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dc.contributorGonzález Díez, David
dc.contributorSolé Busquet, Jaume
dc.contributor.authorTió Malo, Xavier
dc.contributor.otherUniversitat Politècnica de Catalunya. Departament d'Enginyeria Electrònica
dc.date.accessioned2020-05-04T12:14:20Z
dc.date.issued2017-06-10
dc.identifier.urihttp://hdl.handle.net/2117/186163
dc.description.abstractAiming to be the first step towards the design of a fully operational stabilization system for rockets, thebuilding of a model is done representing the attitudeof a rocket with anactive stability system. Several tests are done with the model both static and dynamic with different type of sensors that give us a view of the response of the system to different situations. Finally, it is described how the model could be upgradedand which steps follow to get a reliable stabilization system.
dc.language.isoeng
dc.publisherUniversitat Politècnica de Catalunya
dc.subjectÀrees temàtiques de la UPC::Enginyeria electrònica
dc.subject.lcshRocket engines
dc.titleStudy of a thrust vectoring system for rockets through a pressurized air test bench
dc.typeBachelor thesis
dc.subject.lemacCoets (Aeronàutica) -- Motors
dc.identifier.slug205-1107
dc.rights.accessRestricted access - author's decision
dc.date.lift10000-01-01
dc.date.updated2019-10-24T12:27:36Z
dc.audience.educationlevelGrau
dc.audience.mediatorEscola Superior d'Enginyeries Industrial, Aeroespacial i Audiovisual de Terrassa


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