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dc.contributorTristancho Martínez, Joshua
dc.contributor.authorPadilla Hernandez, Aymon
dc.description.abstractThis work should be understood as the challenge of integrating different technologies that have a strong boom in the aeronautics field. The aim is to perform a micro air vehicle, where the entire structure consists of a single wing built by inflatable structure. This prototype will be an unmanned vehicle capable of vertical takeoff and landing as if it were a helicopter. We must solve various technological problems arising from constructing and manipulating inflatable structures within the micro air vehicle category and keep it running efficiently as helicopter and flying wing according to a list of limitations agreed with the customer. The weight that is able to support in every phase of flight will be a significant aspect to optimize. This challenge will be faced by studying the technologies available to meet every need, we will establish a requirements and consider various implementation solutions backed into simulations and experimental assays to become compliant as many requirements as possible. In case of non-meet any of them, solutions and future work to be done will be indicated.
dc.publisherUniversitat Politècnica de Catalunya
dc.subjectÀrees temàtiques de la UPC::Aeronàutica i espai::Aeronaus
dc.subject.otherMicro-Air Vehicle
dc.subject.otherFlying wing
dc.subject.otherInflatable structure
dc.subject.otherVertical Take-Off/Landing
dc.titleUn micro-vehicle aeri no tripulat tipus ala volant inflable amb capacitat de enlairament/aterratge vertical
dc.typeMaster thesis (pre-Bologna period)
dc.subject.lemacAeronàutica -- Construcció
dc.rights.accessRestricted access - author's decision
dc.audience.educationlevelEstudis de primer/segon cicle
dc.audience.mediatorEscola d'Enginyeria de Telecomunicació i Aeroespacial de Castelldefels

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