AC/DC Hybrid Electric Power Generation System for More Electric Aircraft by using Prototype Model

This paper declares the modeling and simulation of electric aircraft by using AC/DC hybrid electric power stage system for many electric aircraft. Compare the result of hardware & software system. There are many different voltage stock for the electrical system on ample civilian aircraft, 28 V de that can be used on large aircraft for lower power loads, and full electrical system on small aircraft. For field aircraft, 270 V dc (135 V) is used and several sub-systems are used on few big aircraft. 115 V ac at 400 Hz big loads on large military aircraft. The demonstration of the planned topology is proved with MATLAB / Simulation model.