In this thesis, a flight control design of an unmanned aerial vehicle (UAV) using neural network based feedback linearization and the output redefinition technique is presented. The UAV model we chose in this research is a nonlinear nonminimum phase system. The output redefinition technique is used in a way such that the resulting system is minimum phase and can be inverted. The nonlinear autoregressive moving average (NARMA-L2) neural network is trained off-line to identify the forward dynamics of the UAV model with the redefined output, and then inverted to force the real output to approximately track the desired trajectory. The results shows that a good tracking performance can be achieved using this control scheme
Abstract: This paper presents a theoretical mechanical model of an unmanned aerial vehicle...
In this paper, a novel nonlinear output feedback neural network (NN)-based consensus controller is d...
Helicopter UAVs can be extensively used for military missions as well as in civil operations, rangin...
Abstractin this thesis, a flight control design of an unmanned aerial vehicle (UAV) using output red...
A neural network (NN) based output feedback controller for a quadrotor unmanned aerial vehicle (UAV)...
Recent publications on automatic flight controls are concentrated on neural network based adaptive c...
Aircraft dynamics are in general nonlinear, time-varying, and may be highly uncertain. Current-gener...
Abstract—A position tracking control system is developed for a rotorcraft-based unmanned aerial vehi...
The paper highlights the main steps of adaptive output feedback control for non-affine uncertain sys...
A small scale tri-rotor test bed with tilting propellers has been built to test flight control laws ...
This paper deals with the development of a flight control scheme based on the Nonlinear Dynamic Inve...
This paper deals with the development of a flight control scheme based on the Nonlinear Dynamic Inve...
This thesis presents the development of small, inexpensive unmanned aerial vehicles (UAVs) to achie...
This brief addresses the position and attitude tracking fixed-time practical control for quadrotor u...
A reconfigurable flight control method is developed to be implemented on an Unmanned Aircraft (UA), ...
Abstract: This paper presents a theoretical mechanical model of an unmanned aerial vehicle...
In this paper, a novel nonlinear output feedback neural network (NN)-based consensus controller is d...
Helicopter UAVs can be extensively used for military missions as well as in civil operations, rangin...
Abstractin this thesis, a flight control design of an unmanned aerial vehicle (UAV) using output red...
A neural network (NN) based output feedback controller for a quadrotor unmanned aerial vehicle (UAV)...
Recent publications on automatic flight controls are concentrated on neural network based adaptive c...
Aircraft dynamics are in general nonlinear, time-varying, and may be highly uncertain. Current-gener...
Abstract—A position tracking control system is developed for a rotorcraft-based unmanned aerial vehi...
The paper highlights the main steps of adaptive output feedback control for non-affine uncertain sys...
A small scale tri-rotor test bed with tilting propellers has been built to test flight control laws ...
This paper deals with the development of a flight control scheme based on the Nonlinear Dynamic Inve...
This paper deals with the development of a flight control scheme based on the Nonlinear Dynamic Inve...
This thesis presents the development of small, inexpensive unmanned aerial vehicles (UAVs) to achie...
This brief addresses the position and attitude tracking fixed-time practical control for quadrotor u...
A reconfigurable flight control method is developed to be implemented on an Unmanned Aircraft (UA), ...
Abstract: This paper presents a theoretical mechanical model of an unmanned aerial vehicle...
In this paper, a novel nonlinear output feedback neural network (NN)-based consensus controller is d...
Helicopter UAVs can be extensively used for military missions as well as in civil operations, rangin...