Computer-aided design system for control moment gyroscope; MATEC Web of Conferences; Vol. 158 : Space Engineering
| Parent link: | MATEC Web of Conferences Vol. 158 : Space Engineering.— 2018.— [01021, 5 p.] |
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| Summary: | Title screen 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. |
| Language: | English |
| Published: |
2018
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| Subjects: | |
| Online Access: | https://doi.org/10.1051/matecconf/201815801021 http://earchive.tpu.ru/handle/11683/52920 |
| Format: | Electronic Book Chapter |
| KOHA link: | https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=659428 |
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| 200 | 1 | |a Computer-aided design system for control moment gyroscope |f T. G. Kostyuchenko, N. Indygasheva | |
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| 300 | |a Title screen | ||
| 320 | |a [References: 10 tit.] | ||
| 330 | |a 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. | ||
| 461 | 1 | |0 (RuTPU)RU\TPU\network\4526 |t MATEC Web of Conferences | |
| 463 | 1 | |0 (RuTPU)RU\TPU\network\27949 |t Vol. 158 : Space Engineering |o VI International Forum for Young Scientists, April 26-28, 2018, Tomsk, Russia |o [proceedings] |f National Research Tomsk Polytechnic University (TPU) ; eds. V. N. Borikov [et al.] |v [01021, 5 p.] |d 2018 | |
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| 610 | 1 | |a управление | |
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