On stability of motion of satellite

In this paper we consider the translational and rotational motion of satellites around the Earth. First, we study the motion of an arrow-type satellite. We consider the system of equations of motion in the first approximation. We consider the linear Hamiltonian systems of differential equations. The...

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Main Author: Titova Tatiana
Format: Article
Language:English
Published: EDP Sciences 2023-01-01
Series:E3S Web of Conferences
Online Access:https://www.e3s-conferences.org/articles/e3sconf/pdf/2023/97/e3sconf_bft2023_09024.pdf
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author Titova Tatiana
author_facet Titova Tatiana
author_sort Titova Tatiana
collection DOAJ
description In this paper we consider the translational and rotational motion of satellites around the Earth. First, we study the motion of an arrow-type satellite. We consider the system of equations of motion in the first approximation. We consider the linear Hamiltonian systems of differential equations. The Hamiltonian systems arise in transportation problems. We consider the normalization of Hamiltonian matrix. We solve the system of matrix equations to find the generating function of the canonical transformation. We obtain stability criterion in several cases. Further, we study the motion of a spoke-type satellite. We consider eigenvalues of characteristic equation corresponding to the motion equations. We get the normal form of the Hamiltonian matrix. We obtain the stability criterion.
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spelling doaj.art-85ac96f08ef648efb84eb4db1c104e3c2024-01-26T10:38:40ZengEDP SciencesE3S Web of Conferences2267-12422023-01-014600902410.1051/e3sconf/202346009024e3sconf_bft2023_09024On stability of motion of satelliteTitova Tatiana0Moscow State University of Civil EngineeringIn this paper we consider the translational and rotational motion of satellites around the Earth. First, we study the motion of an arrow-type satellite. We consider the system of equations of motion in the first approximation. We consider the linear Hamiltonian systems of differential equations. The Hamiltonian systems arise in transportation problems. We consider the normalization of Hamiltonian matrix. We solve the system of matrix equations to find the generating function of the canonical transformation. We obtain stability criterion in several cases. Further, we study the motion of a spoke-type satellite. We consider eigenvalues of characteristic equation corresponding to the motion equations. We get the normal form of the Hamiltonian matrix. We obtain the stability criterion.https://www.e3s-conferences.org/articles/e3sconf/pdf/2023/97/e3sconf_bft2023_09024.pdf
spellingShingle Titova Tatiana
On stability of motion of satellite
E3S Web of Conferences
title On stability of motion of satellite
title_full On stability of motion of satellite
title_fullStr On stability of motion of satellite
title_full_unstemmed On stability of motion of satellite
title_short On stability of motion of satellite
title_sort on stability of motion of satellite
url https://www.e3s-conferences.org/articles/e3sconf/pdf/2023/97/e3sconf_bft2023_09024.pdf
work_keys_str_mv AT titovatatiana onstabilityofmotionofsatellite