Decentralized Fault Tolerant Control For Tethered Formation Spacecraft

被引：0
|
作者：
Zhang, Zejun [1 ]
Yang, Hao [1 ]
Jiang, Bin [1 ]
机构：
[1] Nanjing Univ Aeronaut & Astronaut, Coll Automat Engn, Nanjing 210016, Jiangsu, Peoples R China
来源：
2016 31ST YOUTH ACADEMIC ANNUAL CONFERENCE OF CHINESE ASSOCIATION OF AUTOMATION (YAC) | 2016年
基金：
中国国家自然科学基金;
关键词：
tethered spacecraft; attitude control; decentralized controllers; fault tolerant 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 the attitude control problem of a three-inline array tethered spacecraft in two-dimensional plane. The three-spacecraft array is decoupled into three individual dynamics. A feedback control law is proposed to stabilize the center spacecraft. For the single-tethered spacecrafts at the tips, a partially simplified nonlinear model is presented. Considering the coupling property between two angles of the single-tethered spacecraft, a decentralized controller is constructed. The issue of fault tolerant control is further discussed. Numerical simulation results validate the effectiveness of the proposed controllers.
引用
收藏
页码：207 / 212
页数：6
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