中图分类号：
TP3 [计算技术、计算机技术];
学科分类号：
0812 ;
摘要：
The attitude stabilization control for an under-actuated spacecraft with two moving mass is considered in this paper. The kinematic and dynamic equations of the spacecraft are derived. A hybrid controller is proposed to yield global convergence to an arbitrarily small neighborhood of the origin. Simulation results show the superiority of the new type configuration scheme for moving mass moment control spacecraft.
引用
收藏
页码：1914 / 1919
页数：6
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