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Computer-aided design system for control moment gyroscope

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Поле Значение
 
Заглавие Computer-aided design system for control moment gyroscope
 
Автор Kostyuchenko, Tamara Georgievna
Indygasheva, Nelya
 
Тематика автоматизированное проектирование
гироскопы
ориентация
космические аппараты
управление
 
Описание 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.
 
Дата 2019-02-28T03:46:55Z
2019-02-28T03:46:55Z
2018
 
Тип Conference Paper
Published version (info:eu-repo/semantics/publishedVersion)
Conference paper (info:eu-repo/semantics/conferencePaper)
 
Идентификатор Kostyuchenko T. G. Computer-aided design system for control moment gyroscope / T. G. Kostyuchenko, N. Indygasheva // MATEC Web of Conferences. — Les Ulis : EDP Sciences, 2018. — Vol. 158 : Space Engineering : VI International Forum for Young Scientists, April 26-28, 2018, Tomsk, Russia : [proceedings]. — [01021, 5 p.].
http://earchive.tpu.ru/handle/11683/52920
10.1051/matecconf/201815801021
 
Язык en
 
Связанные ресурсы MATEC Web of Conferences. Vol. 158 : Space Engineering. — Les Ulis, 2018.
 
Права Open access (info:eu-repo/semantics/openAccess)
 
Издатель EDP Sciences