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Development of a Dual Axis Tilt Rotorcraft UAV: Modelling, Simulation and Control

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Development of a Dual Axis Tilt Rotorcraft UAV: Modelling, Simulation and Control

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Seguí Gascó, P. (2012). Development of a Dual Axis Tilt Rotorcraft UAV: Modelling, Simulation and Control. http://hdl.handle.net/10251/38205.

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Title: Development of a Dual Axis Tilt Rotorcraft UAV: Modelling, Simulation and Control
Author: Seguí Gascó, Pau
Director(s): Al Savvaris Hyo-Sang Shin
UPV Unit: Universitat Politècnica de València. Escuela Técnica Superior de Ingeniería del Diseño - Escola Tècnica Superior d'Enginyeria del Disseny
Read date / Event date:
2012
Issued date:
Abstract:
This thesis stems from a project to design a novel dual axis tilt quadrotor that uses gyroscopic effects to explore an increase in the performance with respect to a conventionally actuated quadrotor. The project is ...[+]
Subjects: Hélices , MAV , UAV , Quadrotor Design , Gyroscopic Actuation , Overactuated , Novel Actuator , Propellers , Giroscopio , Gyroscopes
Copyrigths: Reserva de todos los derechos
Publisher:
Universitat Politècnica de València
degree: Grado en Ingeniería Aeroespacial-Grau en Enginyeria Aeroespacial
Type: Proyecto/Trabajo fin de carrera/grado

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