The work presented here covers the detailed modelling and trajectory control for an elastic bladed quadrotor vehicle. The benefits of using VehicleSim modelling software are also discussed. The authors present a full elastic structural and dynamical model as well as two different aerodynamic models. These two aerodynamic models differ from each other on their level of complexity and therefore, accuracy. The control methodology employed to stabilize and guide the vehicle is PVA (ProportionalVelocity-Acceleration), derived and implemented by using Simulink. As it will be shown, it stabilises and provides satisfactory quadrotor trajectory tracking. Since the control methodology feeds back the acceleration of the vehicle, and this acceleration ...
This research investigates and demonstrates the fundamental differences in performance and operation...
International audienceIn this paper, an adaptive trajectory tracking controller for quadrotor MAVs i...
In this thesis is studied the landing problem of a VTOL UAV and a 3D sim-ulation environment is buil...
[EN] In this work the authors present the modelling of a quadrotor as a multibody system carried out...
In this work, a novel structure of a Quadrotor Unmanned Aerial Vehicle (UAV) is proposed to change t...
Since there has been an important increase in unmanned vehicles systems research such as quadrotors,...
Unmanned aerial vehicles (UAVs) are now becoming a major topic of interest due to their flying capab...
This work describes a model developed to analyze the aerodynamic loads on a helicopter model on conv...
This document contains the details of the thesis titled Study and suppression of vibrations in rotar...
Quadrotors are aerial vehicles with a four motor-rotor assembly for generating lift and control...
This paper presents modelling, simulation and implementation of a quadrotor Unmanned Arial Vehicle (...
Mathematical model of an unmanned aerial vehicle with four propulsors (quadcopter) is indispensable ...
This thesis presents contributions to the state-of-the-art in quadrotor control, payload transportat...
Quadrotor control is an exciting research area. Despite last years developments, some aspects demand...
this paper presents the modelling of a four rotor vertical take-off and landing (VTOL) unmanned air ...
This research investigates and demonstrates the fundamental differences in performance and operation...
International audienceIn this paper, an adaptive trajectory tracking controller for quadrotor MAVs i...
In this thesis is studied the landing problem of a VTOL UAV and a 3D sim-ulation environment is buil...
[EN] In this work the authors present the modelling of a quadrotor as a multibody system carried out...
In this work, a novel structure of a Quadrotor Unmanned Aerial Vehicle (UAV) is proposed to change t...
Since there has been an important increase in unmanned vehicles systems research such as quadrotors,...
Unmanned aerial vehicles (UAVs) are now becoming a major topic of interest due to their flying capab...
This work describes a model developed to analyze the aerodynamic loads on a helicopter model on conv...
This document contains the details of the thesis titled Study and suppression of vibrations in rotar...
Quadrotors are aerial vehicles with a four motor-rotor assembly for generating lift and control...
This paper presents modelling, simulation and implementation of a quadrotor Unmanned Arial Vehicle (...
Mathematical model of an unmanned aerial vehicle with four propulsors (quadcopter) is indispensable ...
This thesis presents contributions to the state-of-the-art in quadrotor control, payload transportat...
Quadrotor control is an exciting research area. Despite last years developments, some aspects demand...
this paper presents the modelling of a four rotor vertical take-off and landing (VTOL) unmanned air ...
This research investigates and demonstrates the fundamental differences in performance and operation...
International audienceIn this paper, an adaptive trajectory tracking controller for quadrotor MAVs i...
In this thesis is studied the landing problem of a VTOL UAV and a 3D sim-ulation environment is buil...