Transfers between the Lagrangian points and the primaries considering radiation pressure

Detalhes bibliográficos
Autor(a) principal: Oliveira, Geraldo Magela C.
Data de Publicação: 2016
Outros Autores: Gomes, Vivian M. [UNESP], Prado, Antonio F. Bertachini De A., Sanchez, Diogo M.
Tipo de documento: Artigo de conferência
Idioma: eng
Título da fonte: Repositório Institucional da UNESP
Texto Completo: http://hdl.handle.net/11449/169291
Resumo: The idea of the present paper is to study transfers in the restricted three-body problem considering the effects of the radiation pressure in the trajectory of the spacecraft in a bi-impulsive maneuver. Three systems of primaries are used: Sun-Earth, a generic Sun-asteroid system and a system of asteroids. Transfers among the Lagrangian points and between the Lagrangian points and the primaries are considered. The results show that the radiation pressure has a significant participation in the process, in particular in the system formed by asteroids, because their gravitational forces are smaller compared with the systems having larger bodies. In the case of the asteroid system, it is possible to find solutions with lower fuel consumption by considering the solar radiation pressure. The idea is not to use the radiation pressure as a control, but just to measure its effects when performing the bi-impulsive transfer. It is very important to consider this force or the spacecraft will not reach the desired point.
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spelling Transfers between the Lagrangian points and the primaries considering radiation pressureThe idea of the present paper is to study transfers in the restricted three-body problem considering the effects of the radiation pressure in the trajectory of the spacecraft in a bi-impulsive maneuver. Three systems of primaries are used: Sun-Earth, a generic Sun-asteroid system and a system of asteroids. Transfers among the Lagrangian points and between the Lagrangian points and the primaries are considered. The results show that the radiation pressure has a significant participation in the process, in particular in the system formed by asteroids, because their gravitational forces are smaller compared with the systems having larger bodies. In the case of the asteroid system, it is possible to find solutions with lower fuel consumption by considering the solar radiation pressure. The idea is not to use the radiation pressure as a control, but just to measure its effects when performing the bi-impulsive transfer. It is very important to consider this force or the spacecraft will not reach the desired point.Board of the Graduate School National Institute for Space Research - INPESão Paulo State University FEG/UNESPDMC National Institute for Space Research - INPESchool of Aeronautics and Astronautics Purdue University, 701 West Stadium AvenueFederal Center for Technological Education of Minas Gerais - CEFET-MGSão Paulo State University FEG/UNESPNational Institute for Space Research - INPEUniversidade Estadual Paulista (Unesp)Purdue UniversityFederal Center for Technological Education of Minas Gerais - CEFET-MGOliveira, Geraldo Magela C.Gomes, Vivian M. [UNESP]Prado, Antonio F. Bertachini De A.Sanchez, Diogo M.2018-12-11T16:45:14Z2018-12-11T16:45:14Z2016-01-01info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/conferenceObject1513-1530Advances in the Astronautical Sciences, v. 158, p. 1513-1530.0065-3438http://hdl.handle.net/11449/1692912-s2.0-85007338113Scopusreponame:Repositório Institucional da UNESPinstname:Universidade Estadual Paulista (UNESP)instacron:UNESPengAdvances in the Astronautical Sciences0,187info:eu-repo/semantics/openAccess2021-10-23T21:44:29Zoai:repositorio.unesp.br:11449/169291Repositório InstitucionalPUBhttp://repositorio.unesp.br/oai/requestrepositoriounesp@unesp.bropendoar:29462021-10-23T21:44:29Repositório Institucional da UNESP - Universidade Estadual Paulista (UNESP)false
dc.title.none.fl_str_mv Transfers between the Lagrangian points and the primaries considering radiation pressure
title Transfers between the Lagrangian points and the primaries considering radiation pressure
spellingShingle Transfers between the Lagrangian points and the primaries considering radiation pressure
Oliveira, Geraldo Magela C.
title_short Transfers between the Lagrangian points and the primaries considering radiation pressure
title_full Transfers between the Lagrangian points and the primaries considering radiation pressure
title_fullStr Transfers between the Lagrangian points and the primaries considering radiation pressure
title_full_unstemmed Transfers between the Lagrangian points and the primaries considering radiation pressure
title_sort Transfers between the Lagrangian points and the primaries considering radiation pressure
author Oliveira, Geraldo Magela C.
author_facet Oliveira, Geraldo Magela C.
Gomes, Vivian M. [UNESP]
Prado, Antonio F. Bertachini De A.
Sanchez, Diogo M.
author_role author
author2 Gomes, Vivian M. [UNESP]
Prado, Antonio F. Bertachini De A.
Sanchez, Diogo M.
author2_role author
author
author
dc.contributor.none.fl_str_mv National Institute for Space Research - INPE
Universidade Estadual Paulista (Unesp)
Purdue University
Federal Center for Technological Education of Minas Gerais - CEFET-MG
dc.contributor.author.fl_str_mv Oliveira, Geraldo Magela C.
Gomes, Vivian M. [UNESP]
Prado, Antonio F. Bertachini De A.
Sanchez, Diogo M.
description The idea of the present paper is to study transfers in the restricted three-body problem considering the effects of the radiation pressure in the trajectory of the spacecraft in a bi-impulsive maneuver. Three systems of primaries are used: Sun-Earth, a generic Sun-asteroid system and a system of asteroids. Transfers among the Lagrangian points and between the Lagrangian points and the primaries are considered. The results show that the radiation pressure has a significant participation in the process, in particular in the system formed by asteroids, because their gravitational forces are smaller compared with the systems having larger bodies. In the case of the asteroid system, it is possible to find solutions with lower fuel consumption by considering the solar radiation pressure. The idea is not to use the radiation pressure as a control, but just to measure its effects when performing the bi-impulsive transfer. It is very important to consider this force or the spacecraft will not reach the desired point.
publishDate 2016
dc.date.none.fl_str_mv 2016-01-01
2018-12-11T16:45:14Z
2018-12-11T16:45:14Z
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. 158, p. 1513-1530.
0065-3438
http://hdl.handle.net/11449/169291
2-s2.0-85007338113
identifier_str_mv Advances in the Astronautical Sciences, v. 158, p. 1513-1530.
0065-3438
2-s2.0-85007338113
url http://hdl.handle.net/11449/169291
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv Advances in the Astronautical Sciences
0,187
dc.rights.driver.fl_str_mv info:eu-repo/semantics/openAccess
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv 1513-1530
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 repositoriounesp@unesp.br
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