State-of-the-art approaches in quadrotor control split the problem into multiple cascaded subproblems, exploiting the different time scales of the rotational and translational dynamics. They calculate a desired acceleration as input for a cascaded attitude controller but omit the attitude dynamics. These approaches use limits on the desired acceleration to maintain feasibility and robustness through the control cascade. We propose an implementation of an LQR controller, which: (I) is linearized depending on the quadrotor’s state; (II) unifies the control of rotational and translational states; (III) handles time-varying system dynamics and control parameters. Our implementation is efficient enough to compute the full linearization and solut...
The main motivation for this paper is to apply LQ and LQG methodologies for quadcopter control syste...
This paper presents an analysis and performance of a LQR control algorithm for quadrotor helicopters...
This work introduces a real time suboptimal control algorithm for six-degree-of-freedom spacecraft m...
State-of-the-art approaches in quadrotor control split the problem into multiple cascaded subproblem...
This paper presents the attitude behaviour of quad-rotor by using a LQR controller. The performance ...
The vertical take-off and landing capabilities of quadrotors, and their maneuverability has contribu...
Abstract—This paper presents an LQR-Based 6DOF control of an unmanned aerial vehicles (UAV), namely ...
A controller is designed for hexacopter platform to achieve accurate tracking of altitude and attitu...
This paper presents a solution to on-board trajectory tracking control of quadrotors. The proposed a...
The purpose of the paper is to discuss a comparative evaluation of performance of two different con...
Quadrotor is an unmanned aircraft which has vertical take-off and landing (VTOL) capability. However...
Unmanned aerial vehicles (UAVs) are subject to the wind and other environmental disturbances that ca...
This study exploits the dynamics and control of quadcopters using Linear Quadratic Regulator (LQR) ...
Quadrotors are aerial vehicles with a four motor-rotor assembly for generating lift and control...
This work presents a solution for the position-heading control problem of a small quadrotor. The mai...
The main motivation for this paper is to apply LQ and LQG methodologies for quadcopter control syste...
This paper presents an analysis and performance of a LQR control algorithm for quadrotor helicopters...
This work introduces a real time suboptimal control algorithm for six-degree-of-freedom spacecraft m...
State-of-the-art approaches in quadrotor control split the problem into multiple cascaded subproblem...
This paper presents the attitude behaviour of quad-rotor by using a LQR controller. The performance ...
The vertical take-off and landing capabilities of quadrotors, and their maneuverability has contribu...
Abstract—This paper presents an LQR-Based 6DOF control of an unmanned aerial vehicles (UAV), namely ...
A controller is designed for hexacopter platform to achieve accurate tracking of altitude and attitu...
This paper presents a solution to on-board trajectory tracking control of quadrotors. The proposed a...
The purpose of the paper is to discuss a comparative evaluation of performance of two different con...
Quadrotor is an unmanned aircraft which has vertical take-off and landing (VTOL) capability. However...
Unmanned aerial vehicles (UAVs) are subject to the wind and other environmental disturbances that ca...
This study exploits the dynamics and control of quadcopters using Linear Quadratic Regulator (LQR) ...
Quadrotors are aerial vehicles with a four motor-rotor assembly for generating lift and control...
This work presents a solution for the position-heading control problem of a small quadrotor. The mai...
The main motivation for this paper is to apply LQ and LQG methodologies for quadcopter control syste...
This paper presents an analysis and performance of a LQR control algorithm for quadrotor helicopters...
This work introduces a real time suboptimal control algorithm for six-degree-of-freedom spacecraft m...