A Discussion Related to Orbit Determination Using Nonlinear Sigma Point Kalman Filter

dc.contributorUniversidade Estadual Paulista (UNESP)
dc.creatorPinto Mesquita Pardal, Paula Cristiane
dc.creatorKuga, Helio Koiti
dc.creatorde Moraes, Rodolpho Vilhena
dc.date2014-05-20T13:28:00Z
dc.date2014-05-20T13:28:00Z
dc.date2009-01-01
dc.date.accessioned2017-04-05T20:10:13Z
dc.date.available2017-04-05T20:10:13Z
dc.identifierMathematical Problems In Engineering. New York: Hindawi Publishing Corporation, p. 12, 2009.
dc.identifier1024-123X
dc.identifierhttp://hdl.handle.net/11449/9293
dc.identifier10.1155/2009/140963
dc.identifierWOS:000276145500001
dc.identifierWOS000276145500001.pdf
dc.identifierhttp://dx.doi.org/10.1155/2009/140963
dc.identifier.urihttp://repositorioslatinoamericanos.uchile.cl/handle/2250/857472
dc.descriptionHerein, the purpose is to present a Kalman filter based on the sigma point unscented transformation development, aiming at real-time satellite orbit determination using GPS measurements. First, a brief review of the extended Kalman filter will be done. After, the sigma point Kalman filter will be introduced as well as the basic idea of the unscented transformation, in which this filter is based. Following, the unscented Kalman filter applied to orbit determination will be explained. Such explanation encloses formulations about the orbit determination through GPS; the dynamic model; the observation model; the unmodeled acceleration estimation; also an application of this new filter approaches on orbit determination using GPS measurements discussion. Copyright (C) 2009 Paula Cristiane Pinto Mesquita Pardal et al.
dc.descriptionFundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP)
dc.languageeng
dc.publisherHindawi Publishing Corporation
dc.relationMathematical Problems in Engineering
dc.rightsinfo:eu-repo/semantics/openAccess
dc.titleA Discussion Related to Orbit Determination Using Nonlinear Sigma Point Kalman Filter
dc.typeOtro


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