This paper presents an optimal state feedback controller based on Linear Quadratic Regulator (LQR) for a two-rotor aero-dynamical system (TRAS). TRAS is a highly nonlinear multi-input multi-output (MIMO) system with two degrees of freedom and cross coupling. There are two parameters that define the behavior of LQR controller: state weighting matrix and control weighting matrix. The two parameters influence the performance of LQR. Particle Swarm Optimization (PSO) is proposed to optimally tune weighting matrices of LQR. The major concern of using LQR controller is to stabilize the TRAS by making the beam move quickly and accurately for tracking a trajectory or to reach a desired altitude. The simulation results were carried out in MATLAB/Sim...
This paper presents the linear quadratic tracking (LQT) control of a quadrotor UAV by solving discre...
Unmanned aerial vehicles (UAVs) are subject to the wind and other environmental disturbances that ca...
This paper investigates and benchmarks quadrotor navigation and hold autopilots’ global control perf...
Abstract—This paper presents an optimal state feedback controller based on Linear Quadratic Regulato...
This paper deals with the attitude tracking control problem for a 2 DoF laboratory helicopter using ...
Quadrotor unmanned aerial vehicle (UAV) is an unstable nonlinear control system. Therefore, the deve...
LQR is an optimal controller. Optimal in that it is defined so as to provide the smallest possible e...
Quadrotor is an unmanned aircraft which has vertical take-off and landing (VTOL) capability. However...
In this paper, a novel analytical tuning methodology for PID gains, based on Linear Quadratic Regula...
The attitude control of a rocket during flight is crucial for ensuring precise trajectory adjustment...
A real-time novel algorithm for proportional, integral and derivative (PID) controller tuning for qu...
The project involves designing the controller for a two-axle railway vehicle suspension system. The ...
Autonomous air vehicles that are effcient and robust require reliable control systems that enable th...
Twin Rotor MIMO system (TRMS) is considered as a prototype model of Helicopter. The aim of studying ...
This paper proposes a linear quadratic controller based on particle swarm algorithm for the rear whe...
This paper presents the linear quadratic tracking (LQT) control of a quadrotor UAV by solving discre...
Unmanned aerial vehicles (UAVs) are subject to the wind and other environmental disturbances that ca...
This paper investigates and benchmarks quadrotor navigation and hold autopilots’ global control perf...
Abstract—This paper presents an optimal state feedback controller based on Linear Quadratic Regulato...
This paper deals with the attitude tracking control problem for a 2 DoF laboratory helicopter using ...
Quadrotor unmanned aerial vehicle (UAV) is an unstable nonlinear control system. Therefore, the deve...
LQR is an optimal controller. Optimal in that it is defined so as to provide the smallest possible e...
Quadrotor is an unmanned aircraft which has vertical take-off and landing (VTOL) capability. However...
In this paper, a novel analytical tuning methodology for PID gains, based on Linear Quadratic Regula...
The attitude control of a rocket during flight is crucial for ensuring precise trajectory adjustment...
A real-time novel algorithm for proportional, integral and derivative (PID) controller tuning for qu...
The project involves designing the controller for a two-axle railway vehicle suspension system. The ...
Autonomous air vehicles that are effcient and robust require reliable control systems that enable th...
Twin Rotor MIMO system (TRMS) is considered as a prototype model of Helicopter. The aim of studying ...
This paper proposes a linear quadratic controller based on particle swarm algorithm for the rear whe...
This paper presents the linear quadratic tracking (LQT) control of a quadrotor UAV by solving discre...
Unmanned aerial vehicles (UAVs) are subject to the wind and other environmental disturbances that ca...
This paper investigates and benchmarks quadrotor navigation and hold autopilots’ global control perf...