FAULT TOLERANT ATTITUDE CONTROL DURING FORMATION FLYING

被引：0
|
作者：
Li, Junquan [1 ]
Kumar, K. D. [2 ]
机构：
[1] Ryerson Univ, Dept Aerosp Engn, 350 Victoria St, Toronto, ON M58 2K3, Canada
[2] Ryerson Univ, Dept Aerosp Engn, Space Syst, Toronto, ON M58 2K3, Canada
来源：
SPACEFLIGHT MECHANICS 2010, PTS I-III | 2010年 / 136卷
关键词：
SLIDING MODE-CONTROL; SPACECRAFT; SYSTEMS;
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：
The authors propose an adaptive fuzzy terminal sliding mode control algorithm (AFTSMC) for attitude tracking of multiple picosatellites during formation flying. The relative attitude of the leader and follower picosatellites under gravity gradient torque and external periodic disturbances is controlled by four reaction wheels. This method can accommodate faults rapidly without controller reconfiguration. The numerical simulations (under the fault and failure of wheel) demonstrate the effectiveness of the proposed controllers.
引用
收藏
页码：1933 / +
页数：4
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