Abstract — This paper describes the stages of identification, dynamic modelling and control of an unmanned aerial vehicle of type quad-rotor designed to capture images and video in high definition with relatively low cost. The identification process describes the methods used to identify the elements of the vehicle such as propellers parameters, mathematical modeling of the whole ESC-Motor-Propeller and modeling of the complete structure of the quad-rotor. PID controllers were used for the control and stabilization of the structure, controlling the rotational speed of the four motors independently. To tune the controller we have used the pole placement method, followed by simulations in MATLAB, based on the models obtained in identification...
This paper presents preliminary results on modeling and control of a quadrotor UAV. With aerodynamic...
This paper presents modelling, simulation and implementation of a quadrotor Unmanned Arial Vehicle (...
International audienceSeveral methods can be applied to estimate the propeller thrust and torque coe...
This dissertation presents the development of an unmanned aerial vehicle of the type quadrirotor, it...
This paper presents the modeling of a four rotor vertical take-off and landing (VTOL) unmanned air v...
this paper presents the modelling of a four rotor vertical take-off and landing (VTOL) unmanned air ...
The key goal of this work was to develop a functional mathematical model of a 4-rotor UAV, including...
Esta dissertaÃÃo apresenta o desenvolvimento de um veÃculo aÃreo nÃo tripulado do tipo quadrirotor, ...
International audienceThis paper is focused on modeling and control of quadrotor; first modeling of ...
Quad-Rotor Control develops original control methods for the navigation and hovering flight of an au...
Motivated by the important growth of VTOL vehicles research such as quadrotors and to a small extent...
The interest in UAV technology is increasing in engineering and military usage and now even hobbyist...
This paper describes the experimental framework for the control system design and validation of a ro...
Unmanned aerial vehicles are used for research in many areas: photography and video shooting and so ...
Small rotary-wing UAVs have many potential non-military applications and specifically multi rotor UA...
This paper presents preliminary results on modeling and control of a quadrotor UAV. With aerodynamic...
This paper presents modelling, simulation and implementation of a quadrotor Unmanned Arial Vehicle (...
International audienceSeveral methods can be applied to estimate the propeller thrust and torque coe...
This dissertation presents the development of an unmanned aerial vehicle of the type quadrirotor, it...
This paper presents the modeling of a four rotor vertical take-off and landing (VTOL) unmanned air v...
this paper presents the modelling of a four rotor vertical take-off and landing (VTOL) unmanned air ...
The key goal of this work was to develop a functional mathematical model of a 4-rotor UAV, including...
Esta dissertaÃÃo apresenta o desenvolvimento de um veÃculo aÃreo nÃo tripulado do tipo quadrirotor, ...
International audienceThis paper is focused on modeling and control of quadrotor; first modeling of ...
Quad-Rotor Control develops original control methods for the navigation and hovering flight of an au...
Motivated by the important growth of VTOL vehicles research such as quadrotors and to a small extent...
The interest in UAV technology is increasing in engineering and military usage and now even hobbyist...
This paper describes the experimental framework for the control system design and validation of a ro...
Unmanned aerial vehicles are used for research in many areas: photography and video shooting and so ...
Small rotary-wing UAVs have many potential non-military applications and specifically multi rotor UA...
This paper presents preliminary results on modeling and control of a quadrotor UAV. With aerodynamic...
This paper presents modelling, simulation and implementation of a quadrotor Unmanned Arial Vehicle (...
International audienceSeveral methods can be applied to estimate the propeller thrust and torque coe...