This paper presents a disturbance attenuation controller for horizontal position stabilization for hover and automatic landings of a Rotary-wing Unmanned Aerial Vehicle (RUAV) operating in rough seas. Based on a helicopter model representing aerodynamics during the landing phase, a nonlinear state feedback H-infinity controller is designed to achieve rapid horizontal position tracking in a gusty environment. The resultant control variables are further treated in consideration of practical constraints (flapping dynamics, servo dynamics and time lag effect) for implementation purpose. The high-fidelity closed-loop simulation using parameters of the Vario helicopter verifies performance of the proposed position controller. It not only increase...
The autonomous ship landing control issue of multi-rotor Unmanned Aerial Vehicles (UAVs) is investig...
The objective of this work was to develop a variety of control systems for a Stop-Rotor Unmanned Aer...
This paper presents the development and experimental implementation of a novel two-time scale contro...
This paper presents a disturbance attenuation controller for horizontal position stabilization for h...
This study presents a disturbance attenuation controller for horizontal position stabilisation for h...
This paper presents a practical scheme to control heave motion for hover and automatic landing of a ...
This paper outlines an innovative and feasible flight control scheme for a rotary-wing unmanned aeri...
This thesis presents a novel position control method for rotary wing unmanned aerialvehicles (RUAVs)...
In this paper, the autonomous landing control issue on moving shipboard is investigated for unmanned...
Abstract The problem of stabilization of vertical, lateral and longitudinal dynamics for hover fligh...
Abstract- This paper considered the problem of stabilization of longitudinal and lateral dynamics of...
This paper presents a novel compensation method for the coupled fuselage-rotor mode of a Rotary wing...
Abstract—This paper presents a novel compensation method for the coupled fuselage-rotor mode of a Ro...
An aerial manipulator is a new kind of flying robot system composed of a rotorcraft unmanned aerial ...
This paper presents a nonlinear gust-attenuation controller to stabilize velocities, attitudes and a...
The autonomous ship landing control issue of multi-rotor Unmanned Aerial Vehicles (UAVs) is investig...
The objective of this work was to develop a variety of control systems for a Stop-Rotor Unmanned Aer...
This paper presents the development and experimental implementation of a novel two-time scale contro...
This paper presents a disturbance attenuation controller for horizontal position stabilization for h...
This study presents a disturbance attenuation controller for horizontal position stabilisation for h...
This paper presents a practical scheme to control heave motion for hover and automatic landing of a ...
This paper outlines an innovative and feasible flight control scheme for a rotary-wing unmanned aeri...
This thesis presents a novel position control method for rotary wing unmanned aerialvehicles (RUAVs)...
In this paper, the autonomous landing control issue on moving shipboard is investigated for unmanned...
Abstract The problem of stabilization of vertical, lateral and longitudinal dynamics for hover fligh...
Abstract- This paper considered the problem of stabilization of longitudinal and lateral dynamics of...
This paper presents a novel compensation method for the coupled fuselage-rotor mode of a Rotary wing...
Abstract—This paper presents a novel compensation method for the coupled fuselage-rotor mode of a Ro...
An aerial manipulator is a new kind of flying robot system composed of a rotorcraft unmanned aerial ...
This paper presents a nonlinear gust-attenuation controller to stabilize velocities, attitudes and a...
The autonomous ship landing control issue of multi-rotor Unmanned Aerial Vehicles (UAVs) is investig...
The objective of this work was to develop a variety of control systems for a Stop-Rotor Unmanned Aer...
This paper presents the development and experimental implementation of a novel two-time scale contro...