The algorithmic weak stability boundary in earth-to-moon mission design: dynamical aspects and applicability.

Detalhes bibliográficos
Autor(a) principal: Priscilla Andressa de Sousa Silva
Data de Publicação: 2011
Tipo de documento: Tese
Idioma: eng
Título da fonte: Biblioteca Digital de Teses e Dissertações do ITA
Texto Completo: http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=1111
Resumo: This thesis consists of an extensive study of the Weak Stability Boundary (WSB) concept in low-energy Earth-to-Moon mission design within the mathematical structure provided by the Planar Circular Restricted Three-Body Problem (PCR3BP). By employing the patched three-body approach to approximate the Sun-Earth-Moon-spacecraft system, we examine and characterize the construction of Earth-to-Moon transfer orbits. Then, we focus on the final portion of the transfer trajectories, investigating the WSB algorithmic definition proposed by E. Belbruno. We perform a dynamical characterization of the WSB associated sets generated in the lunar sphere of influence by two implementations of this algorithmic definition, namely, considering the Moon as a punctual mass and as a body with finite radius. In addition, the associated sets are analysed according to relevant criteria established on three-body problem elements in order to clarify their possible applicability in external and internal transfers and to verify the consistency of the algorithmic construction procedure. Finally, we extract the boundary of stability and investigate the structure of the boundary set by characterizing specific stable-unstable transitions. This study identifies various vulnerable aspects of the algorithmic definition concerning the adequate detection of stability regions for ballistic lunar capture, and indicates required corrections to the algorithmic construction.
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spelling The algorithmic weak stability boundary in earth-to-moon mission design: dynamical aspects and applicability.Mecânica celesteÓrbitas de transferênciaFunções hamiltonianasProblema de três corposSistemas Terra-LuaMissões espaciaisAstronomiaAstronáuticaThis thesis consists of an extensive study of the Weak Stability Boundary (WSB) concept in low-energy Earth-to-Moon mission design within the mathematical structure provided by the Planar Circular Restricted Three-Body Problem (PCR3BP). By employing the patched three-body approach to approximate the Sun-Earth-Moon-spacecraft system, we examine and characterize the construction of Earth-to-Moon transfer orbits. Then, we focus on the final portion of the transfer trajectories, investigating the WSB algorithmic definition proposed by E. Belbruno. We perform a dynamical characterization of the WSB associated sets generated in the lunar sphere of influence by two implementations of this algorithmic definition, namely, considering the Moon as a punctual mass and as a body with finite radius. In addition, the associated sets are analysed according to relevant criteria established on three-body problem elements in order to clarify their possible applicability in external and internal transfers and to verify the consistency of the algorithmic construction procedure. Finally, we extract the boundary of stability and investigate the structure of the boundary set by characterizing specific stable-unstable transitions. This study identifies various vulnerable aspects of the algorithmic definition concerning the adequate detection of stability regions for ballistic lunar capture, and indicates required corrections to the algorithmic construction.Instituto Tecnológico de AeronáuticaMaisa de Oliveira TerraPriscilla Andressa de Sousa Silva2011-02-10info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/doctoralThesishttp://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=1111reponame:Biblioteca Digital de Teses e Dissertações do ITAinstname:Instituto Tecnológico de Aeronáuticainstacron:ITAenginfo:eu-repo/semantics/openAccessapplication/pdf2019-02-02T14:02:34Zoai:agregador.ibict.br.BDTD_ITA:oai:ita.br:1111http://oai.bdtd.ibict.br/requestopendoar:null2020-05-28 19:35:24.453Biblioteca Digital de Teses e Dissertações do ITA - Instituto Tecnológico de Aeronáuticatrue
dc.title.none.fl_str_mv The algorithmic weak stability boundary in earth-to-moon mission design: dynamical aspects and applicability.
title The algorithmic weak stability boundary in earth-to-moon mission design: dynamical aspects and applicability.
spellingShingle The algorithmic weak stability boundary in earth-to-moon mission design: dynamical aspects and applicability.
