Adaptive Pose Tracking Control for On-orbit Tumbling Target Spacecraft

被引：0
|
作者：
Chen, Ying [1 ]
Rong, Siyuan [1 ]
Li, Shunli [1 ]
He, Chen [1 ]
机构：
[1] Harbin Inst Technol, Sch Astronaut, Harbin, Peoples R China
来源：
2015 FIFTH INTERNATIONAL CONFERENCE ON INSTRUMENTATION AND MEASUREMENT, COMPUTER, COMMUNICATION AND CONTROL (IMCCC) | 2015年
关键词：
autonomous rendezvous; pose coupling; dual quaternion; mass property; adptive control;
D O I：
10.1109/IMCCC.2015.416
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
It is assumed in this paper that the service spacecraft perform autonomous rendezvous and proximity operation to a tumbling target in space. Under this background, this paper proposes a relative coupled position and attitude dynamics. Using a Lyapunov framework, an adaptive controller is designed with the mass property of the service spacecraft uncertain. Numerical simulation is finally provided to illustrate the performance of the proposed controller.
引用
收藏
页码：1972 / 1976
页数：5
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