A numerical mapping of energy gains in a powered Swing-By maneuver

Detalhes bibliográficos
Autor(a) principal: Ferreira, Alessandra F. S.
Data de Publicação: 2017
Outros Autores: Prado, Antonio F. B. A., Winter, Othon C. [UNESP]
Tipo de documento: Artigo
Idioma: eng
Título da fonte: Repositório Institucional da UNESP
Texto Completo: http://dx.doi.org/10.1007/s11071-017-3485-2
http://hdl.handle.net/11449/165651
Resumo: The present paper studies the effects of a powered Swing-By maneuver, considering the particular and important situations where there are energy gains for the spacecraft. The objective is to map the energy variations obtained from this maneuver as a function of the three parameters that identify the pure gravity Swing-By with a fixed mass ratio (angle of approach, periapsis distance and velocity at periapsis) and the three parameters that define the impulsive maneuver (direction, magnitude and the point where the impulse is applied). The mathematical model used here is the version of the restricted three-body problem that includes the LemaItre regularization, to increase the accuracy of the numerical integrations. It is developed and implemented by an algorithm that obtains the energy variation of the spacecraft with respect to the largest primary of the system in a maneuver where the impulse is applied inside the sphere of influence of the secondary body, during the passage of the spacecraft. The point of application of the impulse is a free parameter, as well as the direction of the impulse. The results make a complete map of the possibilities, including the maximum gains of energy, but also showing alternatives that can be used considering particularities of the mission.
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spelling A numerical mapping of energy gains in a powered Swing-By maneuverAstrodynamicsSwing-ByClose approachOrbital maneuversInterplanetary missionsThe present paper studies the effects of a powered Swing-By maneuver, considering the particular and important situations where there are energy gains for the spacecraft. The objective is to map the energy variations obtained from this maneuver as a function of the three parameters that identify the pure gravity Swing-By with a fixed mass ratio (angle of approach, periapsis distance and velocity at periapsis) and the three parameters that define the impulsive maneuver (direction, magnitude and the point where the impulse is applied). The mathematical model used here is the version of the restricted three-body problem that includes the LemaItre regularization, to increase the accuracy of the numerical integrations. It is developed and implemented by an algorithm that obtains the energy variation of the spacecraft with respect to the largest primary of the system in a maneuver where the impulse is applied inside the sphere of influence of the secondary body, during the passage of the spacecraft. The point of application of the impulse is a free parameter, as well as the direction of the impulse. The results make a complete map of the possibilities, including the maximum gains of energy, but also showing alternatives that can be used considering particularities of the mission.Conselho Nacional de Desenvolvimento Científico e Tecnológico (CNPq)Fundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP)Coordenação de Aperfeiçoamento de Pessoal de Nível Superior (CAPES)Inst Nacl Pesquisas Espaciais, BR-12227010 Sao Paulo, BrazilUniv Estadual Paulista, BR-12516410 Sao Paulo, BrazilUniv Estadual Paulista, BR-12516410 Sao Paulo, BrazilCNPq: 304700/2009-6FAPESP: 2011/08171-3FAPESP: 2014/06688-7SpringerInst Nacl Pesquisas EspaciaisUniversidade Estadual Paulista (Unesp)Ferreira, Alessandra F. S.Prado, Antonio F. B. A.Winter, Othon C. [UNESP]2018-11-28T14:21:46Z2018-11-28T14:21:46Z2017-07-01info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/article791-818application/pdfhttp://dx.doi.org/10.1007/s11071-017-3485-2Nonlinear Dynamics. Dordrecht: Springer, v. 89, n. 2, p. 791-818, 2017.0924-090Xhttp://hdl.handle.net/11449/16565110.1007/s11071-017-3485-2WOS:000404756600003WOS000404756600003.pdfWeb of Sciencereponame:Repositório Institucional da UNESPinstname:Universidade Estadual Paulista (UNESP)instacron:UNESPengNonlinear Dynamicsinfo:eu-repo/semantics/openAccess2024-07-02T14:29:31Zoai:repositorio.unesp.br:11449/165651Repositório InstitucionalPUBhttp://repositorio.unesp.br/oai/requestopendoar:29462024-08-05T22:45:20.132178Repositório Institucional da UNESP - Universidade Estadual Paulista (UNESP)false
dc.title.none.fl_str_mv A numerical mapping of energy gains in a powered Swing-By maneuver
title A numerical mapping of energy gains in a powered Swing-By maneuver
spellingShingle A numerical mapping of energy gains in a powered Swing-By maneuver
Ferreira, Alessandra F. S.
