Lifetime and Dynamics of Natural Orbits around Titan

Detalhes bibliográficos
Autor(a) principal: Ferreira, Lucas S. [UNESP]
Data de Publicação: 2022
Outros Autores: Sfair, Rafael [UNESP], Prado, Antônio F. Bertachini A.
Tipo de documento: Artigo
Idioma: eng
Título da fonte: Repositório Institucional da UNESP
Texto Completo: http://dx.doi.org/10.3390/sym14061243
http://hdl.handle.net/11449/240329
Resumo: Considering the growing interest in sending probes to the natural satellite Titan, our work aims to investigate and map natural orbits around this moon. For that, we use mathematical models with forces that have symmetry/asymmetry phenomena, depending on the force, applied to orbits around Titan. We evaluated the effects due to the gravitational attraction of the Saturn, together with the perturbative effects coming from the non-sphericity of Titan (the gravitational coefficient J2) and the effects of the atmospheric drag present in the natural satellite. Lifetime maps were generated for different initial configurations of the orbit of the probe, which were analyzed in different scenarios of orbital perturbations. The results showed the existence of orbits surviving at least 20 years and conditions with shorter times, but sufficient to carry out possible missions, including the important polar orbits. Furthermore, the investigation of the oscillation rate of the altitude of the probe, called coefficient ∆, proposed in this work, showed orbital conditions that result in more minor oscillations in the altitude of the spacecraft.
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spelling Lifetime and Dynamics of Natural Orbits around Titanastrodynamicslifetime of orbitsmission designplanetary satelliteTitanConsidering the growing interest in sending probes to the natural satellite Titan, our work aims to investigate and map natural orbits around this moon. For that, we use mathematical models with forces that have symmetry/asymmetry phenomena, depending on the force, applied to orbits around Titan. We evaluated the effects due to the gravitational attraction of the Saturn, together with the perturbative effects coming from the non-sphericity of Titan (the gravitational coefficient J2) and the effects of the atmospheric drag present in the natural satellite. Lifetime maps were generated for different initial configurations of the orbit of the probe, which were analyzed in different scenarios of orbital perturbations. The results showed the existence of orbits surviving at least 20 years and conditions with shorter times, but sufficient to carry out possible missions, including the important polar orbits. Furthermore, the investigation of the oscillation rate of the altitude of the probe, called coefficient ∆, proposed in this work, showed orbital conditions that result in more minor oscillations in the altitude of the spacecraft.Coordenação de Aperfeiçoamento de Pessoal de Nível Superior (CAPES)Conselho Nacional de Desenvolvimento Científico e Tecnológico (CNPq)Deutsche ForschungsgemeinschaftGrupo de Dinâmica Orbital e Planetologia (GDOP) São Paulo State University (UNESP), SPInstitut für Astronomie und Astrophysik Eberhard Karls Universität Tübingen, Auf der Morgenstelle 10Academy of Engineering Peoples’ Friendship University of Russia (RUDN University), 6 Miklukho-Maklaya StreetPostgraduate Division National Institute for Space Research (INPE), , SPGrupo de Dinâmica Orbital e Planetologia (GDOP) São Paulo State University (UNESP), SPCAPES: 001CNPq: 309089/2021-CNPq: 309089/2021-2Deutsche Forschungsgemeinschaft: 446102036Universidade Estadual Paulista (UNESP)Eberhard Karls Universität TübingenPeoples’ Friendship University of Russia (RUDN University)National Institute for Space Research (INPE)Ferreira, Lucas S. [UNESP]Sfair, Rafael [UNESP]Prado, Antônio F. Bertachini A.2023-03-01T20:12:17Z2023-03-01T20:12:17Z2022-06-01info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/articlehttp://dx.doi.org/10.3390/sym14061243Symmetry, v. 14, n. 6, 2022.2073-8994http://hdl.handle.net/11449/24032910.3390/sym140612432-s2.0-85132730719Scopusreponame:Repositório Institucional da UNESPinstname:Universidade Estadual Paulista (UNESP)instacron:UNESPengSymmetryinfo:eu-repo/semantics/openAccess2023-03-01T20:12:17Zoai:repositorio.unesp.br:11449/240329Repositório InstitucionalPUBhttp://repositorio.unesp.br/oai/requestopendoar:29462024-08-05T20:24:52.062425Repositório Institucional da UNESP - Universidade Estadual Paulista (UNESP)false
dc.title.none.fl_str_mv Lifetime and Dynamics of Natural Orbits around Titan
title Lifetime and Dynamics of Natural Orbits around Titan
spellingShingle Lifetime and Dynamics of Natural Orbits around Titan
Ferreira, Lucas S. [UNESP]
astrodynamics
lifetime of orbits
mission design
planetary satellite
Titan
title_short Lifetime and Dynamics of Natural Orbits around Titan
title_full Lifetime and Dynamics of Natural Orbits around Titan
title_fullStr Lifetime and Dynamics of Natural Orbits around Titan
title_full_unstemmed Lifetime and Dynamics of Natural Orbits around Titan
title_sort Lifetime and Dynamics of Natural Orbits around Titan
author Ferreira, Lucas S. [UNESP]
author_facet Ferreira, Lucas S. [UNESP]
Sfair, Rafael [UNESP]
Prado, Antônio F. Bertachini A.
author_role author
author2 Sfair, Rafael [UNESP]
Prado, Antônio F. Bertachini A.
author2_role author
author
dc.contributor.none.fl_str_mv Universidade Estadual Paulista (UNESP)
Eberhard Karls Universität Tübingen
Peoples’ Friendship University of Russia (RUDN University)
National Institute for Space Research (INPE)
dc.contributor.author.fl_str_mv Ferreira, Lucas S. [UNESP]
Sfair, Rafael [UNESP]
Prado, Antônio F. Bertachini A.
dc.subject.por.fl_str_mv astrodynamics
lifetime of orbits
mission design
planetary satellite
Titan
topic astrodynamics
lifetime of orbits
mission design
planetary satellite
Titan
description Considering the growing interest in sending probes to the natural satellite Titan, our work aims to investigate and map natural orbits around this moon. For that, we use mathematical models with forces that have symmetry/asymmetry phenomena, depending on the force, applied to orbits around Titan. We evaluated the effects due to the gravitational attraction of the Saturn, together with the perturbative effects coming from the non-sphericity of Titan (the gravitational coefficient J2) and the effects of the atmospheric drag present in the natural satellite. Lifetime maps were generated for different initial configurations of the orbit of the probe, which were analyzed in different scenarios of orbital perturbations. The results showed the existence of orbits surviving at least 20 years and conditions with shorter times, but sufficient to carry out possible missions, including the important polar orbits. Furthermore, the investigation of the oscillation rate of the altitude of the probe, called coefficient ∆, proposed in this work, showed orbital conditions that result in more minor oscillations in the altitude of the spacecraft.
publishDate 2022
dc.date.none.fl_str_mv 2022-06-01
2023-03-01T20:12:17Z
2023-03-01T20:12:17Z
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/10.3390/sym14061243
Symmetry, v. 14, n. 6, 2022.
2073-8994
http://hdl.handle.net/11449/240329
10.3390/sym14061243
2-s2.0-85132730719
url http://dx.doi.org/10.3390/sym14061243
http://hdl.handle.net/11449/240329
identifier_str_mv Symmetry, v. 14, n. 6, 2022.
2073-8994
10.3390/sym14061243
2-s2.0-85132730719
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv Symmetry
dc.rights.driver.fl_str_mv info:eu-repo/semantics/openAccess
eu_rights_str_mv openAccess
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
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