控制力矩陀螺发展与应用研究

Aerospace Contrd and Application ›› 2020, Vol. 46 ›› Issue (2): 1-7.

Development and Application of Control Moment Gyroscope

ZHAI Hua, LAI Lin, WU Dengyun, LI Gang, WEI Wenshan

1.Beijing Institute of Tracking and Telecommunications Technology, Beijing 100094, China; 2.Beijing Institute of Control Engineering，Beijing 100094, China; 3. Beijing Key Laboratory of Longlife Technology of Precise Rotation and Transmission Mechanisms, Beijing 100094, China.

Online:2020-04-25 Published:2020-05-21
Supported by:
National Nature Science Foundation of China(U1837602).

Abstract

CLC Number:

V448

ZHAI Hua, LAI Lin, WU Dengyun, LI Gang, WEI Wenshan. Development and Application of Control Moment Gyroscope[J].Aerospace Contrd and Application, 2020, 46(2): 1-7.

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[1]	YUAN Quan, HE Ying-Zi, XING Yan, XIONG Kai. Fault Diagnosis for Star Sensors Based on Linear Minimum Mean Square Filter[J]. , 2013, 39(2): 30 -35 .
[2]	. [J]. , 2018, 44(5): 0 .
[3]	NI Feng-Lei, LIN Peng-Fei, ZOU Tian. [J]. , 2018, 44(5): 7 -13 .
[4]	HU Xiao-Dong, HUANG Xue-Xiang, HU Tian-Jian, WANG Feng-Lin, LIANG Shu-Li. [J]. , 2018, 44(5): 14 -21 .
[5]	WANG Yun-Peng, JIE Yong-Chun. [J]. , 2018, 44(5): 22 -29 .
[6]	HUANG Jian-Bin, HUANG Long-Fei, HAN Xu, MENG Bo, LI Zhi, WANG Wen-Long, LI Wen. [J]. , 2018, 44(5): 30 -37 .
[7]	HAN Dong, HUANG Pan-Feng, LIU Xi-Yao. [J]. , 2018, 44(5): 38 -46 .
[8]	LIU Miao, LI Zhong-Kui. [J]. , 2018, 44(5): 47 -54 .
[9]	QIN Xin-Li, ZONG Qun, LI Xiao-Yu, ZHANG Bo-Yuan, ZHANG Xiu-Yun. [J]. , 2018, 44(5): 55 -59 .
[10]	GUO Xiao-Long, GUO Min-Hua, TAN Yuan, CAO Han-Yu, DIAN Song-Yi, LI Bin. [J]. , 2018, 44(5): 70 -75 .

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Development and Application of Control Moment Gyroscope

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