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dc.contributorPalà Schönwälder, Pere
dc.contributor.authorRivero Prat, Marc
dc.contributor.otherUniversitat Politècnica de Catalunya. Departament de Disseny i Programació de Sistemes Electrònics
dc.date.accessioned2015-11-19T08:35:45Z
dc.date.available2015-11-19T08:35:45Z
dc.date.issued2015-07
dc.identifier.urihttp://hdl.handle.net/2117/79458
dc.description.abstractThe objective of this project, is to develop a system for deploying a parachute in order to save the integrity of various flying widgets. This project was developed having in mind the idea of saving a drone. This goal wants to be achieved using the information given by a barometrical sensor. The project itself starts explaining the physics behind the movement of the whole parachute. It talks about the different forces acting on the body, like the speed and acceleration achieved during the free fall, before and after deploying the parachute. Then the shape of the parachute is also studied in order to obtaining the biggest drag force possible for going against the gravity force. The time of opening is also important so it will be explained. the next part explains the device that makes the deployment of the parachute be possible, explaining all of the parts of this device. This parts are: the barometric sensor, the EEPROM memory and the Arduino Nano among others. One of the most important parts for making this possible, is the software. The software allows to the different parts of the project work together. It is explained how the software works for achieving our primary goal: save the flying device attached to it. This project, also explains some issues that occurred during the assembly of the different electronic components and how a printed circuit board can help on it. It also explain how to build one. One of the last parts explained in the project is the assembly of the whole project, starting from the assembly of the mechanical parts up to the assembly of the electronic parts. For ending the project, an experiment proving the efficiency of the parachute is done dropping the parachute from a high position in order to see if the parachute is deployed or not. The last part of the project are the conclusions achieved during the realisation of the project, and the thanks to the people that has contributed on the project
dc.language.isocat
dc.publisherUniversitat Politècnica de Catalunya
dc.subjectÀrees temàtiques de la UPC::Informàtica::Automàtica i control
dc.subject.lcshFlight control
dc.subject.lcshParachutes
dc.subject.lcshDrone aircraft--Automatic control
dc.subject.lcshAtmospheric pressure--Measurement
dc.subject.otherGiny volador
dc.subject.otherParacaigudes
dc.subject.otherSensor baromètric
dc.titleSistema de paracaigudes per a ginys voladors
dc.typeBachelor thesis
dc.subject.lemacSistemes de control (Vol)
dc.subject.lemacParacaigudes
dc.subject.lemacAvions no tripulats
dc.subject.lemacBaròmetres
dc.rights.accessOpen Access
dc.audience.educationlevelGrau
dc.audience.mediatorEscola Politècnica Superior d'Enginyeria de Manresa
dc.audience.degreeGRAU EN ENGINYERIA DE SISTEMES TIC (Pla 2010)


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