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dc.contributorPérez Batlle, Marcos
dc.contributor.authorMarcos Benitez, Monica
dc.date.accessioned2017-08-29T11:36:15Z
dc.date.available2017-08-29T11:36:15Z
dc.date.issued2016-09-13
dc.identifier.urihttp://hdl.handle.net/2117/107241
dc.description.abstractIn this project the vortex affectation generated by a commercial airliner to a RPAS (Remotely Piloted Aircraft Systems) when both are at enroute phase is studied. The objective is to perform a vortex detection system that allows the RPAS to know if it can fly through its assigned route with no risks, or if it will have to modify it as a consequence of the vortex existence generated by the commercial airliner, producing a hazard situation, where the RPAS could turned upside down and therefore, to have an accident or produce another one. To execute it, a vortex model will be performed, which will be used at the collision model. Furthermore, there will be two collision models. One will consider the airliner flying in a straight line, and the other one will take into account that the commercial aircraft can make turns in order to change its heading.
dc.language.isoeng
dc.publisherUniversitat Politècnica de Catalunya
dc.rights.urihttp://creativecommons.org/licenses/by-nc-sa/3.0/es/
dc.subjectÀrees temàtiques de la UPC::Aeronàutica i espai::Navegació aèria::Procediments operacionals
dc.subject.lcshNavigation (Aeronautics)
dc.subject.otherEnroute vortex
dc.subject.otherRPAS
dc.subject.otherSeparation management
dc.titleEnroute vortex conflict detection system for RPAS operations
dc.typeBachelor thesis
dc.subject.lemacNavegació aèria
dc.rights.accessOpen Access
dc.date.updated2016-09-14T06:48:41Z
dc.audience.educationlevelEstudis de primer/segon cicle
dc.audience.mediatorEscola d'Enginyeria de Telecomunicació i Aeroespacial de Castelldefels
dc.audience.degreeGRAU EN ENGINYERIA D'AERONAVEGACIÓ (Pla 2010)


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