Fault Tolerant Sliding Mode Control for a Nanosatellite

被引:0
|
作者
Shin, Miri [2 ]
Kang, Chul Woo [2 ]
Lim, Junkyu [2 ]
Park, Chan Gook [1 ]
机构
[1] Seoul Natl Univ, Sch Mech & Aerosp Engn, Automat & Syst Res Inst, Seoul 151742, South Korea
[2] Seoul Natl Univ, Sch Mech & Aerosp Engn, Seoul 151742, South Korea
关键词
Sliding Mode Control; Nanosatellite; Fault tolerant attitude control; SNUSAT-1;
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 describes a nanosatellite attitude control being able to perform fault tolerant control to increase a reliability of a nanosatellite. A fault-tolerant sliding mode controller is used for a nanosatellite using four reaction wheels as a set of actuators. The fault-tolerant sliding mode controller is designed to perform the rest-to-rest maneuver of a satellite system. The actuator fault reflects the degradation of the actuation effectiveness. The Lyapunov theorem is used to analyze the system stability. In computer simulations, we use SNUSAT-1 made in Seoul National University as an applied nanosatellite. The control scheme of a nanosatellite is verified under the actuator fault situation that one reaction wheel of four reaction wheels is fault as well as the normal situation that four reaction wheels are healthy.
引用
收藏
页码:44 / 48
页数:5
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