Stationary configurations of space tether anchored on smaller primary in three-body problem

Detalhes bibliográficos
Autor(a) principal: Ferreira, A. F. S. [UNESP]
Data de Publicação: 2019
Outros Autores: Burov, A. A., Guerman, A. D., Prado, A. F. B. A., Nikonov, V.
Tipo de documento: Artigo
Idioma: eng
Título da fonte: Repositório Institucional da UNESP
Texto Completo: http://dx.doi.org/10.1016/j.actaastro.2019.01.031
http://hdl.handle.net/11449/184541
Resumo: Spatial dynamics of a system composed by a planet, its moon and a spacecraft tethered to the moon surface is studied in the framework of circular restricted three-body problem. The moon is assumed to be in synchronous condition (1:1 mean motion resonances) so as to keep its orientation with respect to the planet; the size of the moon is non-negligible. The tether is considered to be light and inextensible. Equilibrium configurations of the tether are identified; their stability is analyzed. The bifurcation points, where the number of equilibria changes and new branches arise, are determined. The theoretical results are applied to particular cases of the Earth-Moon, Mars-Phobos and Pluto-Charon systems.
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spelling Stationary configurations of space tether anchored on smaller primary in three-body problemTether systemSpace elevatorTether dynamicsMoon explorationSmall celestial bodiesSpatial dynamics of a system composed by a planet, its moon and a spacecraft tethered to the moon surface is studied in the framework of circular restricted three-body problem. The moon is assumed to be in synchronous condition (1:1 mean motion resonances) so as to keep its orientation with respect to the planet; the size of the moon is non-negligible. The tether is considered to be light and inextensible. Equilibrium configurations of the tether are identified; their stability is analyzed. The bifurcation points, where the number of equilibria changes and new branches arise, are determined. The theoretical results are applied to particular cases of the Earth-Moon, Mars-Phobos and Pluto-Charon systems.RFBRPortuguese Foundation for Science and Technologies via Centre for Mechanical and Aerospace Science and Technologies, C-MASTNatl Space Res Sao Paulo State Univ, BR-12516410 Sao Paulo, BrazilRussian Acad Sci, Fed Res Ctr Comp Sci & Control, Moscow, RussiaNatl Res Univ, Higher Sch Econ, Moscow, RussiaUniv Beira Interior, CMAST, Covilha, PortugalNatl Space Res Inst, BR-12227010 Sao Paulo, BrazilNatl Space Res Sao Paulo State Univ, BR-12516410 Sao Paulo, BrazilRFBR: 16-01-00625RFBR: 18-01-00335RFBR: EMaDeS (Centro-01-0145-FEDER-000017)Portuguese Foundation for Science and Technologies via Centre for Mechanical and Aerospace Science and Technologies, C-MAST: POCI-01-0145-FEDER-007718Elsevier B.V.Universidade Estadual Paulista (Unesp)Russian Acad SciNatl Res UnivUniv Beira InteriorNatl Space Res InstFerreira, A. F. S. [UNESP]Burov, A. A.Guerman, A. D.Prado, A. F. B. A.Nikonov, V.2019-10-04T12:14:31Z2019-10-04T12:14:31Z2019-07-01info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/article572-582http://dx.doi.org/10.1016/j.actaastro.2019.01.031Acta Astronautica. Oxford: Pergamon-elsevier Science Ltd, v. 160, p. 572-582, 2019.0094-5765http://hdl.handle.net/11449/18454110.1016/j.actaastro.2019.01.031WOS:000472695500057Web of Sciencereponame:Repositório Institucional da UNESPinstname:Universidade Estadual Paulista (UNESP)instacron:UNESPengActa Astronauticainfo:eu-repo/semantics/openAccess2021-10-23T15:01:15Zoai:repositorio.unesp.br:11449/184541Repositório InstitucionalPUBhttp://repositorio.unesp.br/oai/requestopendoar:29462024-08-05T19:28:11.772367Repositório Institucional da UNESP - Universidade Estadual Paulista (UNESP)false
dc.title.none.fl_str_mv Stationary configurations of space tether anchored on smaller primary in three-body problem
title Stationary configurations of space tether anchored on smaller primary in three-body problem
spellingShingle Stationary configurations of space tether anchored on smaller primary in three-body problem
Ferreira, A. F. S. [UNESP]
Tether system
Space elevator
Tether dynamics
Moon exploration
Small celestial bodies
title_short Stationary configurations of space tether anchored on smaller primary in three-body problem
title_full Stationary configurations of space tether anchored on smaller primary in three-body problem
title_fullStr Stationary configurations of space tether anchored on smaller primary in three-body problem
title_full_unstemmed Stationary configurations of space tether anchored on smaller primary in three-body problem
title_sort Stationary configurations of space tether anchored on smaller primary in three-body problem
author Ferreira, A. F. S. [UNESP]
author_facet Ferreira, A. F. S. [UNESP]
Burov, A. A.
Guerman, A. D.
Prado, A. F. B. A.
Nikonov, V.
author_role author
author2 Burov, A. A.
Guerman, A. D.
Prado, A. F. B. A.
Nikonov, V.
author2_role author
author
author
author
dc.contributor.none.fl_str_mv Universidade Estadual Paulista (Unesp)
Russian Acad Sci
Natl Res Univ
Univ Beira Interior
Natl Space Res Inst
dc.contributor.author.fl_str_mv Ferreira, A. F. S. [UNESP]
Burov, A. A.
Guerman, A. D.
Prado, A. F. B. A.
Nikonov, V.
dc.subject.por.fl_str_mv Tether system
Space elevator
Tether dynamics
Moon exploration
Small celestial bodies
topic Tether system
Space elevator
Tether dynamics
Moon exploration
Small celestial bodies
description Spatial dynamics of a system composed by a planet, its moon and a spacecraft tethered to the moon surface is studied in the framework of circular restricted three-body problem. The moon is assumed to be in synchronous condition (1:1 mean motion resonances) so as to keep its orientation with respect to the planet; the size of the moon is non-negligible. The tether is considered to be light and inextensible. Equilibrium configurations of the tether are identified; their stability is analyzed. The bifurcation points, where the number of equilibria changes and new branches arise, are determined. The theoretical results are applied to particular cases of the Earth-Moon, Mars-Phobos and Pluto-Charon systems.
publishDate 2019
dc.date.none.fl_str_mv 2019-10-04T12:14:31Z
2019-10-04T12:14:31Z
2019-07-01
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/10.1016/j.actaastro.2019.01.031
Acta Astronautica. Oxford: Pergamon-elsevier Science Ltd, v. 160, p. 572-582, 2019.
0094-5765
http://hdl.handle.net/11449/184541
10.1016/j.actaastro.2019.01.031
WOS:000472695500057
url http://dx.doi.org/10.1016/j.actaastro.2019.01.031
http://hdl.handle.net/11449/184541
identifier_str_mv Acta Astronautica. Oxford: Pergamon-elsevier Science Ltd, v. 160, p. 572-582, 2019.
0094-5765
10.1016/j.actaastro.2019.01.031
WOS:000472695500057
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv Acta Astronautica
dc.rights.driver.fl_str_mv info:eu-repo/semantics/openAccess
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv 572-582
dc.publisher.none.fl_str_mv Elsevier B.V.
publisher.none.fl_str_mv Elsevier B.V.
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_ 1808129072765599744

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