Real time orbit determination using GPS navigation solution

dc.contributorABCM
dc.contributorInstituto Nacional de Pesquisas Espaciais (INPE)
dc.contributorUniversidade Estadual Paulista (Unesp)
dc.date.accessioned2014-05-27T11:22:31Z
dc.date.accessioned2022-10-05T18:07:40Z
dc.date.available2014-05-27T11:22:31Z
dc.date.available2022-10-05T18:07:40Z
dc.date.created2014-05-27T11:22:31Z
dc.date.issued2007-07-01
dc.identifierJournal of the Brazilian Society of Mechanical Sciences and Engineering, v. 29, n. 3, p. 274-278, 2007.
dc.identifier1678-5878
dc.identifier1806-3691
dc.identifierhttp://hdl.handle.net/11449/69758
dc.identifier10.1590/S1678-58782007000300006
dc.identifierS1678-58782007000300006
dc.identifierWOS:000255403600006
dc.identifier2-s2.0-36248953364
dc.identifier2-s2.0-36248953364.pdf
dc.identifier.urihttp://repositorioslatinoamericanos.uchile.cl/handle/2250/3919152
dc.description.abstractThis work analyses a real time orbit estimator using the raw navigation solution provided by GPS receivers. The estimation algorithm considers a Kalman filter with a rather simple orbit dynamic model and random walk modeling of the receiver clock bias and drift. Using the Topex/Poseidon satellite as test bed, characteristics of model truncation, sampling rates and degradation of the GPS receiver (Selective Availability) were analysed. Copyright © 2007 by ABCM.
dc.languageeng
dc.relationJournal of the Brazilian Society of Mechanical Sciences and Engineering
dc.relation1.627
dc.relation0,362
dc.rightsAcesso aberto
dc.sourceScopus
dc.subjectGPS
dc.subjectKalman filter
dc.subjectNavigation solution
dc.subjectOrbit determination
dc.subjectModel truncation
dc.subjectOrbit estimator
dc.subjectAlgorithms
dc.subjectDynamic models
dc.subjectGlobal positioning system
dc.subjectKalman filters
dc.subjectReal time systems
dc.subjectSignal receivers
dc.subjectOrbits
dc.titleReal time orbit determination using GPS navigation solution
dc.typeArtigo


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