Analytical and semi-analytical analysis of an artificial satellite's rotational motion

Página do item simplificado
dc.contributor.authorZanardi, M. C.
dc.contributor.authorDe Moraes, R. V.
dc.contributor.institutionUniversidade Estadual Paulista (Unesp)
dc.date.accessioned2014-05-20T13:27:57Z
dc.date.available2014-05-20T13:27:57Z
dc.date.issued1999-01-01
dc.description.abstractThe rotational motion of an artificial satellite is studied by considering torques produced by gravity gradient and direct solar radiation pressure. A satellite of circular cylinder shape is considered here, and Andoyers variables are used to describe the rotational motion. Expressions for direct solar radiation torque are derived. When the earth's shadow is not considered, an analytical solution is obtained using Lagrange's method of variation of parameters. A semi-analytical procedure is proposed to predict the satellite's attitude under the influence of the earth's shadow. The analytical solution shows that angular variables are linear and periodic functions of time while their conjugates suffer only periodic variations. When compared, numerical and analytical solutions have a good agreement during the time range considered.en
dc.description.affiliationUNESP, Dept Math, Grp Dinam Orbital & Planetol, BR-12500000 Guaratingueta, SP, Brazil
dc.description.affiliationUnespUNESP, Dept Math, Grp Dinam Orbital & Planetol, BR-12500000 Guaratingueta, SP, Brazil
dc.format.extent227-250
dc.identifierhttp://dx.doi.org/10.1023/A:1008358801859
dc.identifier.citationCelestial Mechanics & Dynamical Astronomy. Dordrecht: Kluwer Academic Publ, v. 75, n. 4, p. 227-250, 1999.
dc.identifier.doi10.1023/A:1008358801859
dc.identifier.issn0923-2958
dc.identifier.lattes7740917144757410
dc.identifier.urihttp://hdl.handle.net/11449/9267
dc.identifier.wosWOS:000088220200001
dc.language.isoeng
dc.publisherKluwer Academic Publ
dc.relation.ispartofCelestial Mechanics & Dynamical Astronomy
dc.relation.ispartofjcr2.121
dc.relation.ispartofsjr1,092
dc.rights.accessRightsAcesso restrito
dc.sourceWeb of Science
dc.subjectrotational motionpt
dc.subjectsolar radiation torquept
dc.subjectAndoyer variablespt
dc.titleAnalytical and semi-analytical analysis of an artificial satellite's rotational motionen
dc.typeArtigo
dcterms.licensehttp://www.springer.com/open+access/authors+rights
dcterms.rightsHolderKluwer Academic Publ
unesp.author.lattes7740917144757410
unesp.campusUniversidade Estadual Paulista (Unesp), Faculdade de Engenharia, Guaratinguetápt
unesp.departmentMatemática - FEGpt

Arquivos

Licença do Pacote
Agora exibindo 1 - 1 de 1
Nenhuma Miniatura disponível
Nome:
license.txt
Tamanho:
1.71 KB
Formato:
Item-specific license agreed upon to submission
Descrição:

Coleções

Guaratinguetá - FEG - Faculdade de Engenharia e Ciências