Please use this identifier to cite or link to this item: http://earchive.tpu.ru/handle/11683/52920
Title: Computer-aided design system for control moment gyroscope
Authors: Kostyuchenko, Tamara Georgievna
Indygasheva, Nelya
Keywords: автоматизированное проектирование; гироскопы; ориентация; космические аппараты; управление
Issue Date: 2018
Publisher: EDP Sciences
Citation: 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.].
Abstract: 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.
URI: http://earchive.tpu.ru/handle/11683/52920
Appears in Collections:Материалы конференций

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