Studying Close Approaches for a Cloud of Particles Considering Atmospheric Drag

Detalhes bibliográficos
Autor(a) principal: Gomes, Vivian Martins [UNESP]
Data de Publicação: 2013
Outros Autores: Formiga, Jorge, Moraes, Rodolpho Vilhena de
Tipo de documento: Artigo
Idioma: eng
Título da fonte: Repositório Institucional da UNESP
Texto Completo: http://dx.doi.org/10.1155/2013/468624
http://hdl.handle.net/11449/112103
Resumo: The present paper has the goal of studying close approaches between a planet and a group of particles. The mathematical model includes the presence of the atmosphere of the planet. This cloud is assumed to be created by the passage of the spacecraft in the atmosphere of the planet, which can cause the explosion of the spacecraft. The system is assumed to be formed by the Sun, the planet, and the spacecraft that explodes and becomes a cloud of particles. The Sun and the planet are assumed to be in circular orbits and the motion is planar. The equations of motion are the ones given by the circular planar restricted three-body problem combined with the forces given by the atmospheric drag. In the numerical simulations, the planet Jupiter is the celestial body used for the close approaches. The initial positions and velocities of the spacecraft and the particles are specified at the periapsis, because it is assumed that this is the point where the explosion occurs.
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spelling Studying Close Approaches for a Cloud of Particles Considering Atmospheric DragThe present paper has the goal of studying close approaches between a planet and a group of particles. The mathematical model includes the presence of the atmosphere of the planet. This cloud is assumed to be created by the passage of the spacecraft in the atmosphere of the planet, which can cause the explosion of the spacecraft. The system is assumed to be formed by the Sun, the planet, and the spacecraft that explodes and becomes a cloud of particles. The Sun and the planet are assumed to be in circular orbits and the motion is planar. The equations of motion are the ones given by the circular planar restricted three-body problem combined with the forces given by the atmospheric drag. In the numerical simulations, the planet Jupiter is the celestial body used for the close approaches. The initial positions and velocities of the spacecraft and the particles are specified at the periapsis, because it is assumed that this is the point where the explosion occurs.Fundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP)Univ Estadual Paulista FEG UNESP, Grp Dinam Orbital & Planetol, Jaboticabal, BrazilInst Nacl Pesquisas Espaciais INPE, Manaus, Amazonas, BrazilUniv Fed Sao Paulo ICT, Sao Paulo, BrazilUniv Estadual Paulista FEG UNESP, Grp Dinam Orbital & Planetol, Jaboticabal, BrazilFAPESP: 11/13101-4FAPESP: 12/21023-6Hindawi Publishing CorporationUniversidade Estadual Paulista (Unesp)Instituto Nacional de Pesquisas Espaciais (INPE)Universidade Federal de São Paulo (UNIFESP)Gomes, Vivian Martins [UNESP]Formiga, JorgeMoraes, Rodolpho Vilhena de2014-12-03T13:09:14Z2014-12-03T13:09:14Z2013-01-01info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/article10application/pdfhttp://dx.doi.org/10.1155/2013/468624Mathematical Problems In Engineering. New York: Hindawi Publishing Corporation, 10 p., 2013.1024-123Xhttp://hdl.handle.net/11449/11210310.1155/2013/468624WOS:000324999700001WOS000324999700001.pdf688090337616469077409171447574100000-0003-1289-8332Web of Sciencereponame:Repositório Institucional da UNESPinstname:Universidade Estadual Paulista (UNESP)instacron:UNESPengMathematical Problems in Engineering1.145info:eu-repo/semantics/openAccess2024-07-02T14:29:21Zoai:repositorio.unesp.br:11449/112103Repositório InstitucionalPUBhttp://repositorio.unesp.br/oai/requestopendoar:29462024-08-05T21:07:52.792026Repositório Institucional da UNESP - Universidade Estadual Paulista (UNESP)false
dc.title.none.fl_str_mv Studying Close Approaches for a Cloud of Particles Considering Atmospheric Drag
title Studying Close Approaches for a Cloud of Particles Considering Atmospheric Drag
spellingShingle Studying Close Approaches for a Cloud of Particles Considering Atmospheric Drag
Gomes, Vivian Martins [UNESP]
title_short Studying Close Approaches for a Cloud of Particles Considering Atmospheric Drag
title_full Studying Close Approaches for a Cloud of Particles Considering Atmospheric Drag
title_fullStr Studying Close Approaches for a Cloud of Particles Considering Atmospheric Drag
title_full_unstemmed Studying Close Approaches for a Cloud of Particles Considering Atmospheric Drag
title_sort Studying Close Approaches for a Cloud of Particles Considering Atmospheric Drag
author Gomes, Vivian Martins [UNESP]
author_facet Gomes, Vivian Martins [UNESP]
Formiga, Jorge
Moraes, Rodolpho Vilhena de
author_role author
author2 Formiga, Jorge
Moraes, Rodolpho Vilhena de
author2_role author
author
dc.contributor.none.fl_str_mv Universidade Estadual Paulista (Unesp)
Instituto Nacional de Pesquisas Espaciais (INPE)
Universidade Federal de São Paulo (UNIFESP)
dc.contributor.author.fl_str_mv Gomes, Vivian Martins [UNESP]
Formiga, Jorge
Moraes, Rodolpho Vilhena de
description The present paper has the goal of studying close approaches between a planet and a group of particles. The mathematical model includes the presence of the atmosphere of the planet. This cloud is assumed to be created by the passage of the spacecraft in the atmosphere of the planet, which can cause the explosion of the spacecraft. The system is assumed to be formed by the Sun, the planet, and the spacecraft that explodes and becomes a cloud of particles. The Sun and the planet are assumed to be in circular orbits and the motion is planar. The equations of motion are the ones given by the circular planar restricted three-body problem combined with the forces given by the atmospheric drag. In the numerical simulations, the planet Jupiter is the celestial body used for the close approaches. The initial positions and velocities of the spacecraft and the particles are specified at the periapsis, because it is assumed that this is the point where the explosion occurs.
publishDate 2013
dc.date.none.fl_str_mv 2013-01-01
2014-12-03T13:09:14Z
2014-12-03T13:09:14Z
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/10.1155/2013/468624
Mathematical Problems In Engineering. New York: Hindawi Publishing Corporation, 10 p., 2013.
1024-123X
http://hdl.handle.net/11449/112103
10.1155/2013/468624
WOS:000324999700001
WOS000324999700001.pdf
6880903376164690
7740917144757410
0000-0003-1289-8332
url http://dx.doi.org/10.1155/2013/468624
http://hdl.handle.net/11449/112103
identifier_str_mv Mathematical Problems In Engineering. New York: Hindawi Publishing Corporation, 10 p., 2013.
1024-123X
10.1155/2013/468624
WOS:000324999700001
WOS000324999700001.pdf
6880903376164690
7740917144757410
0000-0003-1289-8332
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv Mathematical Problems in Engineering
1.145
dc.rights.driver.fl_str_mv info:eu-repo/semantics/openAccess
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv 10
application/pdf
dc.publisher.none.fl_str_mv Hindawi Publishing Corporation
publisher.none.fl_str_mv Hindawi Publishing Corporation
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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