Trajectory analysis of a spacecraft making a three-dimensional powered swing-by maneuver

Detalhes bibliográficos
Autor(a) principal: Ferreira, A. F.S. [UNESP]
Data de Publicação: 2018
Outros Autores: Moraes, R. V. [UNESP], Prado, A. F.B.A., Winter, O. C. [UNESP]
Tipo de documento: Artigo de conferência
Idioma: eng
Título da fonte: Repositório Institucional da UNESP
Texto Completo: http://hdl.handle.net/11449/232879
Resumo: The present paper studies the problem of orbital maneuvers performed combining the passage of a spacecraft by a celestial body with an impulse applied to the spacecraft during the close approach. The motion of the spacecraft is assumed to be in the three-dimensional space, thus allowing plane change. This type of maneuver can also send the spacecraft to a point far from the orbit or to end in capture or collision of the spacecraft by the celestial body. The effects of the variations in the orbital plane, energy and the angular momentum of the spacecraft are presented.
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spelling Trajectory analysis of a spacecraft making a three-dimensional powered swing-by maneuverThe present paper studies the problem of orbital maneuvers performed combining the passage of a spacecraft by a celestial body with an impulse applied to the spacecraft during the close approach. The motion of the spacecraft is assumed to be in the three-dimensional space, thus allowing plane change. This type of maneuver can also send the spacecraft to a point far from the orbit or to end in capture or collision of the spacecraft by the celestial body. The effects of the variations in the orbital plane, energy and the angular momentum of the spacecraft are presented.Fundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP)Conselho Nacional de Desenvolvimento Científico e Tecnológico (CNPq)Department of Mathematics Universidade Estadual PaulistaINPE, Av. dos Astronautas, 1758INPE, Av. dos Astronautas 1758Department of Mathematics Universidade Estadual PaulistaFAPESP: 2016/14665-2FAPESP: 2016/23542-1FAPESP: 2016/24561-0CNPq: 300923/2017-1CNPq: 301338/2016-7CNPq: 312813/2013-9CNPq: 406841/2016-0Universidade Estadual Paulista (UNESP)INPEFerreira, A. F.S. [UNESP]Moraes, R. V. [UNESP]Prado, A. F.B.A.Winter, O. C. [UNESP]2022-04-30T18:07:58Z2022-04-30T18:07:58Z2018-01-01info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/conferenceObject1107-1126Advances in the Astronautical Sciences, v. 167, p. 1107-1126.0065-3438http://hdl.handle.net/11449/2328792-s2.0-85065332334Scopusreponame:Repositório Institucional da UNESPinstname:Universidade Estadual Paulista (UNESP)instacron:UNESPengAdvances in the Astronautical Sciencesinfo:eu-repo/semantics/openAccess2022-04-30T18:07:58Zoai:repositorio.unesp.br:11449/232879Repositório InstitucionalPUBhttp://repositorio.unesp.br/oai/requestopendoar:29462022-04-30T18:07:58Repositório Institucional da UNESP - Universidade Estadual Paulista (UNESP)false
dc.title.none.fl_str_mv Trajectory analysis of a spacecraft making a three-dimensional powered swing-by maneuver
title Trajectory analysis of a spacecraft making a three-dimensional powered swing-by maneuver
spellingShingle Trajectory analysis of a spacecraft making a three-dimensional powered swing-by maneuver
Ferreira, A. F.S. [UNESP]
title_short Trajectory analysis of a spacecraft making a three-dimensional powered swing-by maneuver
title_full Trajectory analysis of a spacecraft making a three-dimensional powered swing-by maneuver
title_fullStr Trajectory analysis of a spacecraft making a three-dimensional powered swing-by maneuver
title_full_unstemmed Trajectory analysis of a spacecraft making a three-dimensional powered swing-by maneuver
title_sort Trajectory analysis of a spacecraft making a three-dimensional powered swing-by maneuver
author Ferreira, A. F.S. [UNESP]
author_facet Ferreira, A. F.S. [UNESP]
Moraes, R. V. [UNESP]
Prado, A. F.B.A.
Winter, O. C. [UNESP]
author_role author
author2 Moraes, R. V. [UNESP]
Prado, A. F.B.A.
Winter, O. C. [UNESP]
author2_role author
author
author
dc.contributor.none.fl_str_mv Universidade Estadual Paulista (UNESP)
INPE
dc.contributor.author.fl_str_mv Ferreira, A. F.S. [UNESP]
Moraes, R. V. [UNESP]
Prado, A. F.B.A.
Winter, O. C. [UNESP]
description The present paper studies the problem of orbital maneuvers performed combining the passage of a spacecraft by a celestial body with an impulse applied to the spacecraft during the close approach. The motion of the spacecraft is assumed to be in the three-dimensional space, thus allowing plane change. This type of maneuver can also send the spacecraft to a point far from the orbit or to end in capture or collision of the spacecraft by the celestial body. The effects of the variations in the orbital plane, energy and the angular momentum of the spacecraft are presented.
publishDate 2018
dc.date.none.fl_str_mv 2018-01-01
2022-04-30T18:07:58Z
2022-04-30T18:07:58Z
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 Advances in the Astronautical Sciences, v. 167, p. 1107-1126.
0065-3438
http://hdl.handle.net/11449/232879
2-s2.0-85065332334
identifier_str_mv Advances in the Astronautical Sciences, v. 167, p. 1107-1126.
0065-3438
2-s2.0-85065332334
url http://hdl.handle.net/11449/232879
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv Advances in the Astronautical Sciences
dc.rights.driver.fl_str_mv info:eu-repo/semantics/openAccess
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv 1107-1126
dc.source.none.fl_str_mv Scopus
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_ 1799964383047057408

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