Computer-aided design system for control moment gyroscope

Computer-aided design system for control moment gyroscope

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 pro...

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Bibliographic Details
Main Authors: Kostyuchenko Tamara, Indygasheva Nelya
Format: Article
Language:English
Published: EDP Sciences 2018-01-01
Series:MATEC Web of Conferences
Online Access:https://doi.org/10.1051/matecconf/201815801021
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spelling doaj-b6896e12ebfa4aaba8f6203d14ba583e2021-02-02T00:13:57ZengEDP SciencesMATEC Web of Conferences2261-236X2018-01-011580102110.1051/matecconf/201815801021matecconf_se2018_01021Computer-aided design system for control moment gyroscopeKostyuchenko TamaraIndygasheva NelyaControl 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.https://doi.org/10.1051/matecconf/201815801021
collection DOAJ
language English
format Article
sources DOAJ
author Kostyuchenko Tamara
Indygasheva Nelya
spellingShingle Kostyuchenko Tamara
Indygasheva Nelya
Computer-aided design system for control moment gyroscope
MATEC Web of Conferences
author_facet Kostyuchenko Tamara
Indygasheva Nelya
author_sort Kostyuchenko Tamara
title Computer-aided design system for control moment gyroscope
title_short Computer-aided design system for control moment gyroscope
title_full Computer-aided design system for control moment gyroscope
title_fullStr Computer-aided design system for control moment gyroscope
title_full_unstemmed Computer-aided design system for control moment gyroscope
title_sort computer-aided design system for control moment gyroscope
publisher EDP Sciences
series MATEC Web of Conferences
issn 2261-236X
publishDate 2018-01-01
description 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.
url https://doi.org/10.1051/matecconf/201815801021
work_keys_str_mv AT kostyuchenkotamara computeraideddesignsystemforcontrolmomentgyroscope
AT indygashevanelya computeraideddesignsystemforcontrolmomentgyroscope
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