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dc.contributor.advisorRoldán Aranda, Andrés María es_ES
dc.contributor.authorAguilera Jiménez, Davides_ES
dc.contributor.otherUniversidad de Granada. Departamento de Electrónica y Tecnología de los Computadoreses_ES
dc.date.accessioned2017-11-14T07:21:59Z
dc.date.available2017-11-14T07:21:59Z
dc.date.issued2017-11-14
dc.date.submitted2015-09-15
dc.identifier.urihttp://hdl.handle.net/10481/48127
dc.description.abstractThis Thesis presents the design of a ground segment for the GranaSAT-I cubesat, a microsatellite in development process which will require of a system capable of receiving its telemetry and sending telecommands when it is launched. The project includes an analysis of all the physical phenomena and components involved in the transmission of the signal from an spacecraft in Low Earth Orbit to the station located in the Faculty of Sciences of the University of Granada. The deployment and testing processes were also carried out and are described in detail.en_EN
dc.description.sponsorshipProyecto Fin de Carrera de la Univ. de Granada. Departamento de Electrónica y Tecnología de Computadores. Curso 2014-2015es_ES
dc.language.isoengen
dc.subjectGranaSATen_EN
dc.subjectCubeSaten_EN
dc.subjectGround Stationen_EN
dc.subjectGround segmenten_EN
dc.subjectMicrosatelliteen_EN
dc.subjectLink budgeten_EN
dc.subjectRadiolinken_EN
dc.subjectAtmospheric attenuationen_EN
dc.subjectOrbit mechanicsen_EN
dc.titleGround segment design and deployment for GranaSAT-Ien_EN
dc.typeinfo:eu-repo/semantics/bachelorThesises_ES


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