The subject of this paper is to review, comparative analysis and simulation of selected components of power electronic systems (PES), consistent with the concept of a more electric aircraft (MEA). Comparative analysis and simulation in software environment MATLAB / Simulink were carried out on the base of a group of representatives of civil aircraft (B-787, A-380) and military (F-22 Raptor, F-35) in the context of multi-pulse converters used in them (6- and 12-pulse, and 18- and 24-pulse), which are key components of high-tech electronics on-board power systems of autonomous power systems (ASE) of modern aircraft (airplanes of the future)
The complete electrification of aircraft power systems entails the implementation of smart logics fo...
In this thesis a modeling and simulation based methodology is proposed to study the general power fl...
Developing electrically-powered systems to boost the performance and reliability of tomorrow’s air...
he work deals with the issues of modern architecture power supply compatible with the trend of...
The subject of this paper is to conduct the testing process of multi-pulse rectifiers (6-, 12- and ...
The purpose of this paper is to review and make a comparative analysis of advanced architecture of t...
The subject of this paper is to make an analysis of advanced autonomous power systems (EPS, PES), in...
The purpose of this paper is to present some selected issues on the problems related to the power su...
We współczesnym lotnictwie (wojskowym, cywilnym), coraz częściej w projektowanych autonomicznych pok...
This article focuses on power electronic multi-pulse 12-, 24- and 36-impulse rectifiers based on mul...
W referacie przedstawiono analizę, model matematyczny oraz symulacje przekształtników energoelektron...
The purpose of this paper is to present some selected issues relating to the alternative application...
Based on the mathematical model of synchronous electric machine, basing on permanent magnets, presen...
Based on the analysis and mathematical models of synchronous electric machines (motor/generator), ba...
The present study aims at the implementation of a Matlab/Simulink environment to assess the performa...
The complete electrification of aircraft power systems entails the implementation of smart logics fo...
In this thesis a modeling and simulation based methodology is proposed to study the general power fl...
Developing electrically-powered systems to boost the performance and reliability of tomorrow’s air...
he work deals with the issues of modern architecture power supply compatible with the trend of...
The subject of this paper is to conduct the testing process of multi-pulse rectifiers (6-, 12- and ...
The purpose of this paper is to review and make a comparative analysis of advanced architecture of t...
The subject of this paper is to make an analysis of advanced autonomous power systems (EPS, PES), in...
The purpose of this paper is to present some selected issues on the problems related to the power su...
We współczesnym lotnictwie (wojskowym, cywilnym), coraz częściej w projektowanych autonomicznych pok...
This article focuses on power electronic multi-pulse 12-, 24- and 36-impulse rectifiers based on mul...
W referacie przedstawiono analizę, model matematyczny oraz symulacje przekształtników energoelektron...
The purpose of this paper is to present some selected issues relating to the alternative application...
Based on the mathematical model of synchronous electric machine, basing on permanent magnets, presen...
Based on the analysis and mathematical models of synchronous electric machines (motor/generator), ba...
The present study aims at the implementation of a Matlab/Simulink environment to assess the performa...
The complete electrification of aircraft power systems entails the implementation of smart logics fo...
In this thesis a modeling and simulation based methodology is proposed to study the general power fl...
Developing electrically-powered systems to boost the performance and reliability of tomorrow’s air...