Design and implementation of a VTOL flight transition mechanism and development of a mathematical model for a tilt rotor UAV

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 approach...

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Dettagli Bibliografici

Autore principale:	Paiva, Enrique (author)
Altri autori:	Llano, Marcelo (author), Rodas Benítez, Jorge Esteban (author), Gregor Recalde, Raúl Igmar (author), Rodríguez Piñeiro, José (author), Gómez, Marcos (author)
Natura:	article
Lingua:	inglese
Pubblicazione:	2018
Soggetti:	4. Transporte, telecomunicaciones y otras infraestructuras UNMANNED AERIAL VEHICLE (UAV) HYBRID UAV MATHEMATICAL MODEL TRI-ROTOR FIXED-WING VERTICAL TAKEOFF AND LANDING (VTOL) INGENIERIA
Accesso online:	http://hdl.handle.net/20.500.14066/3642
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