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 3 3 identity matrix
In this paper vertical, transition and horizontal modes flight controllers of a tilt-wing quadrotor ...
In this paper a continuous attitude tracking control law is derived directly on the rotation group S...
\u3cp\u3eThe control of a quadrotor is typically split into two subsequent problems: finding desired...
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 control has been noted for its trouble as the consequence of the high maneuverability, sys...
This paper presents the design of auto-stabilization control technique for a quadrotor system. Aqua...
This paper presents the design of auto-stabilization control technique for a quadrotor system. Aquad...
In this paper, we propose a new quaternion-based feedback control scheme for exponential attitude st...
Multirotors have been recognized to be particularly interesting for surveillance, search and rescue,...
Quadrotor are four rotor helicopters that fly using a pair of rotors spinning in opposite directions...
This paper presents the attitude behaviour of quad-rotor by using a LQR controller. The performance ...
Abstract—A new control scheme for position-orientation tracking of underactuated quadrotor robotic v...
The purpose of the paper is to discuss a comparative evaluation of performance of two different con...
As technology progresses, it is evident that an increasing amount of processes are adopting the idea...
In this paper vertical, transition and horizontal modes flight controllers of a tilt-wing quadrotor ...
In this paper a continuous attitude tracking control law is derived directly on the rotation group S...
\u3cp\u3eThe control of a quadrotor is typically split into two subsequent problems: finding desired...
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 control has been noted for its trouble as the consequence of the high maneuverability, sys...
This paper presents the design of auto-stabilization control technique for a quadrotor system. Aqua...
This paper presents the design of auto-stabilization control technique for a quadrotor system. Aquad...
In this paper, we propose a new quaternion-based feedback control scheme for exponential attitude st...
Multirotors have been recognized to be particularly interesting for surveillance, search and rescue,...
Quadrotor are four rotor helicopters that fly using a pair of rotors spinning in opposite directions...
This paper presents the attitude behaviour of quad-rotor by using a LQR controller. The performance ...
Abstract—A new control scheme for position-orientation tracking of underactuated quadrotor robotic v...
The purpose of the paper is to discuss a comparative evaluation of performance of two different con...
As technology progresses, it is evident that an increasing amount of processes are adopting the idea...
In this paper vertical, transition and horizontal modes flight controllers of a tilt-wing quadrotor ...
In this paper a continuous attitude tracking control law is derived directly on the rotation group S...
\u3cp\u3eThe control of a quadrotor is typically split into two subsequent problems: finding desired...