Relative Attitude Tracking Control Of Multiple Spacecraft With Unknown Inertia Using Line-of-Sight Measurements

被引：0
|
作者：
Warier, Rakesh R. [1 ]
Sukumar, Srikant [1 ]
机构：
[1] Indian Inst Technol, Dept Syst & Control Engn, Bombay 400076, Maharashtra, India
来源：
2017 INDIAN CONTROL CONFERENCE (ICC) | 2017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：
This paper considers adaptive relative attitude tracking control of two spacecraft formulated in SO(3) using line-of-sight measurements. The objective is to control the attitudes of individual spacecraft with unknown moment of inertia so as to track a specified time-varying relative attitude trajectory. We propose an estimation scheme for the moment of inertia. Proposed control torques and estimation schemes are obtained in terms of line-of-sight measurements. The trajectories of the resulting closed loop system are shown to be asymptotically tracking the desired time-varying trajectories.
引用
收藏
页码：105 / 110
页数：6
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