Application of the GPS system for preliminary satellite orbit determination

dc.contributor.authorChiaradia, A. P M
dc.contributor.authorDa Silva Fernandes, S.
dc.contributor.authorVilhena de Moraes, R. [UNESP]
dc.contributor.institutionCTA
dc.contributor.institutionUniversidade Estadual Paulista (Unesp)
dc.date.accessioned2014-05-27T11:18:17Z
dc.date.available2014-05-27T11:18:17Z
dc.date.issued1997-12-01
dc.description.abstractIn this paper, we discuss a method of preliminary orbit determination for an artificial satellite based on the navigation message of the GPS constellation. Orbital elements are considered as state variables and a simple dynamic model, based on the classic two-body problem, is used. The observations are formed by range and range and range-rate with respect to four visible GPS. A discrete Kalman filter with simulated data is used as filtering technique. The data are obtained through numerical propagation (Cowell's method), which considers special perturbations for the GPS satellite constellation and a user satellite. © 1997 COSPAR. Published by Elsevier Science Ltd.en
dc.description.affiliationInst. Tecn. de Aeronáutica CTA, 12228-300, Sao Jose dos Campos, SP
dc.description.affiliationGrupo Dynamica Orbital Planetologia DMA-FEG-UNESP, 12500-000 Guaratinguetá, SP
dc.description.affiliationUnespGrupo Dynamica Orbital Planetologia DMA-FEG-UNESP, 12500-000 Guaratinguetá, SP
dc.format.extent1671-1675
dc.identifierhttp://dx.doi.org/10.1016/S0273-1177(97)00322-0
dc.identifier.citationAdvances in Space Research, v. 19, n. 11, p. 1671-1675, 1997.
dc.identifier.doi10.1016/S0273-1177(97)00322-0
dc.identifier.issn0273-1177
dc.identifier.lattes5651353474953307
dc.identifier.scopus2-s2.0-0031445722
dc.identifier.urihttp://hdl.handle.net/11449/65249
dc.identifier.wosWOS:A1997BJ16E00007
dc.language.isoeng
dc.relation.ispartofAdvances in Space Research
dc.relation.ispartofjcr1.529
dc.relation.ispartofsjr0,569
dc.rights.accessRightsAcesso restrito
dc.sourceScopus
dc.subjectGPS
dc.subjectorbit determination
dc.subjectsatellite system
dc.titleApplication of the GPS system for preliminary satellite orbit determinationen
dc.typeArtigo
dcterms.licensehttp://www.elsevier.com/about/open-access/open-access-policies/article-posting-policy
unesp.author.lattes5651353474953307[1]
unesp.author.orcid0000-0002-7941-8666[1]
unesp.campusUniversidade Estadual Paulista (Unesp), Faculdade de Engenharia, Guaratinguetápt

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