Proceedings of the 2016 International Conference on Mechanics, Materials and Structural Engineering

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/).

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Volume Title
Proceedings of the 2016 International Conference on Mechanics, Materials and Structural Engineering
Series
Advances in Engineering Research
Publication Date
March 2016
ISBN
978-94-6252-187-2
ISSN
2352-5401
DOI
10.2991/icmmse-16.2016.4How to use a DOI?
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  -