Satellite formation flying via Lyapunov stabilization

被引：0
|
作者：
Ahn, Hyo-Sung [1 ]
Won, Chang-Hee [2 ]
Park, Sang-Young [3 ]
机构：
[1] Gwangju Inst Sci & Technol, Dept Mechatron, 1 Oryong Dong, Kwangju 500712, South Korea
[2] Temple Univ, Dept Elect & Comp Engn, Philadelphia, PA 19122 USA
[3] Yonsei Univ, Dept Astron & Space Sci, Astrodynam & Control Lab, Seoul, South Korea
来源：
2007 INTERNATIONAL CONFERENCE ON CONTROL, AUTOMATION AND SYSTEMS, VOLS 1-6 | 2007年
关键词：
satellite; formation flying; Lyapunov analysis; asymptotical convergence;
D O I：
暂无
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 presents a control scheme for satellite formation flying based on Lyapunov stabilization. It is assumed that the angular rate and angular acceleration of true anomaly are not known, but they are bounded. In such a case, the control law proposed in this paper guarantees asymptotical convergence of the states to the desired values. Through numerical simulations, the validity of the proposed-formation flying scheme is illustrated.
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页码：2250 / 2253
页数：4
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