On One Method for Constructing a Programmed Trajectory in Problems of Stabilizing a Spacecraft

A method is proposed for constructing a programmed trajectory in the problems of stabilizing a spacecraft in a fixed time. The method allows constructing a programmed motion, because of which the spacecraft is stabilized in rotational motion around the axis of dynamic symmetry, and this axis is orie...

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Auteurs principaux:	Lamotkin Alexey, Misura Natalia, Mityushov Evgenij
Format:	article
Langue:	EN FR
Publié:	EDP Sciences 2021
Sujets:	Engineering (General). Civil engineering (General) TA1-2040
Accès en ligne:	https://doaj.org/article/be55b729dc9c4ff3ab9c928e0f252bc5
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spelling	oai:doaj.org-article:be55b729dc9c4ff3ab9c928e0f252bc52021-11-08T15:20:33ZOn One Method for Constructing a Programmed Trajectory in Problems of Stabilizing a Spacecraft2261-236X10.1051/matecconf/202134603055https://doaj.org/article/be55b729dc9c4ff3ab9c928e0f252bc52021-01-01T00:00:00Zhttps://www.matec-conferences.org/articles/matecconf/pdf/2021/15/matecconf_icmtmte2021_03055.pdfhttps://doaj.org/toc/2261-236XA method is proposed for constructing a programmed trajectory in the problems of stabilizing a spacecraft in a fixed time. The method allows constructing a programmed motion, because of which the spacecraft is stabilized in rotational motion around the axis of dynamic symmetry, and this axis is oriented along the local vertical. The proposed algorithm is based on the possibility of representing the unit sphere of quaternions in four-dimensional space as a ball with a radius in three-dimensional space. This makes it possible to obtain a visual representation of the spacecraft rotation trajectory.Lamotkin AlexeyMisura NataliaMityushov EvgenijEDP SciencesarticleEngineering (General). Civil engineering (General)TA1-2040ENFRMATEC Web of Conferences, Vol 346, p 03055 (2021)
institution	DOAJ
collection	DOAJ
language	EN FR
topic	Engineering (General). Civil engineering (General) TA1-2040
spellingShingle	Engineering (General). Civil engineering (General) TA1-2040 Lamotkin Alexey Misura Natalia Mityushov Evgenij On One Method for Constructing a Programmed Trajectory in Problems of Stabilizing a Spacecraft
description	A method is proposed for constructing a programmed trajectory in the problems of stabilizing a spacecraft in a fixed time. The method allows constructing a programmed motion, because of which the spacecraft is stabilized in rotational motion around the axis of dynamic symmetry, and this axis is oriented along the local vertical. The proposed algorithm is based on the possibility of representing the unit sphere of quaternions in four-dimensional space as a ball with a radius in three-dimensional space. This makes it possible to obtain a visual representation of the spacecraft rotation trajectory.
format	article
author	Lamotkin Alexey Misura Natalia Mityushov Evgenij
author_facet	Lamotkin Alexey Misura Natalia Mityushov Evgenij
author_sort	Lamotkin Alexey
title	On One Method for Constructing a Programmed Trajectory in Problems of Stabilizing a Spacecraft
title_short	On One Method for Constructing a Programmed Trajectory in Problems of Stabilizing a Spacecraft
title_full	On One Method for Constructing a Programmed Trajectory in Problems of Stabilizing a Spacecraft
title_fullStr	On One Method for Constructing a Programmed Trajectory in Problems of Stabilizing a Spacecraft
title_full_unstemmed	On One Method for Constructing a Programmed Trajectory in Problems of Stabilizing a Spacecraft
title_sort	on one method for constructing a programmed trajectory in problems of stabilizing a spacecraft
publisher	EDP Sciences
publishDate	2021
url	https://doaj.org/article/be55b729dc9c4ff3ab9c928e0f252bc5
work_keys_str_mv	AT lamotkinalexey ononemethodforconstructingaprogrammedtrajectoryinproblemsofstabilizingaspacecraft AT misuranatalia ononemethodforconstructingaprogrammedtrajectoryinproblemsofstabilizingaspacecraft AT mityushovevgenij ononemethodforconstructingaprogrammedtrajectoryinproblemsofstabilizingaspacecraft
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On One Method for Constructing a Programmed Trajectory in Problems of Stabilizing a Spacecraft

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