International audienceThis paper addresses the problem of attitude/altitude control of a quadrotor. The main contribution consists in developing a simple Linear Parameter Varying model which includes the motor dynamics and weight variations. Afterwards, a reference model is introduced and an error model is derived. An integral action is thus naturally included in the loop. The proposed controller takes the form of a static output feedback which is synthesised using the Linear Matrix Inequalities framework. Thanks to a relaxation method the nonlinear terms are removed from the matrix inequalities. The controller in then reconstructed as a combination of the integral of the error, the actual output and the preview reference signal. Simulation...
Quadrotor is an unmanned aircraft which has vertical take-off and landing (VTOL) capability. However...
The findings of this paper are focused on the dynamics and control of a quadcopter using a modified ...
A quadrotor is a typical multiple-input multiple-output (MIMO), underactuated, strong coupled nonlin...
International audienceThis paper addresses the problem of attitude/altitude control of a quadrotor. ...
This master thesis addresses the LPV control of a quadrotor system. The quadorotor model is first tr...
This work presents a solution for the position-heading control problem of a small quadrotor. The mai...
Máster Automàtica i Robòtica.This master thesis addresses the LPV control of a quadrotor system. The...
In this paper, a solution for the attitude/altitude tracking control problem is proposed for a quadr...
Small quadcopters have demonstrated to be the perfect testing bench for addressing the autonomous fl...
This paper presents the attitude behaviour of quad-rotor by using a LQR controller. The performance ...
International audienceThis paper presents a hybrid robust control strategy to solve the trajectory t...
Due to the various applications of the quadrotor UAV systems increase in a daily basis, the research...
ABSTRACT The work proposed in this paper aim to design tow controllers for attitude stabilization of...
This paper proposes a linear parameter varying (LPV) model reference-based control for fixed-wing un...
Due to the various applications of the quadrotor unmanned aerial vehicle (UAV) systems increase dail...
Quadrotor is an unmanned aircraft which has vertical take-off and landing (VTOL) capability. However...
The findings of this paper are focused on the dynamics and control of a quadcopter using a modified ...
A quadrotor is a typical multiple-input multiple-output (MIMO), underactuated, strong coupled nonlin...
International audienceThis paper addresses the problem of attitude/altitude control of a quadrotor. ...
This master thesis addresses the LPV control of a quadrotor system. The quadorotor model is first tr...
This work presents a solution for the position-heading control problem of a small quadrotor. The mai...
Máster Automàtica i Robòtica.This master thesis addresses the LPV control of a quadrotor system. The...
In this paper, a solution for the attitude/altitude tracking control problem is proposed for a quadr...
Small quadcopters have demonstrated to be the perfect testing bench for addressing the autonomous fl...
This paper presents the attitude behaviour of quad-rotor by using a LQR controller. The performance ...
International audienceThis paper presents a hybrid robust control strategy to solve the trajectory t...
Due to the various applications of the quadrotor UAV systems increase in a daily basis, the research...
ABSTRACT The work proposed in this paper aim to design tow controllers for attitude stabilization of...
This paper proposes a linear parameter varying (LPV) model reference-based control for fixed-wing un...
Due to the various applications of the quadrotor unmanned aerial vehicle (UAV) systems increase dail...
Quadrotor is an unmanned aircraft which has vertical take-off and landing (VTOL) capability. However...
The findings of this paper are focused on the dynamics and control of a quadcopter using a modified ...
A quadrotor is a typical multiple-input multiple-output (MIMO), underactuated, strong coupled nonlin...