| dc.contributor.author | Paiva, Enrique | |
| dc.contributor.author | Llano, Marcelo | |
| dc.contributor.author | Rodas Benítez, Jorge Esteban | |
| dc.contributor.author | Gregor Recalde, Raúl Igmar | |
| dc.contributor.author | Rodríguez Piñeiro, José | |
| dc.contributor.author | Gómez, Marcos | |
| dc.contributor.other | Universidad Nacional de Asunción - Facultad de Ingeniería | es |
| dc.date.accessioned | 2022-04-25T22:41:20Z | |
| dc.date.available | 2022-04-25T22:41:20Z | |
| dc.date.issued | 2018 | |
| dc.identifier.uri | http://hdl.handle.net/20.500.14066/3642 | |
| dc.description.abstract | In the last decade, the interest in the development of unmanned aerial vehicles and the implementation of different flight topologies have been justified mainly by a wide range of applications, both military and civil. The current work can be used for educational purposes and we present two approaches in this area. | es |
| dc.description.sponsorship | Consejo Nacional de Ciencia y Tecnología | es |
| dc.language.iso | eng | es |
| dc.subject.classification | 4. Transporte, telecomunicaciones y otras infraestructuras | es |
| dc.subject.other | UNMANNED AERIAL VEHICLE (UAV) | es |
| dc.subject.other | HYBRID UAV MATHEMATICAL MODEL | es |
| dc.subject.other | TRI-ROTOR | es |
| dc.subject.other | FIXED-WING | es |
| dc.subject.other | VERTICAL TAKEOFF AND LANDING (VTOL) | es |
| dc.title | Design and implementation of a VTOL flight transition mechanism and development of a mathematical model for a tilt rotor UAV | es |
| dc.type | info:eu-repo/semantics/article | es |
| dc.type | info:eu-repo/semantics/publishedVersion | es |
| dc.description.fundingtext | PROCIENCIA | es |
| dc.relation.projectCONACYT | PINV15-136 | es |
| dc.rights.accessRights | info:eu-repo/semantics/openAccess | es |
| dc.subject.ocde | INGENIERIA | es |
