Study of the roto-orbital motion using intermediaries: numerical experiments
Autor(a) principal: | |
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Data de Publicação: | 2019 |
Outros Autores: | , |
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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Repositório Institucional da UNESP |
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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 |
|
_version_ |
1808129331770163200 |