The purpose of the paper is to discuss a comparative evaluation of performance of two different controllers i.e. Proportional-Derivative Controller (PD) and Linear Quadratic Regulation (LQR) in Quadrotor dynamic system that is under-actuated with high nonlinearity. As only four states can be controlled at the same time in the Quadrotor, the trajectories are designed on the basis of the four states whereas three dimensional position and rotation along an axis, known as yaw movement are considered. In this work, both the PD controller and LQR control approach are used for Quadrotor nonlinear model to track the trajectories. LQR control approach for nonlinear model is designed on the basis of a linear model of the Quadrotor because the...
The quadrotor is an ideal platform for testing control strategies because of its non-linearity and u...
In this work, two approaches to the control of a quadcopter are followed. The rst approach resorts ...
A quadcopter control system is a fundamentally difficult and challenging problem because its dynamic...
The purpose of this article is to evaluate the performances of the three different controllers such ...
This paper presents the attitude behaviour of quad-rotor by using a LQR controller. The performance ...
The purpose of this article is to evaluate the performances of the three different controllers such...
The vertical take-off and landing capabilities of quadrotors, and their maneuverability has contribu...
This study exploits the dynamics and control of quadcopters using Linear Quadratic Regulator (LQR) ...
In this thesis, trajectory tracking of a quadrotor UAV is obtained by controlling attitude and posit...
The findings of this paper are focused on the dynamics and control of a quadcopter using a modified ...
International audienceRecently the quadrotors are being increasingly employed in both military and c...
Orientador: Juan Francisco CaminoDissertação (mestrado) - Universidade Estadual de Campinas, Faculda...
This paper presents the linear quadratic tracking (LQT) control of a quadrotor UAV by solving discre...
As technology progresses, it is evident that an increasing amount of processes are adopting the idea...
In this work, a mathematical model of a quadrotor’s dynamics is derived, usingNewton’s and Euler’s l...
The quadrotor is an ideal platform for testing control strategies because of its non-linearity and u...
In this work, two approaches to the control of a quadcopter are followed. The rst approach resorts ...
A quadcopter control system is a fundamentally difficult and challenging problem because its dynamic...
The purpose of this article is to evaluate the performances of the three different controllers such ...
This paper presents the attitude behaviour of quad-rotor by using a LQR controller. The performance ...
The purpose of this article is to evaluate the performances of the three different controllers such...
The vertical take-off and landing capabilities of quadrotors, and their maneuverability has contribu...
This study exploits the dynamics and control of quadcopters using Linear Quadratic Regulator (LQR) ...
In this thesis, trajectory tracking of a quadrotor UAV is obtained by controlling attitude and posit...
The findings of this paper are focused on the dynamics and control of a quadcopter using a modified ...
International audienceRecently the quadrotors are being increasingly employed in both military and c...
Orientador: Juan Francisco CaminoDissertação (mestrado) - Universidade Estadual de Campinas, Faculda...
This paper presents the linear quadratic tracking (LQT) control of a quadrotor UAV by solving discre...
As technology progresses, it is evident that an increasing amount of processes are adopting the idea...
In this work, a mathematical model of a quadrotor’s dynamics is derived, usingNewton’s and Euler’s l...
The quadrotor is an ideal platform for testing control strategies because of its non-linearity and u...
In this work, two approaches to the control of a quadcopter are followed. The rst approach resorts ...
A quadcopter control system is a fundamentally difficult and challenging problem because its dynamic...