This paper proposes a simple scheme of Proportional-Derivative (PD) plus Feedforward controller on SO(3) to control the attitude of a quadrotor. This controller only needs the measurement of angular velocity to calculate the exponential coordinates of the rotation matrix. With rotation matrix as an error variable of the controller, the simulation shows that the controller is able to drive the attitude of the quadrotor from hovering condition to desired attitude and from an attitude condition goes to the hovering condition, despite the system is disturbed. When the system is convergent, the rotation error matrix will be a 3x3 identity matrix
This paper describes nonlinear dynamics model of x-configuration quadrotor using Newton-Euler modell...
This paper describes nonlinear dynamics model of x-configuration quadrotor using Newton-Euler modell...
The following article represents the control of an unmanned airborne vehicle (Quadcopter), using non...
This paper proposes a simple scheme of Proportional-Derivative (PD) plus Feedforward controller on...
This paper proposes a simple scheme of Proportional-Derivative (PD) plus Feedforward controller on S...
Quadrotor are four rotor helicopters that fly using a pair of rotors spinning in opposite directions...
Quadrotor control has been noted for its trouble as the consequence of the high maneuverability, sys...
This study investigates the directional and lateral motion control of unmanned aerial vehicles by co...
Published version of an article in the journal: Mathematical Problems in Engineering. Also available...
A quadcopter control system is a fundamentally difficult and challenging problem because its dynamic...
Disturbance compensation is a challenging problem in quadrotor control, especially in nonzero set po...
Position control should maintain the position of the quadcopter at the desired location using the cu...
This paper present a control method “x? configuration quadcopter. The control method used PDAFC (Pro...
In this paper, a real-time setup and an implementation of a Proportional Derivative (PD) controller ...
Quadcopter is one of Unmanned Aerial Vehicle (UAV) which has two pairs of identical fixed pitched ro...
This paper describes nonlinear dynamics model of x-configuration quadrotor using Newton-Euler modell...
This paper describes nonlinear dynamics model of x-configuration quadrotor using Newton-Euler modell...
The following article represents the control of an unmanned airborne vehicle (Quadcopter), using non...
This paper proposes a simple scheme of Proportional-Derivative (PD) plus Feedforward controller on...
This paper proposes a simple scheme of Proportional-Derivative (PD) plus Feedforward controller on S...
Quadrotor are four rotor helicopters that fly using a pair of rotors spinning in opposite directions...
Quadrotor control has been noted for its trouble as the consequence of the high maneuverability, sys...
This study investigates the directional and lateral motion control of unmanned aerial vehicles by co...
Published version of an article in the journal: Mathematical Problems in Engineering. Also available...
A quadcopter control system is a fundamentally difficult and challenging problem because its dynamic...
Disturbance compensation is a challenging problem in quadrotor control, especially in nonzero set po...
Position control should maintain the position of the quadcopter at the desired location using the cu...
This paper present a control method “x? configuration quadcopter. The control method used PDAFC (Pro...
In this paper, a real-time setup and an implementation of a Proportional Derivative (PD) controller ...
Quadcopter is one of Unmanned Aerial Vehicle (UAV) which has two pairs of identical fixed pitched ro...
This paper describes nonlinear dynamics model of x-configuration quadrotor using Newton-Euler modell...
This paper describes nonlinear dynamics model of x-configuration quadrotor using Newton-Euler modell...
The following article represents the control of an unmanned airborne vehicle (Quadcopter), using non...