A Method of Force Output Test for a Low Thrust High Precision Flat Space Electromagnetism Actuator

被引:0
|
作者
Deng, Chengchen [1 ]
Tang, Zhongxing [1 ]
Zhu, Min [1 ]
Zhao, Hongbo [1 ]
Liao, He [1 ]
机构
[1] Shanghai Inst Satellite Engn, Shanghai 200240, Peoples R China
来源
Proceedings of the 2016 International Conference on Mechanics, Materials and Structural Engineering (ICMMSE) | 2016年 / 29卷
关键词
Flat space electromagnetism actuator; Low thrust; High precision; Micro vibration suppress;
D O I
暂无
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Future satellites require higher and higher payload's pointing precision and attitude stability, it is urgent to suppress micro vibration efficiently. This article designs a low thrust, high precision flat electromagnetism actuator. Firstly, the article designs the configuration of the actuator. Secondly, based on the working principle this article analysis data stimulation result of output force using the software-Ansoft Maxwell. Thirdly, aiming at testing the extremely low force output of an actuator, this article designs a new method based on single axe airing bear and high precision gyro. The simulation and examination show validity of the micro vibration suppression through the configuration and the force testing method.
引用
收藏
页码:12 / 19
页数:8
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