Third-body perturbation in the case of elliptic orbits for the disturbing body
Autor(a) principal: | |
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Data de Publicação: | 2008 |
Outros Autores: | , |
Tipo de documento: | Artigo |
Idioma: | eng |
Título da fonte: | Repositório Institucional da UNESP |
Texto Completo: | http://dx.doi.org/10.1155/2008/763654 http://hdl.handle.net/11449/9290 |
Resumo: | This work presents a semi-analytical and numerical study of the perturbation caused in a spacecraft by a third-body using a double averaged analytical model with the disturbing function expanded in Legendre polynomials up to the second order. The important reason for this procedure is to eliminate terms due to the short periodic motion of the spacecraft and to show smooth curves for the evolution of the mean orbital elements for a long-time period. The aim of this study is to calculate the effect of lunar perturbations on the orbits of spacecrafts that are traveling around the Earth. An analysis of the stability of near-circular orbits is made, and a study to know under which conditions this orbit remains near circular completes this analysis. A study of the equatorial orbits is also performed. Copyright (C) 2008 R. C. Domingos et al. |
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Repositório Institucional da UNESP |
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spelling |
Third-body perturbation in the case of elliptic orbits for the disturbing bodyThis work presents a semi-analytical and numerical study of the perturbation caused in a spacecraft by a third-body using a double averaged analytical model with the disturbing function expanded in Legendre polynomials up to the second order. The important reason for this procedure is to eliminate terms due to the short periodic motion of the spacecraft and to show smooth curves for the evolution of the mean orbital elements for a long-time period. The aim of this study is to calculate the effect of lunar perturbations on the orbits of spacecrafts that are traveling around the Earth. An analysis of the stability of near-circular orbits is made, and a study to know under which conditions this orbit remains near circular completes this analysis. A study of the equatorial orbits is also performed. Copyright (C) 2008 R. C. Domingos et al.Univ Estadual Paulista UNESP, Dept Math, BR-12516410 São Paulo, BrazilINPE, BR-12227010 São Paulo, BrazilUniv Estadual Paulista UNESP, Dept Math, BR-12516410 São Paulo, BrazilHindawi Publishing CorporationUniversidade Estadual Paulista (Unesp)Instituto Nacional de Pesquisas Espaciais (INPE)Domingos, R. C. [UNESP]de Moraes, R. Vilhena [UNESP]Bertachini de Almeida Prado, A. F.2014-05-20T13:28:00Z2014-05-20T13:28:00Z2008-01-01info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/article14application/pdfhttp://dx.doi.org/10.1155/2008/763654Mathematical Problems In Engineering. New York: Hindawi Publishing Corporation, p. 14, 2008.1024-123Xhttp://hdl.handle.net/11449/929010.1155/2008/763654WOS:000258128500001WOS000258128500001.pdf774091714475741066521690834643270000-0002-0516-0420Web of Sciencereponame:Repositório Institucional da UNESPinstname:Universidade Estadual Paulista (UNESP)instacron:UNESPengMathematical Problems in Engineering1.145info:eu-repo/semantics/openAccess2023-10-26T06:04:32Zoai:repositorio.unesp.br:11449/9290Repositório InstitucionalPUBhttp://repositorio.unesp.br/oai/requestopendoar:29462023-10-26T06:04:32Repositório Institucional da UNESP - Universidade Estadual Paulista (UNESP)false |
dc.title.none.fl_str_mv |
Third-body perturbation in the case of elliptic orbits for the disturbing body |
title |
Third-body perturbation in the case of elliptic orbits for the disturbing body |
spellingShingle |
Third-body perturbation in the case of elliptic orbits for the disturbing body Domingos, R. C. [UNESP] |
title_short |
Third-body perturbation in the case of elliptic orbits for the disturbing body |
title_full |
Third-body perturbation in the case of elliptic orbits for the disturbing body |
title_fullStr |
Third-body perturbation in the case of elliptic orbits for the disturbing body |
title_full_unstemmed |
Third-body perturbation in the case of elliptic orbits for the disturbing body |
title_sort |
Third-body perturbation in the case of elliptic orbits for the disturbing body |
author |
Domingos, R. C. [UNESP] |
author_facet |
Domingos, R. C. [UNESP] de Moraes, R. Vilhena [UNESP] Bertachini de Almeida Prado, A. F. |
author_role |
author |
author2 |
de Moraes, R. Vilhena [UNESP] Bertachini de Almeida Prado, A. F. |
author2_role |
author author |
dc.contributor.none.fl_str_mv |
Universidade Estadual Paulista (Unesp) Instituto Nacional de Pesquisas Espaciais (INPE) |
dc.contributor.author.fl_str_mv |
Domingos, R. C. [UNESP] de Moraes, R. Vilhena [UNESP] Bertachini de Almeida Prado, A. F. |
description |
This work presents a semi-analytical and numerical study of the perturbation caused in a spacecraft by a third-body using a double averaged analytical model with the disturbing function expanded in Legendre polynomials up to the second order. The important reason for this procedure is to eliminate terms due to the short periodic motion of the spacecraft and to show smooth curves for the evolution of the mean orbital elements for a long-time period. The aim of this study is to calculate the effect of lunar perturbations on the orbits of spacecrafts that are traveling around the Earth. An analysis of the stability of near-circular orbits is made, and a study to know under which conditions this orbit remains near circular completes this analysis. A study of the equatorial orbits is also performed. Copyright (C) 2008 R. C. Domingos et al. |
publishDate |
2008 |
dc.date.none.fl_str_mv |
2008-01-01 2014-05-20T13:28:00Z 2014-05-20T13:28:00Z |
dc.type.status.fl_str_mv |
info:eu-repo/semantics/publishedVersion |
dc.type.driver.fl_str_mv |
info:eu-repo/semantics/article |
format |
article |
status_str |
publishedVersion |
dc.identifier.uri.fl_str_mv |
http://dx.doi.org/10.1155/2008/763654 Mathematical Problems In Engineering. New York: Hindawi Publishing Corporation, p. 14, 2008. 1024-123X http://hdl.handle.net/11449/9290 10.1155/2008/763654 WOS:000258128500001 WOS000258128500001.pdf 7740917144757410 6652169083464327 0000-0002-0516-0420 |
url |
http://dx.doi.org/10.1155/2008/763654 http://hdl.handle.net/11449/9290 |
identifier_str_mv |
Mathematical Problems In Engineering. New York: Hindawi Publishing Corporation, p. 14, 2008. 1024-123X 10.1155/2008/763654 WOS:000258128500001 WOS000258128500001.pdf 7740917144757410 6652169083464327 0000-0002-0516-0420 |
dc.language.iso.fl_str_mv |
eng |
language |
eng |
dc.relation.none.fl_str_mv |
Mathematical Problems in Engineering 1.145 |
dc.rights.driver.fl_str_mv |
info:eu-repo/semantics/openAccess |
eu_rights_str_mv |
openAccess |
dc.format.none.fl_str_mv |
14 application/pdf |
dc.publisher.none.fl_str_mv |
Hindawi Publishing Corporation |
publisher.none.fl_str_mv |
Hindawi Publishing Corporation |
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_ |
1799964700089253888 |