15:1 Resonance effects on the orbital motion of artificial satellites
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Data de Publicação: | 2011 |
Outros Autores: | |
Tipo de documento: | Artigo |
Idioma: | eng |
Título da fonte: | Journal of Aerospace Technology and Management (Online) |
Texto Completo: | http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462011000300251 |
Resumo: | Abstract The motion of an artificial satellite is studied considering geopotential perturbations and resonances between the frequencies of the mean orbital motion and the Earth rotational motion. The behavior of the satellite motion is analyzed in the neighborhood of the resonances 15:1. A suitable sequence of canonical transformations reduces the system of differential equations describing the orbital motion to an integrable kernel. The phase space of the resulting system is studied taking into account that one resonant angle is fixed. Simulations are presented showing the variations of the semi-major axis of artificial satellites due to the resonance effects. |
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Journal of Aerospace Technology and Management (Online) |
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15:1 Resonance effects on the orbital motion of artificial satellitesResonanceArtificial satellitesCelestial mechanicsAbstract The motion of an artificial satellite is studied considering geopotential perturbations and resonances between the frequencies of the mean orbital motion and the Earth rotational motion. The behavior of the satellite motion is analyzed in the neighborhood of the resonances 15:1. A suitable sequence of canonical transformations reduces the system of differential equations describing the orbital motion to an integrable kernel. The phase space of the resulting system is studied taking into account that one resonant angle is fixed. Simulations are presented showing the variations of the semi-major axis of artificial satellites due to the resonance effects.Departamento de Ciência e Tecnologia Aeroespacial2011-12-01info:eu-repo/semantics/articleinfo:eu-repo/semantics/publishedVersiontext/htmlhttp://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462011000300251Journal of Aerospace Technology and Management v.3 n.3 2011reponame:Journal of Aerospace Technology and Management (Online)instname:Departamento de Ciência e Tecnologia Aeroespacial (DCTA)instacron:DCTA10.5028/jatm.2011.03032011info:eu-repo/semantics/openAccessFormiga,Jorge Kennety S.Moraes,Rodolpho Vilhena deeng2017-05-18T00:00:00Zoai:scielo:S2175-91462011000300251Revistahttp://www.jatm.com.br/ONGhttps://old.scielo.br/oai/scielo-oai.php||secretary@jatm.com.br2175-91461984-9648opendoar:2017-05-18T00:00Journal of Aerospace Technology and Management (Online) - Departamento de Ciência e Tecnologia Aeroespacial (DCTA)false |
dc.title.none.fl_str_mv |
15:1 Resonance effects on the orbital motion of artificial satellites |
title |
15:1 Resonance effects on the orbital motion of artificial satellites |
spellingShingle |
15:1 Resonance effects on the orbital motion of artificial satellites Formiga,Jorge Kennety S. Resonance Artificial satellites Celestial mechanics |
title_short |
15:1 Resonance effects on the orbital motion of artificial satellites |
title_full |
15:1 Resonance effects on the orbital motion of artificial satellites |
title_fullStr |
15:1 Resonance effects on the orbital motion of artificial satellites |
title_full_unstemmed |
15:1 Resonance effects on the orbital motion of artificial satellites |
title_sort |
15:1 Resonance effects on the orbital motion of artificial satellites |
author |
Formiga,Jorge Kennety S. |
author_facet |
Formiga,Jorge Kennety S. Moraes,Rodolpho Vilhena de |
author_role |
author |
author2 |
Moraes,Rodolpho Vilhena de |
author2_role |
author |
dc.contributor.author.fl_str_mv |
Formiga,Jorge Kennety S. Moraes,Rodolpho Vilhena de |
dc.subject.por.fl_str_mv |
Resonance Artificial satellites Celestial mechanics |
topic |
Resonance Artificial satellites Celestial mechanics |
description |
Abstract The motion of an artificial satellite is studied considering geopotential perturbations and resonances between the frequencies of the mean orbital motion and the Earth rotational motion. The behavior of the satellite motion is analyzed in the neighborhood of the resonances 15:1. A suitable sequence of canonical transformations reduces the system of differential equations describing the orbital motion to an integrable kernel. The phase space of the resulting system is studied taking into account that one resonant angle is fixed. Simulations are presented showing the variations of the semi-major axis of artificial satellites due to the resonance effects. |
publishDate |
2011 |
dc.date.none.fl_str_mv |
2011-12-01 |
dc.type.driver.fl_str_mv |
info:eu-repo/semantics/article |
dc.type.status.fl_str_mv |
info:eu-repo/semantics/publishedVersion |
format |
article |
status_str |
publishedVersion |
dc.identifier.uri.fl_str_mv |
http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462011000300251 |
url |
http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462011000300251 |
dc.language.iso.fl_str_mv |
eng |
language |
eng |
dc.relation.none.fl_str_mv |
10.5028/jatm.2011.03032011 |
dc.rights.driver.fl_str_mv |
info:eu-repo/semantics/openAccess |
eu_rights_str_mv |
openAccess |
dc.format.none.fl_str_mv |
text/html |
dc.publisher.none.fl_str_mv |
Departamento de Ciência e Tecnologia Aeroespacial |
publisher.none.fl_str_mv |
Departamento de Ciência e Tecnologia Aeroespacial |
dc.source.none.fl_str_mv |
Journal of Aerospace Technology and Management v.3 n.3 2011 reponame:Journal of Aerospace Technology and Management (Online) instname:Departamento de Ciência e Tecnologia Aeroespacial (DCTA) instacron:DCTA |
instname_str |
Departamento de Ciência e Tecnologia Aeroespacial (DCTA) |
instacron_str |
DCTA |
institution |
DCTA |
reponame_str |
Journal of Aerospace Technology and Management (Online) |
collection |
Journal of Aerospace Technology and Management (Online) |
repository.name.fl_str_mv |
Journal of Aerospace Technology and Management (Online) - Departamento de Ciência e Tecnologia Aeroespacial (DCTA) |
repository.mail.fl_str_mv |
||secretary@jatm.com.br |
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1754732530473369600 |