Published Paper Details:

This paper with the design model and analysis of modern aircraft electrical power system (AEPS) using fuzzy logic control (FLC) technique with implemented proportional integral derivative (PID) control. In order to meet the standards of the of the aircraft, the behaviours of the aircraft electrical power system (AEPS) during load switching is controlled using PID -FLC technique. This technique is mainly suitable for the control of generator control unit, Ac-Dc controlled rectifier. In this proposed paper, the simulation of power MOSFET based Dc-Dc converter forward buck converter has been done in the MATLAB/SIMULINK and their corresponding voltage and current waveform are plotted obtained. To achieve high power factor and to have high efficiency, the advantage of forward buck converter is contained to form a novel forward buck converter. It is capable of operating in forward buck converter. Hance the lesser are highly reduced and the current near the zero crossing of input side is reduced using the balancing capacitor. The variable reactive load is employed to demonstrate the value of hormonic reduced at various value of voltage and current in the system.