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北京航空航天大学 [1]
长春光学精密机械与物... [1]
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会议论文 [1]
期刊论文 [1]
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2018 [1]
2010 [1]
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Fault-Tolerant Decoupling Control for Spacecraft with SGCMGs Based on an Active-Disturbance Rejection-Control Technique
期刊论文
JOURNAL OF AEROSPACE ENGINEERING, 2018, 卷号: 31
作者:
Zhang, Fuzhen
;
Jin, Lei
;
Xu, Shijie
;
Zhao, Yushan
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浏览/下载:2/0
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提交时间:2019/12/30
Spacecraft attitude control
Single-gimbal control moment gyroscopes (SGCMGs)
Fault-tolerant control
Active-disturbance rejection control
Extended-state observer (ESO)
United steering of control moment gyros for small satellite with limited gimbal rate (EI CONFERENCE)
会议论文
2010 IEEE International Conference on Information and Automation, ICIA 2010, June 20, 2010 - June 23, 2010, Harbin, Heilongjiang, China
Xu K.
;
Jin G.
;
Chen C.
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提交时间:2013/03/25
Single Gimbal Control Moment Gyroscopes (SGCMG) can could provide large control torque and quick attitude maneuver rate to small satellites without any increase in power
volume and mass
which will help small satellites become more powerful. Singularity avoidance and failure steering are two important problems to SGCMGs and also the main focus in this field. A new united steering law for SGCMGs with capabilities of singularity avoidance and quick transition of singularity surfaces is developed in this paper. To ensuring the existence of null motion
the commanded output of controller was changed real-timely as the variation of singularity measurement of SGCMGs
which can avoid the gimbal angle rate saturation. This developed steering law could help the SGCMGs provide real-time control toques in spite of limitation of gimbal angle rate. Simulation analysis is conducted for a certain 4-SGCMG system mounted on a small satellite. Simulation results indicate that the steering law is very effective in singularity avoidance. 2010 IEEE.
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