Configuration Analysis and Singularity Visualization of Single Gimbal Control Moment Gyroscopes

doi:10.3780/j.issn.1000-758X.2013.01.004

Chinese Space Science and Technology ›› 2013, Vol. 33 ›› Issue (1): 21-29.doi: 10.3780/j.issn.1000-758X.2013.01.004

Previous Articles Next Articles

Configuration Analysis and Singularity Visualization of Single Gimbal Control Moment Gyroscopes

Wei Kongming,Wu Zhong,Liu Tao

(School of Instrumentation Science and Opto-electronics Engineering, Beijing 100191)

Received:2012-03-01 Revised:2012-04-07 Published:2013-02-25 Online:2013-02-25

Abstract

Abstract: The configuration efficiency and controllable efficiency are important indices in evaluating the configuration of a single gimbal control moment gyroscope (SGCMG) system. But the configuration efficiency is non-normalized, and the controllable efficiency depends on the magnitude of the angular momentum envelop. By normalizing the configuration efficiency and excluding the impact of the angular momentum envelop to the controllable efficiency, two improved indices, which are capacity ratio and nonsingular capacity ratio, were introduced. As the singularity of SGCMGs is complex and these scalar indices do not indicate the whole properties of the configuration, visualization techniques were used to compare the singular surfaces of different configurations. The analysis results show that the quality of the SGCMG and the symmetries of the configurations mainly affect the configuration indices and the complexity of the singular surface.

Key words: Control moment gyroscope, Configuration analysis, Attitude control, Spacecraft

WEI Kong-Ming, WU Zhong, LIU Tao. Configuration Analysis and Singularity Visualization of Single Gimbal Control Moment Gyroscopes[J]. Chinese Space Science and Technology, 2013, 33(1): 21-29.

Add to citation manager EndNote|Reference Manager|ProCite|BibTeX|RefWorks

URL: https://journal26.magtechjournal.com/kjkxjs/EN/10.3780/j.issn.1000-758X.2013.01.004

https://journal26.magtechjournal.com/kjkxjs/EN/Y2013/V33/I1/21

[1]	ZHANG Honghua, GUAN Yifeng, LI Ji, YU Jie, CHEN Yao, WANG Zhiwen, ZHANG Xiaowen, ZHANG Luchen, LI Linfeng, SUN Guojian, WANG Zhenhua, GUO Minwen, LI Xiaofeng, GAO Xizhen. A dual-loop fault tolerant attitude control for the Chang′e-6 lunar orbit flight [J]. Chinese Space Science and Technology, 2024, 44(5): 15-22.
[2]	MENG Henghui, XU Yawei, HAN Dongyang, LIU Xin, GENG Liyin, ZHANG Qingjun, LIU Liping, ZHANG Hongxing, WANG Yuying. Design and verification of loop heat pipe coupling heat system based on brazing technology [J]. Chinese Space Science and Technology, 2024, 44(5): 57-65.
[3]	ZHENG Xinyu, ZHANG Yi, ZHOU Jie, TANG Peijia, PENG Shengren, DANG Zhaohui. Improvement and application of MCTS in turn-based orbital games [J]. Chinese Space Science and Technology, 2024, 44(5): 75-82.
[4]	LI Ruifeng, SUN Chong, WANG Zheng, FANG Qun, ZHANG Xiang. Capture configuration design for space non-cooperative target based on reachable domain [J]. Chinese Space Science and Technology, 2024, 44(5): 83-94.
[5]	TAO Xinyong, KANG Guohua, WU Junfeng, HU Miaomiao, YANG Zhenghao, ZHOU Shaohui. Design of flexible docking mechanism for micro-nano satellites [J]. Chinese Space Science and Technology, 2024, 44(4): 119-129.
[6]	LEI Yongjun, LU Dongning, YUAN li, CHEN chao. An attitude control method of satellites with hybrid flywheel configuration for skew maneuvers [J]. Chinese Space Science and Technology, 2024, 44(3): 111-119.
[7]	JIANG Yipeng, CUI Yufu, LIU Zhijia, QING Jiang. Optimization of drag reduction configuration on windward side of very low orbit spacecraft [J]. Chinese Space Science and Technology, 2024, 44(3): 120-126.
[8]	ZHOU Siyu, GU Yingying, YANG Yuetang, SHI Liheng, MA Yuxuan, ZHU Feihu, ZHANG Yunfang, WU Guanhao. Space application and test design of dual-comb ranging technique [J]. Chinese Space Science and Technology, 2024, 44(3): 127-135.
[9]	GAO Xin, NIAN Jiawei, LIU Hongjin, YANG Mengfei. Efficient cache replacement framework based on access hotness for spacecraft processors [J]. Chinese Space Science and Technology, 2024, 44(2): 74-88.
[10]	HUANG Yuan, WEI Chunling, YAN Han, HAO Renjian. Ability modeling for spacecraft control system based on partial least square structural equation model approach [J]. Chinese Space Science and Technology, 2024, 44(2): 98-108.
[11]	NIU Zitian, FU Zhendong, MIAO Jianyin, YANG Qi, WU Qi, YANG Le. Research progress of transcritical carbon dioxide heat pumps in space applications [J]. Chinese Space Science and Technology, 2024, 44(1): 23-33.
[12]	PENG Qibo, WU Xinfeng, WANG Beichao, LI Shuang. Research progress and prospect of spacecraft reconfiguration technology [J]. Chinese Space Science and Technology, 2023, 43(2): 16-31.
[13]	LIANG Wei, LI Jun, LI Jingling, CUI Tao, WEI Jiayuan, ZHANG Yi. Link-state-based adaptive interference cancellation for cabin in spacecraft [J]. Chinese Space Science and Technology, 2023, 43(2): 128-134.
[14]	DONG Yicheng, WANG Weizong, ZHANG Jinrui, QI Yue, YAN Jiaqi. Study on braking mechanism of planetary probe based on plasma magnetic shell [J]. Chinese Space Science and Technology, 2022, 42(6): 35-45.
[15]	WEI Jianyu, KANG Guohua, WU Junfeng, ZHAO Teng, QIU Yuhuan, XU Chuanxiao. Research on relative position and attitude measurement of visible light/laser combination [J]. Chinese Space Science and Technology, 2022, 42(6): 71-78.

Configuration Analysis and Singularity Visualization of Single Gimbal Control Moment Gyroscopes

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Recommended Articles

Metrics

Comments