Power Distribution Management System of the On-Board Electric Energy of an Aircraft Compatible with the MEA/AEA Concept

The subject of this paper is to analyze the subject of the research, to present a mathematical description of physical phenomena (mathematical model) and to perform simulation tests of the on-board autonomous power supply system ASE, both in the electric power system EPS and energo-electronic power system PES, implemented on modern advanced aircrafts of key aviation companies, including Airbus, Boeing, Lockheed Martin. The main goal of the article is to carry out simulation studies of the supply system of modern aircrafts compliant with the trend of electrified aircraft, not only in the field of electricity management and transmission, but above all in the aspect of the analysis of the variability of the nature of terminal equipment (receivers), e.g. in terms of inductive-capacitive, resistive-capacitive load and their mutual modification. In the final part of the work, based on the created mathematical model and the necessary simulation tests and analysis in this area, in accordance with the concept of a more electric aircraft, a summary was made and practical conclusions were drawn.