Formation Control for Tracking Non-cooperative Space Objects

被引：0
|
作者：
Bhat, Ishfaq Zahoor [1 ]
Ghose, Debasish [1 ,2 ]
机构：
[1] Indian Inst Sci Bangalore, Dept Aerosp Engn, Bangalore, Karnataka, India
[2] Indian Inst Sci Bangalore, RBCCPS, Bangalore, Karnataka, India
来源：
2024 IEEE SPACE, AEROSPACE AND DEFENCE CONFERENCE, SPACE 2024 | 2024年
关键词：
Formation; control; differential keplerian orbital elements; perturbation; SATELLITE RELATIVE MOTION;
D O I：
10.1109/SPACE63117.2024.10668092
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
In this paper, we present the dynamics and control of satellite formation where the chaser satellites fence a target satellite. Using velocity impulsive control the chasers are guided towards the desired relative positions for the general elliptical planar formation. Next, a control strategy for the chasers is proposed for tracking the target satellite, wherein they orient their sensors towards the target satellite. Numerical simulations are done to validate the efficacy of the methods and proposed controller.
引用
收藏
页码：359 / 362
页数：4
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