Add to ORKGOne of the most critical issues for unmanned aerial vehicle (UAV) safety and precision flight is wind disturbance. To this end, this paper presents an acceleration feedback (AF) enhanced H∞ method for UAV flight control against wind disturbance and its application on a hex-rotor platform. The dynamics of the UAV system are decoupled into attitude control and position control loops. A hierarchical H∞ controller is then designed for the decoupled system. Finally, an AF-enhanced method is introduced into the decoupled system without altering the original control structure. The stability of the AF-enhanced H∞ method for the UAV system is analyzed and verified using the H∞ theory. Two types of wind disturbances—cont...
In a follow-up to our previous study, the current work examines the gust-induced “cone of uncertaint...
Small UAVs are susceptible to the external disturbance, especially the wind field disturbance in the...
For the case of helicopters in straight horizontal flight, the effects of a rotary gust to the forwa...
Wind disturbance has always been a critical challenge for safety flight and high precision control o...
One of the most critical issues for unmanned aerial vehicle (UAV) safety and precision flight is win...
Wind disturbance has always been a critical issue for safety fiight of unmanned aerial vehicle (UAV)...
An aerial manipulator is a new kind of flying robot system composed of a rotorcraft unmanned aerial ...
While a few proposed control strategies have shown their acceptable effectiveness, performance impro...
In this paper, a robust controller design method is proposed with measurable acceleration signals. I...
This paper presents a practical scheme to control heave motion for hover and automatic landing of a ...
In this paper altitude hold control system based on robust Hinf controller is considered. Tactical U...
This paper presents a novel acceleration feedback control method for robust hovering of a quadrotor ...
This paper outlines an innovative and feasible flight control scheme for a rotary-wing unmanned aeri...
Introduction. Unmanned aerial vehicles as quadcopters, twin rotors, fixed-wing crafts, and helicopte...
This paper presents a nonlinear gust-attenuation controller to stabilize velocities, attitudes and a...
In a follow-up to our previous study, the current work examines the gust-induced “cone of uncertaint...
Small UAVs are susceptible to the external disturbance, especially the wind field disturbance in the...
For the case of helicopters in straight horizontal flight, the effects of a rotary gust to the forwa...
Wind disturbance has always been a critical challenge for safety flight and high precision control o...
One of the most critical issues for unmanned aerial vehicle (UAV) safety and precision flight is win...
Wind disturbance has always been a critical issue for safety fiight of unmanned aerial vehicle (UAV)...
An aerial manipulator is a new kind of flying robot system composed of a rotorcraft unmanned aerial ...
While a few proposed control strategies have shown their acceptable effectiveness, performance impro...
In this paper, a robust controller design method is proposed with measurable acceleration signals. I...
This paper presents a practical scheme to control heave motion for hover and automatic landing of a ...
In this paper altitude hold control system based on robust Hinf controller is considered. Tactical U...
This paper presents a novel acceleration feedback control method for robust hovering of a quadrotor ...
This paper outlines an innovative and feasible flight control scheme for a rotary-wing unmanned aeri...
Introduction. Unmanned aerial vehicles as quadcopters, twin rotors, fixed-wing crafts, and helicopte...
This paper presents a nonlinear gust-attenuation controller to stabilize velocities, attitudes and a...
In a follow-up to our previous study, the current work examines the gust-induced “cone of uncertaint...
Small UAVs are susceptible to the external disturbance, especially the wind field disturbance in the...
For the case of helicopters in straight horizontal flight, the effects of a rotary gust to the forwa...