You are in the accessibility menu

Please use this identifier to cite or link to this item: http://acervodigital.unesp.br/handle/11449/9313
Full metadata record
DC FieldValueLanguage
dc.contributor.authorCelestino, Claudia C.-
dc.contributor.authorSousa, Cristina T.-
dc.contributor.authorYamaguti, Wilson-
dc.contributor.authorKuga, Helio Koiti-
dc.date.accessioned2014-05-20T13:28:06Z-
dc.date.available2014-05-20T13:28:06Z-
dc.date.issued2009-01-01-
dc.identifierhttp://dx.doi.org/10.1155/2009/856138-
dc.identifier.citationMathematical Problems In Engineering. New York: Hindawi Publishing Corporation, p. 9, 2009.-
dc.identifier.issn1024-123X-
dc.identifier.urihttp://hdl.handle.net/11449/9313-
dc.description.abstractThe current Brazilian System of Environmental Data Collection is composed of several satellites (SCD-1 and 2, CBERS-2 and 2B), Data Collection Platforms (DCPs) spread mostly over the Brazilian territory, and ground reception stations located in Cuiaba and Alcantara. An essential functionality offered to the users is the geographic location of these DCPs. The location is computed by the in-house developed GEOLOC program which processes the onboard measured Doppler shifts suffered by the signal transmitted by the DCPs. These data are relayed and stored on ground when the satellite passes over the receiving stations. Another important input data to GEOLOC are the orbit ephemeris of the satellite corresponding to the Doppler data. In this work, the impact on the geographic location accuracy when using orbit ephemeris which can be obtained through several sources is assessed. First, this evaluation is performed by computer simulation of the Doppler data, corresponding to real existing satellite passes. Then real Doppler data are used to assess the performance of the location system. The results indicate that the use of precise ephemeris can improve the performance of GEOLOC by reducing the location errors, and such conclusion can then be extended to similar location systems. Copyright (C) 2009 Claudia C. Celestino et al.en
dc.description.sponsorshipConselho Nacional de Desenvolvimento Científico e Tecnológico (CNPq)-
dc.description.sponsorshipFundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP)-
dc.format.extent9-
dc.language.isoeng-
dc.publisherHindawi Publishing Corporation-
dc.sourceWeb of Science-
dc.titleThe Impact on Geographic Location Accuracy due to Different Satellite Orbit Ephemeridesen
dc.typeoutro-
dc.contributor.institutionInstituto Nacional de Pesquisas Espaciais (INPE)-
dc.contributor.institutionUniversidade Estadual Paulista (UNESP)-
dc.description.affiliationINPE, Space Mech & Control Div DMC, BR-12227010 Sao Jose Dos Campos, SP, Brazil-
dc.description.affiliationINPE, Space Syst Div DSE, BR-12227010 Sao Jose Dos Campos, SP, Brazil-
dc.description.affiliationUniv São Paulo State UNESP FEG, Math Dept DMA, BR-12516410 Guaratingueta, SP, Brazil-
dc.description.affiliationUnespUniv São Paulo State UNESP FEG, Math Dept DMA, BR-12516410 Guaratingueta, SP, Brazil-
dc.description.sponsorshipIdCNPq: 382746/2005-8-
dc.description.sponsorshipIdFAPESP: 05/04497-0-
dc.identifier.doi10.1155/2009/856138-
dc.identifier.wosWOS:000274900000001-
dc.rights.accessRightsAcesso aberto-
dc.identifier.fileWOS000274900000001.pdf-
dc.relation.ispartofMathematical Problems in Engineering-
Appears in Collections:Artigos, TCCs, Teses e Dissertações da Unesp

There are no files associated with this item.
 

Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.