Leader/Follower synchronization of satellite attitude without angular velocity measurements

被引:0
作者
Bondhus, Anne Karin [1 ]
Pettersen, Kristin Y. [1 ]
Gravdahl, J. Tommy [1 ]
机构
[1] Norwegian Univ Sci & Technol, Dept Engn Cybernet, N-7491 Trondheim, Norway
来源
2005 44TH IEEE CONFERENCE ON DECISION AND CONTROL & EUROPEAN CONTROL CONFERENCE, VOLS 1-8 | 2005年
关键词
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
In this paper we propose a Leader/Follower output feedback synchronization scheme for control of the attitude of two satellites when angular velocity measurements are not available. Nonlinear observers are used to estimate the angular velocities. The attitudes of the satellites are represented by unit quaternions, and the control design is based on vectorial observer backstepping. The analysis of the method shows that the rotation matrices representing the attitude errors between the follower and the leader, and between the leader and its reference attitude, converge to the identity matrix for any initial conditions. The control scheme is simulated to validate the results.
引用
收藏
页码:7270 / 7277
页数:8
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