| Issue |
MATEC Web Conf.
Volume 158, 2018
VI International Forum for Young Scientists “Space Engineering 2018”
|
|
|---|---|---|
| Article Number | 01021 | |
| Number of page(s) | 5 | |
| DOI | https://doi.org/10.1051/matecconf/201815801021 | |
| Published online | 19 March 2018 | |
Computer-aided design system for control moment gyroscope
Tomsk Polytechnic University, 634050 Tomsk, Russia
* Corresponding author: ktg@tpu.ru
Control moment gyroscope or two-axis balking gyroscope is used in spacecraft orientation systems. The control moment gyroscope is a complex electromechanical system with different parameters which connect by means of specific instant and inverse dependences. This fact could complicate the design process as of getting the optimal parameters the search of construction variations becomes harder. To simplify the control moment gyroscope designing process and increase its efficiency the computer-aided design system could be as highly useful. The computer-aided design system which is used in the present research and described in the article consists of five main subsystems. They cover the main stages of control moment gyroscope designing.
© The Authors, published by EDP Sciences, 2018
This is an Open Access article distributed under the terms of the Creative Commons Attribution License 4.0, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited. (http://creativecommons.org/licenses/by/4.0/).
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