Ensuring Survivability of Spacecraft Attitude Control System at Failures in Flywheel Cluster

A method for ensuring the survivability of a spacecraft attitude control system with minimally redundant cluster of the flywheels and magnetic actuator at the faults of any reaction wheels are presented. The results of computer simulation were obtained and it was found if any two of the four fly...

Full description

Bibliographic Details
Main Authors:	Sergey Somov, Tatyana Somova
Format:	Article
Language:	English
Published:	Hezarfen Aeronautics and Space Technologies Institue 2021-01-01
Series:	Havacılık ve Uzay Teknolojileri Dergisi
Subjects:	satellite earth observation control system survivability
Online Access:	http://jast.hho.edu.tr/index.php/JAST/article/view/434

id	doaj-cc7fd16010bc40a6bf8fa163e5681c24
record_format	Article
spelling	doaj-cc7fd16010bc40a6bf8fa163e5681c242021-02-04T12:05:44ZengHezarfen Aeronautics and Space Technologies InstitueHavacılık ve Uzay Teknolojileri Dergisi1304-04482021-01-011418998Ensuring Survivability of Spacecraft Attitude Control System at Failures in Flywheel ClusterSergey Somov0https://orcid.org/0000-0002-2844-7627Tatyana Somova1https://orcid.org/0000-0002-1862-7210Samara State Technical UniversitySamara State Technical UniversityA method for ensuring the survivability of a spacecraft attitude control system with minimally redundant cluster of the flywheels and magnetic actuator at the faults of any reaction wheels are presented. The results of computer simulation were obtained and it was found if any two of the four flywheels according to the General Electric scheme fail, digital control of the flywheel cluster and magnetic drive allows the land-survey satellite to maintain the ability for observation of given terrestrial targets.http://jast.hho.edu.tr/index.php/JAST/article/view/434satelliteearth observationcontrol systemsurvivability
collection	DOAJ
language	English
format	Article
sources	DOAJ
author	Sergey Somov Tatyana Somova
spellingShingle	Sergey Somov Tatyana Somova Ensuring Survivability of Spacecraft Attitude Control System at Failures in Flywheel Cluster Havacılık ve Uzay Teknolojileri Dergisi satellite earth observation control system survivability
author_facet	Sergey Somov Tatyana Somova
author_sort	Sergey Somov
title	Ensuring Survivability of Spacecraft Attitude Control System at Failures in Flywheel Cluster
title_short	Ensuring Survivability of Spacecraft Attitude Control System at Failures in Flywheel Cluster
title_full	Ensuring Survivability of Spacecraft Attitude Control System at Failures in Flywheel Cluster
title_fullStr	Ensuring Survivability of Spacecraft Attitude Control System at Failures in Flywheel Cluster
title_full_unstemmed	Ensuring Survivability of Spacecraft Attitude Control System at Failures in Flywheel Cluster
title_sort	ensuring survivability of spacecraft attitude control system at failures in flywheel cluster
publisher	Hezarfen Aeronautics and Space Technologies Institue
series	Havacılık ve Uzay Teknolojileri Dergisi
issn	1304-0448
publishDate	2021-01-01
description	A method for ensuring the survivability of a spacecraft attitude control system with minimally redundant cluster of the flywheels and magnetic actuator at the faults of any reaction wheels are presented. The results of computer simulation were obtained and it was found if any two of the four flywheels according to the General Electric scheme fail, digital control of the flywheel cluster and magnetic drive allows the land-survey satellite to maintain the ability for observation of given terrestrial targets.
topic	satellite earth observation control system survivability
url	http://jast.hho.edu.tr/index.php/JAST/article/view/434
work_keys_str_mv	AT sergeysomov ensuringsurvivabilityofspacecraftattitudecontrolsystematfailuresinflywheelcluster AT tatyanasomova ensuringsurvivabilityofspacecraftattitudecontrolsystematfailuresinflywheelcluster
_version_	1724285295435710464

Ensuring Survivability of Spacecraft Attitude Control System at Failures in Flywheel Cluster

Similar Items