空间控制技术与应用2017，Vol.43Issue(5)：43-48,6.DOI:10.3969/j.issn.1674-1579.2017.05.007
微小卫星用微型控制力矩陀螺研究
Miniature Control Moment Gyroscope for Small Satellites
摘要
Abstract
With the development of the aerospace technology,the demand for small satellites is increasing gradually.The agility of small satellites is a critical parameter,in the viewpoint of application field expansion and mission return maximization.The control moment gyroscope (CMG) exhibits better performances in terms of torque-power and mass-torque characteristics,which make it a key actuator for agile and precise attitude control.In this paper,a miniature CMG is developed for small satellites with O.1 N · m · s angular momentum.The performance and the environmental tests of the CMG are discussed,which demonstrate that the requirement of small satellites attitude control is perfectly met.关键词
控制力矩陀螺/微小卫星/姿态控制Key words
CMG/small satellites/attitude control分类
航空航天引用本文复制引用
来林,李刚,武登云,翟百臣,马文栋..微小卫星用微型控制力矩陀螺研究[J].空间控制技术与应用,2017,43(5):43-48,6.基金项目
国家自然科学基金青年科学基金资助项目(11402019). （11402019）
