A Method of Force Output Test for a Low Thrust High Precision Flat Space Electromagnetism Actuator
Authors
Chengchen Deng Chengchen Deng, Min Zhu Min Zhu, Hongbo Zhao, Liao He
Corresponding Author
Chengchen Deng Chengchen Deng
Available Online March 2016.
- DOI
- 10.2991/icmmse-16.2016.4How to use a DOI?
- Keywords
- Flat space electromagnetism actuator, Low thrust, High precision, Micro vibration suppress
- Abstract
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.
- Copyright
- © 2016, the Authors. Published by Atlantis Press.
- Open Access
- This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).
Cite this article
TY - CONF AU - Chengchen Deng Chengchen Deng AU - Min Zhu Min Zhu AU - Hongbo Zhao AU - Liao He PY - 2016/03 DA - 2016/03 TI - A Method of Force Output Test for a Low Thrust High Precision Flat Space Electromagnetism Actuator BT - Proceedings of the 2016 International Conference on Mechanics, Materials and Structural Engineering PB - Atlantis Press SP - 17 EP - 24 SN - 2352-5401 UR - https://doi.org/10.2991/icmmse-16.2016.4 DO - 10.2991/icmmse-16.2016.4 ID - ChengchenDeng2016/03 ER -