Finite-time Control for Formation Flying Spacecraft with Coupled Attitude and Translational Dynamics

被引：0
|
作者：
Guo, Yong [1 ]
Song, Shen-min [1 ]
机构：
[1] Harbin Inst Technol Univ, Harbin, Peoples R China
来源：
2013 10TH IEEE INTERNATIONAL CONFERENCE ON CONTROL AND AUTOMATION (ICCA) | 2013年
关键词：
TERMINAL SLIDING-MODE; COORDINATION CONTROL;
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 investigates a distributed coordination control scheme using terminal sliding mode for formation flying spacecraft with coupled attitude and translational dynamics. A six Degree-of-Freedom (6DOF) coupled model in Euler-Lagrange form is established. A continuous controller is proposed to alleviate the chattering phenomenon of a terminal sliding mode control. Theoretical analysis shows that the controller can guarantee the finite-time stability of the overall closed-loop system.
引用
收藏
页码：89 / 94
页数：6
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