Add to ORKGDynamic Radial Basis Function Neural Network (RBFNN) called Extended Minimum Resource Allocation Neural Network or EMRANN is used to aid a Baseline Trajectory Following Controller (BTFC) for achieving better fault tolerance for aircraft auto-landing under severe wind and actuator failures. EMRANN has an inbuilt mechanism to generate or prune the hidden layer neurons based on their contribution to system output, uses on-line training and does not need prior training. The performance of the EMRANN controller is demonstrated using simulated data for single and multiple actuator faults. The results show that the segmentation of BTFC with EMRANN controller improves the ability to handle large faults and also meet the strict touchdown requirement...
In this paper, adaptive critic based neural networks have been used to design a controller for a ben...
The research in this document focuses on the performance of a neural network-based fault tolerant sy...
The purpose of this communication is to deal with the case in which an aerodynamic actuator failure ...
This report presents a neural-aided controller that enhances the fault tolerant high performance fig...
In the paper presented at UKIERI 2009 Workshop, an Extended Minimum Resource Allocation Neural Netwo...
This paper presents an adaptive backstepping neural controller design for aircraft under control sur...
In the paper, a <span class="hit">neural</span> <span class="hit">control</span> scheme is presented...
In this talk, we will cover some recent work carried out in our group for developing intelligent fli...
Part I of this report presents the methodology of reliable autolanding control design for aircraft....
This report presents an adaptive back-stepping neural controller for reconfigurable flight control o...
A dissertation submitted to the Faculty of Engineering and the Built Environment, University of the...
This dissertation aims to do a performance evaluation between two controllers viz. Neural network ai...
This thesis presents the implementation of a newly developed minimal Radial Basis Function ( RBF ) n...
The authors have assessed the capability of various neural-aided classical feedback controllers tha...
Description of the performance of a simplified dynamic inversion controller with neural network augm...
In this paper, adaptive critic based neural networks have been used to design a controller for a ben...
The research in this document focuses on the performance of a neural network-based fault tolerant sy...
The purpose of this communication is to deal with the case in which an aerodynamic actuator failure ...
This report presents a neural-aided controller that enhances the fault tolerant high performance fig...
In the paper presented at UKIERI 2009 Workshop, an Extended Minimum Resource Allocation Neural Netwo...
This paper presents an adaptive backstepping neural controller design for aircraft under control sur...
In the paper, a <span class="hit">neural</span> <span class="hit">control</span> scheme is presented...
In this talk, we will cover some recent work carried out in our group for developing intelligent fli...
Part I of this report presents the methodology of reliable autolanding control design for aircraft....
This report presents an adaptive back-stepping neural controller for reconfigurable flight control o...
A dissertation submitted to the Faculty of Engineering and the Built Environment, University of the...
This dissertation aims to do a performance evaluation between two controllers viz. Neural network ai...
This thesis presents the implementation of a newly developed minimal Radial Basis Function ( RBF ) n...
The authors have assessed the capability of various neural-aided classical feedback controllers tha...
Description of the performance of a simplified dynamic inversion controller with neural network augm...
In this paper, adaptive critic based neural networks have been used to design a controller for a ben...
The research in this document focuses on the performance of a neural network-based fault tolerant sy...
The purpose of this communication is to deal with the case in which an aerodynamic actuator failure ...