Study of the roto-orbital motion using intermediaries: numerical experiments

Detalhes bibliográficos
Autor(a) principal: Cardoso dos Santos, Josué [UNESP]
Data de Publicação: 2019
Outros Autores: Ferrer, Sebastián, Scheeres, Daniel J.
Tipo de documento: Artigo
Idioma: eng
Título da fonte: Repositório Institucional da UNESP
Texto Completo: http://dx.doi.org/10.1007/s10569-019-9900-x
http://hdl.handle.net/11449/187714
Resumo: The purpose of the present study is to test two recently proposed integrable models to study the roto-orbital motion of an axisymmetric rigid body, considering this body under the influence of a central gravitational field. Based on the concept of intermediary, both models are treated in Hamiltonian formalism, as perturbation of the Keplerian–Eulerian motion, using canonical variables associated with the total angular momentum. Parameters are introduced to visualize possibilities for different applications; nevertheless, we concentrate on the binary asteroid-type dynamics. Numerical experiments compare the two intermediaries with respect to the original model. Several values for attitude, shape, orbital eccentricity and distance are considered for systems with a slow-rotating axisymmetric rigid body in an eccentric relative orbit, i.e., with significant disturbing effects. In general, both models present good precision in wide regions of the dynamical parameters spaces defined.
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spelling Study of the roto-orbital motion using intermediaries: numerical experimentsElimination of the parallaxIntermediariesPerturbation theoryRoto-orbital dynamicsThe purpose of the present study is to test two recently proposed integrable models to study the roto-orbital motion of an axisymmetric rigid body, considering this body under the influence of a central gravitational field. Based on the concept of intermediary, both models are treated in Hamiltonian formalism, as perturbation of the Keplerian–Eulerian motion, using canonical variables associated with the total angular momentum. Parameters are introduced to visualize possibilities for different applications; nevertheless, we concentrate on the binary asteroid-type dynamics. Numerical experiments compare the two intermediaries with respect to the original model. Several values for attitude, shape, orbital eccentricity and distance are considered for systems with a slow-rotating axisymmetric rigid body in an eccentric relative orbit, i.e., with significant disturbing effects. In general, both models present good precision in wide regions of the dynamical parameters spaces defined.Fundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP)Ministerio de Economía y CompetitividadFundación SénecaDepartment of Physics/Group of Orbital Dynamics and Planetology São Paulo State University (UNESP)Asher Space Research Institute Israel Institute of Technology (Technion)Space Dynamics Group DITEC Facultad Informática Universidad de MurciaAnn H.J. Smead Department of Aerospace Engineering Science University of ColoradoDepartment of Physics/Group of Orbital Dynamics and Planetology São Paulo State University (UNESP)FAPESP: 2013/26652-6FAPESP: 2015/18881-9Ministerio de Economía y Competitividad: ESP2017-87271-PFundación Séneca: MTM2015-64095-PUniversidade Estadual Paulista (Unesp)Israel Institute of Technology (Technion)Universidad de MurciaUniversity of ColoradoCardoso dos Santos, Josué [UNESP]Ferrer, SebastiánScheeres, Daniel J.2019-10-06T15:45:01Z2019-10-06T15:45:01Z2019-06-01info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/articlehttp://dx.doi.org/10.1007/s10569-019-9900-xCelestial Mechanics and Dynamical Astronomy, v. 131, n. 6, 2019.1572-94780923-2958http://hdl.handle.net/11449/18771410.1007/s10569-019-9900-x2-s2.0-85066791886Scopusreponame:Repositório Institucional da UNESPinstname:Universidade Estadual Paulista (UNESP)instacron:UNESPengCelestial Mechanics and Dynamical Astronomyinfo:eu-repo/semantics/openAccess2021-10-23T00:57:09Zoai:repositorio.unesp.br:11449/187714Repositório InstitucionalPUBhttp://repositorio.unesp.br/oai/requestopendoar:29462024-08-05T21:31:50.916706Repositório Institucional da UNESP - Universidade Estadual Paulista (UNESP)false
dc.title.none.fl_str_mv Study of the roto-orbital motion using intermediaries: numerical experiments
title Study of the roto-orbital motion using intermediaries: numerical experiments
spellingShingle Study of the roto-orbital motion using intermediaries: numerical experiments
Cardoso dos Santos, Josué [UNESP]
Elimination of the parallax
Intermediaries
Perturbation theory
Roto-orbital dynamics
title_short Study of the roto-orbital motion using intermediaries: numerical experiments
title_full Study of the roto-orbital motion using intermediaries: numerical experiments
title_fullStr Study of the roto-orbital motion using intermediaries: numerical experiments
title_full_unstemmed Study of the roto-orbital motion using intermediaries: numerical experiments
title_sort Study of the roto-orbital motion using intermediaries: numerical experiments
author Cardoso dos Santos, Josué [UNESP]
author_facet Cardoso dos Santos, Josué [UNESP]
Ferrer, Sebastián
Scheeres, Daniel J.
author_role author
author2 Ferrer, Sebastián
Scheeres, Daniel J.
author2_role author
author
dc.contributor.none.fl_str_mv Universidade Estadual Paulista (Unesp)
Israel Institute of Technology (Technion)
Universidad de Murcia
University of Colorado
dc.contributor.author.fl_str_mv Cardoso dos Santos, Josué [UNESP]
Ferrer, Sebastián
Scheeres, Daniel J.
dc.subject.por.fl_str_mv Elimination of the parallax
Intermediaries
Perturbation theory
Roto-orbital dynamics
topic Elimination of the parallax
Intermediaries
Perturbation theory
Roto-orbital dynamics
description The purpose of the present study is to test two recently proposed integrable models to study the roto-orbital motion of an axisymmetric rigid body, considering this body under the influence of a central gravitational field. Based on the concept of intermediary, both models are treated in Hamiltonian formalism, as perturbation of the Keplerian–Eulerian motion, using canonical variables associated with the total angular momentum. Parameters are introduced to visualize possibilities for different applications; nevertheless, we concentrate on the binary asteroid-type dynamics. Numerical experiments compare the two intermediaries with respect to the original model. Several values for attitude, shape, orbital eccentricity and distance are considered for systems with a slow-rotating axisymmetric rigid body in an eccentric relative orbit, i.e., with significant disturbing effects. In general, both models present good precision in wide regions of the dynamical parameters spaces defined.
publishDate 2019
dc.date.none.fl_str_mv 2019-10-06T15:45:01Z
2019-10-06T15:45:01Z
2019-06-01
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/10.1007/s10569-019-9900-x
Celestial Mechanics and Dynamical Astronomy, v. 131, n. 6, 2019.
1572-9478
0923-2958
http://hdl.handle.net/11449/187714
10.1007/s10569-019-9900-x
2-s2.0-85066791886
url http://dx.doi.org/10.1007/s10569-019-9900-x
http://hdl.handle.net/11449/187714
identifier_str_mv Celestial Mechanics and Dynamical Astronomy, v. 131, n. 6, 2019.
1572-9478
0923-2958
10.1007/s10569-019-9900-x
2-s2.0-85066791886
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv Celestial Mechanics and Dynamical Astronomy
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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