Abstractin this thesis, a flight control design of an unmanned aerial vehicle (UAV) using output redefinition based neutral network control technique is presented. The UAV model chosen is a nonlinear non-minimum phase system. The output redefinition technique is used in a way such that the resulting system is minimum phase and can be inverted.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 show that a good tracking performance can be achieved using this control scheme
Presented at the AIAA Guidance, Navigation, and Control Conference and Exhibit 21 - 24 August 2006,...
In this paper, a novel nonlinear output feedback neural network (NN)-based consensus controller is d...
This paper presents a nonlinear gust-attenuation controller based on constrained neural-network (NN)...
In this thesis, a flight control design of an unmanned aerial vehicle (UAV) using neural network bas...
Abstract In this article, a neural network-based tracking controller is developed for an unmanned he...
This paper deals with the development of a flight control scheme based on the Nonlinear Dynamic Inve...
Recent publications on automatic flight controls are concentrated on neural network based adaptive c...
A neural network (NN) based output feedback controller for a quadrotor unmanned aerial vehicle (UAV)...
This paper deals with the development of a flight control scheme based on the Nonlinear Dynamic Inve...
Reconfigurable control will play a major role in the advancement of aerospace control especially in ...
A small scale tri-rotor test bed with tilting propellers has been built to test flight control laws ...
This thesis presents the development of small, inexpensive unmanned aerial vehicles (UAVs) to achie...
UAVs are mostly used for surveillance, inspection and data acquisition. We have developed a Quadroto...
This article proposes an adaptive flight framework that integrates a discrete-time incremental nonli...
Abstract—A position tracking control system is developed for a rotorcraft-based unmanned aerial vehi...
Presented at the AIAA Guidance, Navigation, and Control Conference and Exhibit 21 - 24 August 2006,...
In this paper, a novel nonlinear output feedback neural network (NN)-based consensus controller is d...
This paper presents a nonlinear gust-attenuation controller based on constrained neural-network (NN)...
In this thesis, a flight control design of an unmanned aerial vehicle (UAV) using neural network bas...
Abstract In this article, a neural network-based tracking controller is developed for an unmanned he...
This paper deals with the development of a flight control scheme based on the Nonlinear Dynamic Inve...
Recent publications on automatic flight controls are concentrated on neural network based adaptive c...
A neural network (NN) based output feedback controller for a quadrotor unmanned aerial vehicle (UAV)...
This paper deals with the development of a flight control scheme based on the Nonlinear Dynamic Inve...
Reconfigurable control will play a major role in the advancement of aerospace control especially in ...
A small scale tri-rotor test bed with tilting propellers has been built to test flight control laws ...
This thesis presents the development of small, inexpensive unmanned aerial vehicles (UAVs) to achie...
UAVs are mostly used for surveillance, inspection and data acquisition. We have developed a Quadroto...
This article proposes an adaptive flight framework that integrates a discrete-time incremental nonli...
Abstract—A position tracking control system is developed for a rotorcraft-based unmanned aerial vehi...
Presented at the AIAA Guidance, Navigation, and Control Conference and Exhibit 21 - 24 August 2006,...
In this paper, a novel nonlinear output feedback neural network (NN)-based consensus controller is d...
This paper presents a nonlinear gust-attenuation controller based on constrained neural-network (NN)...