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Review:A Survey of Single Gimbal Control Moment Gyroscope for Agile Spacecraft Attitude Control

Yunhua Wu Feng Han Bing Hua Zhiming Chen Dafu Xu Linlin Ge

哈尔滨工业大学学报（英文版）2018，Vol.25Issue(6)：22-45,24.

哈尔滨工业大学学报（英文版）2018，Vol.25Issue(6)：22-45,24.DOI:10.11916/j.issn.1005-9113.16225

Review:A Survey of Single Gimbal Control Moment Gyroscope for Agile Spacecraft Attitude Control

Yunhua Wu ¹Feng Han ¹Bing Hua ¹Zhiming Chen ¹Dafu Xu ²Linlin Ge¹

作者信息

1. School of Astronautics, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
2. Aerospace System Engineering Shanghai, Shanghai 201108, China
折叠

摘要

关键词

agile spacecraft/SGCMG/CMG configuration/singularity and steering logic

Key words

agile spacecraft/SGCMG/CMG configuration/singularity and steering logic

分类

航空航天

引用本文复制引用

Yunhua Wu,Feng Han,Bing Hua,Zhiming Chen,Dafu Xu,Linlin Ge..Review:A Survey of Single Gimbal Control Moment Gyroscope for Agile Spacecraft Attitude Control[J].哈尔滨工业大学学报（英文版）,2018,25(6):22-45,24.

基金项目

Sponsored by the National Natural Science Foundation of China ( Grant No.61403197) , the Natural Science Foundation of Jiangsu Province ( Grant No. BK20140830) and the Program of Shanghai Subject Chief Scientist ( Grant No.14XD1423300) . （ Grant No.61403197）

哈尔滨工业大学学报（英文版）

ISSN：1005-9113

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