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dc.contributor.authorMarchante Arjona, Luis
dc.date.accessioned2018-11-16T09:53:04Z
dc.date.available2018-11-16T09:53:04Z
dc.date.issued2018-09-10
dc.identifier.urihttp://hdl.handle.net/10481/53798
dc.description.abstractThis Bachelor Thesis introduces a Theoretical Description and Simulink implementation of di erent ADCS (Attitude Determination and Control System), a fundamental feature of spacecrafts. As it makes possible to control the orientation and stabilize the satellite within its orbit. Which is as complex as fascinating. Mathematical Formalism and Physical Model are presented in order to fully understand this phenomenon and build it to make it work in Simulink, creating a simulation of a Digital Dynamical System that would be present at the on board computer of the satellite GranaSAT-I. In this context, the Aerospace GranaSAT Group at UGR is building the GranaSAT-I.es_ES
dc.language.isoenges_ES
dc.publisherProf. Andrés Roldán Arandaes_ES
dc.rightsAtribución-NoComercial-SinDerivadas 3.0 España*
dc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/3.0/es/*
dc.subjectGranaSATes_ES
dc.subjectADCSes_ES
dc.subjectsimulinkes_ES
dc.titleGranaSAT-I: Kinematic and Dynamic Model for Attitude Determination and Control Systemes_ES
dc.typeinfo:eu-repo/semantics/bachelorThesises_ES
dc.rights.accessRightsinfo:eu-repo/semantics/openAccesses_ES


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Atribución-NoComercial-SinDerivadas 3.0 España
Except where otherwise noted, this item's license is described as Atribución-NoComercial-SinDerivadas 3.0 España