A numerical mapping of energy gains in a powered Swing-By maneuver
Autor(a) principal: | |
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Data de Publicação: | 2017 |
Outros Autores: | , |
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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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 |
|
_version_ |
1808129458827165696 |