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清华大学 [4]
长春光学精密机械与物... [1]
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期刊论文 [4]
会议论文 [1]
发表日期
2010 [5]
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Practical algorithm simulation for vehicle side slip angle
期刊论文
2010, 2010
Yang Cai
;
Song Jian
;
Huang Quan-an
;
Li Hong-zhi
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浏览/下载:5/0
方向盘转角传感器研究进展
期刊论文
2010, 2010
杨财
;
周艳霞
;
YANG Cai
;
ZHOU Yan-xia
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  |  
浏览/下载:1/0
车身侧倾时前轮主销后倾角对转向稳定性的影响
期刊论文
2010, 2010
魏道高
;
王霄锋
;
金达锋
;
李克强
;
Wei Daogao
;
Wang Xiaofeng
;
Jin Dafeng
;
Li Keqiang
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  |  
浏览/下载:2/0
Mazda6轿车转向传感器信号的simulink识别
期刊论文
2010, 2010
张明
;
张鹏
;
何乐
;
夏群生
;
ZHANG Ming
;
ZHANG Peng
;
HE Le
;
XIA Qun-sheng
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浏览/下载:3/0
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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浏览/下载:16/0
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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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