Third body perturbation using a single averaged model considering elliptic orbits for the disturbing body

Detalhes bibliográficos
Autor(a) principal: Domingos, Rita de C. [UNESP]
Data de Publicação: 2008
Outros Autores: de Moraes, Rodolpho V. [UNESP], de Almeida Prado, A. F. B.
Tipo de documento: Artigo de conferência
Idioma: eng
Título da fonte: Repositório Institucional da UNESP
Texto Completo: http://www.univelt.com/book=1740
http://hdl.handle.net/11449/39880
Resumo: In the present work, we expanded the study done by Solorzanol(1) including the eccentricity of the perturbing body. The assumptions used to develop the single-averaged analytical model are the same ones of the restricted elliptic three-body problem. The disturbing function was expanded in Legendre polynomials up to fourth-order. After that, the equations of motion are obtained from the planetary equations and we performed a set of numerical simulations. Different initial eccentricities for the perturbing and perturbed body are considered. The results obtained perform an analysis of the stability of a near-circular orbits and investigate under which conditions this orbit remain near-circular.
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spelling Third body perturbation using a single averaged model considering elliptic orbits for the disturbing bodyIn the present work, we expanded the study done by Solorzanol(1) including the eccentricity of the perturbing body. The assumptions used to develop the single-averaged analytical model are the same ones of the restricted elliptic three-body problem. The disturbing function was expanded in Legendre polynomials up to fourth-order. After that, the equations of motion are obtained from the planetary equations and we performed a set of numerical simulations. Different initial eccentricities for the perturbing and perturbed body are considered. The results obtained perform an analysis of the stability of a near-circular orbits and investigate under which conditions this orbit remain near-circular.UNESP, Grp Dinam Orbital & Planetol, Guarantingueta, SP, BrazilUNESP, Grp Dinam Orbital & Planetol, Guarantingueta, SP, BrazilUnivelt IncUniversidade Estadual Paulista (Unesp)Domingos, Rita de C. [UNESP]de Moraes, Rodolpho V. [UNESP]de Almeida Prado, A. F. B.2014-05-20T15:30:32Z2014-05-20T15:30:32Z2008-01-01info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/conferenceObject1571-1578http://www.univelt.com/book=1740Spaceflight Mechanics 2008, Vol 130, Pts 1 and 2. San Diego: Univelt Inc, v. 130, p. 1571-1578, 2008.1081-6003http://hdl.handle.net/11449/39880WOS:000258397800096Web of Sciencereponame:Repositório Institucional da UNESPinstname:Universidade Estadual Paulista (UNESP)instacron:UNESPengSpaceflight Mechanics 2008, Vol 130, Pts 1 and 2info:eu-repo/semantics/openAccess2024-07-02T14:29:48Zoai:repositorio.unesp.br:11449/39880Repositório InstitucionalPUBhttp://repositorio.unesp.br/oai/requestopendoar:29462024-08-05T21:23:56.171048Repositório Institucional da UNESP - Universidade Estadual Paulista (UNESP)false
dc.title.none.fl_str_mv Third body perturbation using a single averaged model considering elliptic orbits for the disturbing body
title Third body perturbation using a single averaged model considering elliptic orbits for the disturbing body
spellingShingle Third body perturbation using a single averaged model considering elliptic orbits for the disturbing body
Domingos, Rita de C. [UNESP]
title_short Third body perturbation using a single averaged model considering elliptic orbits for the disturbing body
title_full Third body perturbation using a single averaged model considering elliptic orbits for the disturbing body
title_fullStr Third body perturbation using a single averaged model considering elliptic orbits for the disturbing body
title_full_unstemmed Third body perturbation using a single averaged model considering elliptic orbits for the disturbing body
title_sort Third body perturbation using a single averaged model considering elliptic orbits for the disturbing body
author Domingos, Rita de C. [UNESP]
author_facet Domingos, Rita de C. [UNESP]
de Moraes, Rodolpho V. [UNESP]
de Almeida Prado, A. F. B.
author_role author
author2 de Moraes, Rodolpho V. [UNESP]
de Almeida Prado, A. F. B.
author2_role author
author
dc.contributor.none.fl_str_mv Universidade Estadual Paulista (Unesp)
dc.contributor.author.fl_str_mv Domingos, Rita de C. [UNESP]
de Moraes, Rodolpho V. [UNESP]
de Almeida Prado, A. F. B.
description In the present work, we expanded the study done by Solorzanol(1) including the eccentricity of the perturbing body. The assumptions used to develop the single-averaged analytical model are the same ones of the restricted elliptic three-body problem. The disturbing function was expanded in Legendre polynomials up to fourth-order. After that, the equations of motion are obtained from the planetary equations and we performed a set of numerical simulations. Different initial eccentricities for the perturbing and perturbed body are considered. The results obtained perform an analysis of the stability of a near-circular orbits and investigate under which conditions this orbit remain near-circular.
publishDate 2008
dc.date.none.fl_str_mv 2008-01-01
2014-05-20T15:30:32Z
2014-05-20T15:30:32Z
dc.type.status.fl_str_mv info:eu-repo/semantics/publishedVersion
dc.type.driver.fl_str_mv info:eu-repo/semantics/conferenceObject
format conferenceObject
status_str publishedVersion
dc.identifier.uri.fl_str_mv http://www.univelt.com/book=1740
Spaceflight Mechanics 2008, Vol 130, Pts 1 and 2. San Diego: Univelt Inc, v. 130, p. 1571-1578, 2008.
1081-6003
http://hdl.handle.net/11449/39880
WOS:000258397800096
url http://www.univelt.com/book=1740
http://hdl.handle.net/11449/39880
identifier_str_mv Spaceflight Mechanics 2008, Vol 130, Pts 1 and 2. San Diego: Univelt Inc, v. 130, p. 1571-1578, 2008.
1081-6003
WOS:000258397800096
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv Spaceflight Mechanics 2008, Vol 130, Pts 1 and 2
dc.rights.driver.fl_str_mv info:eu-repo/semantics/openAccess
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv 1571-1578
dc.publisher.none.fl_str_mv Univelt Inc
publisher.none.fl_str_mv Univelt Inc
dc.source.none.fl_str_mv Web of Science
reponame:Repositório Institucional da UNESP
instname:Universidade Estadual Paulista (UNESP)
instacron:UNESP
instname_str Universidade Estadual Paulista (UNESP)
instacron_str UNESP
institution UNESP
reponame_str Repositório Institucional da UNESP
collection Repositório Institucional da UNESP
repository.name.fl_str_mv Repositório Institucional da UNESP - Universidade Estadual Paulista (UNESP)
repository.mail.fl_str_mv
_version_ 1808129316624531456

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