Astrodynamics
Swing-By
Close approach
Orbital maneuvers
Interplanetary missions
title_short A numerical mapping of energy gains in a powered Swing-By maneuver
title_full A numerical mapping of energy gains in a powered Swing-By maneuver
title_fullStr A numerical mapping of energy gains in a powered Swing-By maneuver
title_full_unstemmed A numerical mapping of energy gains in a powered Swing-By maneuver
title_sort A numerical mapping of energy gains in a powered Swing-By maneuver
author Ferreira, Alessandra F. S.
author_facet Ferreira, Alessandra F. S.
Prado, Antonio F. B. A.
Winter, Othon C. [UNESP]
author_role author
author2 Prado, Antonio F. B. A.
Winter, Othon C. [UNESP]
author2_role author
author
dc.contributor.none.fl_str_mv Inst Nacl Pesquisas Espaciais
Universidade Estadual Paulista (Unesp)
dc.contributor.author.fl_str_mv Ferreira, Alessandra F. S.
Prado, Antonio F. B. A.
Winter, Othon C. [UNESP]
dc.subject.por.fl_str_mv Astrodynamics
Swing-By
Close approach
Orbital maneuvers
Interplanetary missions
topic Astrodynamics
Swing-By
Close approach
Orbital maneuvers
Interplanetary missions
description The present paper studies the effects of a powered Swing-By maneuver, considering the particular and important situations where there are energy gains for the spacecraft. The objective is to map the energy variations obtained from this maneuver as a function of the three parameters that identify the pure gravity Swing-By with a fixed mass ratio (angle of approach, periapsis distance and velocity at periapsis) and the three parameters that define the impulsive maneuver (direction, magnitude and the point where the impulse is applied). The mathematical model used here is the version of the restricted three-body problem that includes the LemaItre regularization, to increase the accuracy of the numerical integrations. It is developed and implemented by an algorithm that obtains the energy variation of the spacecraft with respect to the largest primary of the system in a maneuver where the impulse is applied inside the sphere of influence of the secondary body, during the passage of the spacecraft. The point of application of the impulse is a free parameter, as well as the direction of the impulse. The results make a complete map of the possibilities, including the maximum gains of energy, but also showing alternatives that can be used considering particularities of the mission.
publishDate 2017
dc.date.none.fl_str_mv 2017-07-01
2018-11-28T14:21:46Z
2018-11-28T14:21:46Z
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/10.1007/s11071-017-3485-2
Nonlinear Dynamics. Dordrecht: Springer, v. 89, n. 2, p. 791-818, 2017.
0924-090X
http://hdl.handle.net/11449/165651
10.1007/s11071-017-3485-2
WOS:000404756600003
WOS000404756600003.pdf
url http://dx.doi.org/10.1007/s11071-017-3485-2
http://hdl.handle.net/11449/165651
identifier_str_mv Nonlinear Dynamics. Dordrecht: Springer, v. 89, n. 2, p. 791-818, 2017.
0924-090X
10.1007/s11071-017-3485-2
WOS:000404756600003
WOS000404756600003.pdf
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv Nonlinear Dynamics
dc.rights.driver.fl_str_mv info:eu-repo/semantics/openAccess
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv 791-818
application/pdf
dc.publisher.none.fl_str_mv Springer
publisher.none.fl_str_mv Springer
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
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