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

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

机构地区：[1]School of Astronautics, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China [2]Aerospace System Engineering Shanghai, Shanghai 201108, China

出　　处：《Journal of Harbin Institute of Technology(New Series)》2018年第6期22-45,共24页哈尔滨工业大学学报（英文版）

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

摘　　要：Agile attitude maneuver is a basic requirement for next generation imaging spacecraft and Control Moment Gyroscope (CMG) is an effective candidate for large space station and agile spacecraft attitude control because of its torque amplification capability. This paper provides a thorough survey of Single Gimbal Control Moment Gyroscope (SGCMG) in terms of configuration,evaluation,modeling,singularity analysis and steering logic,etc. For specific space missions,CMGs are logically mounted into different particular arrays which can be chosen by the proposed evaluation methods. From the dynamic model we find a tough inverse mapping problem which suffers the inherent geometric singularity. Different techniques and theories then are applied for singularity analysis and CMG steering logics design. The pyramid CMG cluster and singular robust logics are proven to be able to enhance the agility of spacecraft. Above work forms a systematic framework of SGCMG for agile spacecraft control with lots of illustrative examples,tables and figures,and will evoke further investigation for future missions.Agile attitude maneuver is a basic requirement for next generation imaging spacecraft and Control Moment Gyroscope （ CMG） is an effective candidate for large space station and agile spacecraft attitude control because of its torque amplification capability. This paper provides a thorough survey of Single Gimbal Control Moment Gyroscope （SGCMG） in terms of configuration, evaluation, modeling, singularity analysis and steering logic, etc. For specific space missions, CMGs are logically mounted into different particul ararrays which can be chosen by the proposed evaluation methods. From the dynamic model we find a toughinverse mapping problem which suffers the inherent geometric singularity. Different techniques and theoriesthen are applied for singularity analysis and CMG steering logics design. The pyramid CMG cluster andsingular robust logics are proven to be able to enhance the agility of spacecraft. Above work forms asystematic frame work of SGCMG for agile spacecraft control with lots of illustrative examples, tables andfigures, and will evoke further investigation for future missions.

关 键 词：AGILE SPACECRAFT SGCMG CMG configuration SINGULARITY and STEERING logic 

分 类 号：V448.22[航空宇航科学与技术—飞行器设计]