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Minimal
Resource Allocation Network: A sequential learning algorithm for realizing a minimal
radial basis function network (RBFN), referred to as Minimal Resource Allocating Network
(MRAN). With the growing and pruning strategy, the MRAN algorithm can implement a more compact network
structure, resulting in fast on-line learning. The MRAN algorithm is
successfully applied in the areas of function approximation, time series prediction, nonlinear system
identification and pattern recognition.
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Yingwei
Lu, N. Sundararajan, P. Saratchandran, “A Sequential Learning
Scheme for Function Approximation using Minimal Radial Basis
Function Neural Networks“, Neural Computation, MIT Press, USA,
Vol. 9, No. 2, pp. 461-478, February 1997.
Matlab
code: MRAN and EMRAN MATLAB Function Files
Call Admission Control: Minimal Resource Allocation Network (MRAN)
and its extend version EMRAN is used to solve the traffic
control problems in high-speed networks. Though the current
focus is on the Call Admission Control (CAC) for Asynchronous
Transfer Mode (ATM) networks, the method is applicable to any
high-speed net-work. The models of MRAN and EMRAN CAC schemes
have been designed by using OPNET. The network performances of
MRAN and EMRAN CAC schemes are com-pared with the two
conventional CAC schemes, Peak Band-width Allocation and Cell
Loss Ratio (CLR) upper bound formula. Simulation results show
that the new proposed CAC schemes are more efficient than the
two conventional CAC approaches under the same traffic
conditions.
Until the later part of 1940's and early 1950s flight control
research was aimed at providing pilot relief capabilities, mainly in
the form of auto-pilots. With the advent of high performance
aircrafts, it become evident that controllers were required to bring
the aircrafts within certain specified operating envelop that would
increase the pilots capabilities for controlling the aircrafts. Due
to stringent requirements and complexities of the modern flight
control system, it is difficult to estimate the nonlinearities
accurately. The performance of conventional controller will be
poor under severe nonlinearities. The research deals with the new
design development of adaptive and fault tolerant control systems using
neural network methodologies. Conventional aircraft, helicopters and
unmanned aerial vehicles are considered. The aim of the research area is the design of
adaptive flight controllers such that the aircraft can even under
severe fault and disturbances. The application of controllers to linear and nonlinear models was investigated.
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