Priscilla Andressa de Sousa Silva
Mecânica celeste
Órbitas de transferência
Funções hamiltonianas
Problema de três corpos
Sistemas Terra-Lua
Missões espaciais
Astronomia
Astronáutica
title_short The algorithmic weak stability boundary in earth-to-moon mission design: dynamical aspects and applicability.
title_full The algorithmic weak stability boundary in earth-to-moon mission design: dynamical aspects and applicability.
title_fullStr The algorithmic weak stability boundary in earth-to-moon mission design: dynamical aspects and applicability.
title_full_unstemmed The algorithmic weak stability boundary in earth-to-moon mission design: dynamical aspects and applicability.
title_sort The algorithmic weak stability boundary in earth-to-moon mission design: dynamical aspects and applicability.
author Priscilla Andressa de Sousa Silva
author_facet Priscilla Andressa de Sousa Silva
author_role author
dc.contributor.none.fl_str_mv Maisa de Oliveira Terra
dc.contributor.author.fl_str_mv Priscilla Andressa de Sousa Silva
dc.subject.por.fl_str_mv Mecânica celeste
Órbitas de transferência
Funções hamiltonianas
Problema de três corpos
Sistemas Terra-Lua
Missões espaciais
Astronomia
Astronáutica
topic Mecânica celeste
Órbitas de transferência
Funções hamiltonianas
Problema de três corpos
Sistemas Terra-Lua
Missões espaciais
Astronomia
Astronáutica
dc.description.none.fl_txt_mv This thesis consists of an extensive study of the Weak Stability Boundary (WSB) concept in low-energy Earth-to-Moon mission design within the mathematical structure provided by the Planar Circular Restricted Three-Body Problem (PCR3BP). By employing the patched three-body approach to approximate the Sun-Earth-Moon-spacecraft system, we examine and characterize the construction of Earth-to-Moon transfer orbits. Then, we focus on the final portion of the transfer trajectories, investigating the WSB algorithmic definition proposed by E. Belbruno. We perform a dynamical characterization of the WSB associated sets generated in the lunar sphere of influence by two implementations of this algorithmic definition, namely, considering the Moon as a punctual mass and as a body with finite radius. In addition, the associated sets are analysed according to relevant criteria established on three-body problem elements in order to clarify their possible applicability in external and internal transfers and to verify the consistency of the algorithmic construction procedure. Finally, we extract the boundary of stability and investigate the structure of the boundary set by characterizing specific stable-unstable transitions. This study identifies various vulnerable aspects of the algorithmic definition concerning the adequate detection of stability regions for ballistic lunar capture, and indicates required corrections to the algorithmic construction.
description This thesis consists of an extensive study of the Weak Stability Boundary (WSB) concept in low-energy Earth-to-Moon mission design within the mathematical structure provided by the Planar Circular Restricted Three-Body Problem (PCR3BP). By employing the patched three-body approach to approximate the Sun-Earth-Moon-spacecraft system, we examine and characterize the construction of Earth-to-Moon transfer orbits. Then, we focus on the final portion of the transfer trajectories, investigating the WSB algorithmic definition proposed by E. Belbruno. We perform a dynamical characterization of the WSB associated sets generated in the lunar sphere of influence by two implementations of this algorithmic definition, namely, considering the Moon as a punctual mass and as a body with finite radius. In addition, the associated sets are analysed according to relevant criteria established on three-body problem elements in order to clarify their possible applicability in external and internal transfers and to verify the consistency of the algorithmic construction procedure. Finally, we extract the boundary of stability and investigate the structure of the boundary set by characterizing specific stable-unstable transitions. This study identifies various vulnerable aspects of the algorithmic definition concerning the adequate detection of stability regions for ballistic lunar capture, and indicates required corrections to the algorithmic construction.
publishDate 2011
dc.date.none.fl_str_mv 2011-02-10
dc.type.driver.fl_str_mv info:eu-repo/semantics/publishedVersion
info:eu-repo/semantics/doctoralThesis
status_str publishedVersion
format doctoralThesis
dc.identifier.uri.fl_str_mv http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=1111
url http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=1111
dc.language.iso.fl_str_mv eng
language eng
dc.rights.driver.fl_str_mv info:eu-repo/semantics/openAccess
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv application/pdf
dc.publisher.none.fl_str_mv Instituto Tecnológico de Aeronáutica
publisher.none.fl_str_mv Instituto Tecnológico de Aeronáutica
dc.source.none.fl_str_mv reponame:Biblioteca Digital de Teses e Dissertações do ITA
instname:Instituto Tecnológico de Aeronáutica
instacron:ITA
reponame_str Biblioteca Digital de Teses e Dissertações do ITA
collection Biblioteca Digital de Teses e Dissertações do ITA
instname_str Instituto Tecnológico de Aeronáutica
instacron_str ITA
institution ITA
repository.name.fl_str_mv Biblioteca Digital de Teses e Dissertações do ITA - Instituto Tecnológico de Aeronáutica
repository.mail.fl_str_mv
subject_por_txtF_mv Mecânica celeste
Órbitas de transferência
Funções hamiltonianas
Problema de três corpos
Sistemas Terra-Lua
Missões espaciais
Astronomia
Astronáutica
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