Analytical prediction of the spin stabilized satellite's attitude using the solar radiation torque
Autor(a) principal: | |
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Data de Publicação: | 2013 |
Outros Autores: | , |
Tipo de documento: | Artigo de conferência |
Idioma: | eng |
Título da fonte: | Repositório Institucional da UNESP |
Texto Completo: | http://dx.doi.org/10.1088/1742-6596/465/1/012009 http://hdl.handle.net/11449/111527 |
Resumo: | The aim of this paper is to present an analytical solution for the spin motion equations of spin-stabilized satellite considering only the influence of solar radiation torque. The theory uses a cylindrical satellite on a circular orbit and considers that the satellite is always illuminated. The average components of this torque were determined over an orbital period. These components are substituted in the spin motion equations in order to get an analytical solution for the right ascension and declination of the satellite spin axis. The time evolution for the pointing deviation of the spin axis was also analyzed. These solutions were numerically implemented and compared with real data of the Brazilian Satellite of Data Collection - SCD1 an SCD2. The results show that the theory has consistency and can be applied to predict the spin motion of spin-stabilized artificial satellites. |
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Repositório Institucional da UNESP |
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Analytical prediction of the spin stabilized satellite's attitude using the solar radiation torqueThe aim of this paper is to present an analytical solution for the spin motion equations of spin-stabilized satellite considering only the influence of solar radiation torque. The theory uses a cylindrical satellite on a circular orbit and considers that the satellite is always illuminated. The average components of this torque were determined over an orbital period. These components are substituted in the spin motion equations in order to get an analytical solution for the right ascension and declination of the satellite spin axis. The time evolution for the pointing deviation of the spin axis was also analyzed. These solutions were numerically implemented and compared with real data of the Brazilian Satellite of Data Collection - SCD1 an SCD2. The results show that the theory has consistency and can be applied to predict the spin motion of spin-stabilized artificial satellites.Sao Paulo State Univ, Grp Orbital Dynam & Planetol, Sao Paulo, BrazilSao Paulo State Univ, Grp Orbital Dynam & Planetol, Sao Paulo, BrazilIop Publishing LtdUniversidade Estadual Paulista (Unesp)Motta, Gabriel Borderes [UNESP]Carvalho, Marlon do Vale [UNESP]Zanardi, Maria Cecília Franca de Paula Santos [UNESP]2014-12-03T13:08:44Z2014-12-03T13:08:44Z2013-01-01info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/conferenceObject6application/pdfhttp://dx.doi.org/10.1088/1742-6596/465/1/012009Xvi Brazilian Colloquium On Orbital Dynamics. Bristol: Iop Publishing Ltd, v. 465, 6 p., 2013.1742-6588http://hdl.handle.net/11449/11152710.1088/1742-6596/465/1/012009WOS:000326877000009WOS000326877000009.pdf16862025940202237120496490032539Web of Sciencereponame:Repositório Institucional da UNESPinstname:Universidade Estadual Paulista (UNESP)instacron:UNESPengXvi Brazilian Colloquium On Orbital Dynamics0,241info:eu-repo/semantics/openAccess2024-07-02T14:29:48Zoai:repositorio.unesp.br:11449/111527Repositório InstitucionalPUBhttp://repositorio.unesp.br/oai/requestopendoar:29462024-08-05T17:51:01.763564Repositório Institucional da UNESP - Universidade Estadual Paulista (UNESP)false |
dc.title.none.fl_str_mv |
Analytical prediction of the spin stabilized satellite's attitude using the solar radiation torque |
title |
Analytical prediction of the spin stabilized satellite's attitude using the solar radiation torque |
spellingShingle |
Analytical prediction of the spin stabilized satellite's attitude using the solar radiation torque Motta, Gabriel Borderes [UNESP] |
title_short |
Analytical prediction of the spin stabilized satellite's attitude using the solar radiation torque |
title_full |
Analytical prediction of the spin stabilized satellite's attitude using the solar radiation torque |
title_fullStr |
Analytical prediction of the spin stabilized satellite's attitude using the solar radiation torque |
title_full_unstemmed |
Analytical prediction of the spin stabilized satellite's attitude using the solar radiation torque |
title_sort |
Analytical prediction of the spin stabilized satellite's attitude using the solar radiation torque |
author |
Motta, Gabriel Borderes [UNESP] |
author_facet |
Motta, Gabriel Borderes [UNESP] Carvalho, Marlon do Vale [UNESP] Zanardi, Maria Cecília Franca de Paula Santos [UNESP] |
author_role |
author |
author2 |
Carvalho, Marlon do Vale [UNESP] Zanardi, Maria Cecília Franca de Paula Santos [UNESP] |
author2_role |
author author |
dc.contributor.none.fl_str_mv |
Universidade Estadual Paulista (Unesp) |
dc.contributor.author.fl_str_mv |
Motta, Gabriel Borderes [UNESP] Carvalho, Marlon do Vale [UNESP] Zanardi, Maria Cecília Franca de Paula Santos [UNESP] |
description |
The aim of this paper is to present an analytical solution for the spin motion equations of spin-stabilized satellite considering only the influence of solar radiation torque. The theory uses a cylindrical satellite on a circular orbit and considers that the satellite is always illuminated. The average components of this torque were determined over an orbital period. These components are substituted in the spin motion equations in order to get an analytical solution for the right ascension and declination of the satellite spin axis. The time evolution for the pointing deviation of the spin axis was also analyzed. These solutions were numerically implemented and compared with real data of the Brazilian Satellite of Data Collection - SCD1 an SCD2. The results show that the theory has consistency and can be applied to predict the spin motion of spin-stabilized artificial satellites. |
publishDate |
2013 |
dc.date.none.fl_str_mv |
2013-01-01 2014-12-03T13:08:44Z 2014-12-03T13:08:44Z |
dc.type.status.fl_str_mv |
info:eu-repo/semantics/publishedVersion |
dc.type.driver.fl_str_mv |
info:eu-repo/semantics/conferenceObject |
format |
conferenceObject |
status_str |
publishedVersion |
dc.identifier.uri.fl_str_mv |
http://dx.doi.org/10.1088/1742-6596/465/1/012009 Xvi Brazilian Colloquium On Orbital Dynamics. Bristol: Iop Publishing Ltd, v. 465, 6 p., 2013. 1742-6588 http://hdl.handle.net/11449/111527 10.1088/1742-6596/465/1/012009 WOS:000326877000009 WOS000326877000009.pdf 1686202594020223 7120496490032539 |
url |
http://dx.doi.org/10.1088/1742-6596/465/1/012009 http://hdl.handle.net/11449/111527 |
identifier_str_mv |
Xvi Brazilian Colloquium On Orbital Dynamics. Bristol: Iop Publishing Ltd, v. 465, 6 p., 2013. 1742-6588 10.1088/1742-6596/465/1/012009 WOS:000326877000009 WOS000326877000009.pdf 1686202594020223 7120496490032539 |
dc.language.iso.fl_str_mv |
eng |
language |
eng |
dc.relation.none.fl_str_mv |
Xvi Brazilian Colloquium On Orbital Dynamics 0,241 |
dc.rights.driver.fl_str_mv |
info:eu-repo/semantics/openAccess |
eu_rights_str_mv |
openAccess |
dc.format.none.fl_str_mv |
6 application/pdf |
dc.publisher.none.fl_str_mv |
Iop Publishing Ltd |
publisher.none.fl_str_mv |
Iop Publishing Ltd |
dc.source.none.fl_str_mv |
Web of Science 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_ |
1808128866715172864 |