The Study of the Autonomous Power Supply System of the More/All Electric Aircraft in AC/DC and DC/DC Processing

The paper presents analysis, simulations and a mathematical model of transducers in the field of processing (conversion) of AC/DC and DC/DC. The proposed transducer model is designed for use in aviation, among others, it may be considered for use on both civil aircrafts of Airbus and Boeing companie...

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Bibliographic Details
Published in2017 European Conference on Electrical Engineering and Computer Science (EECS) pp. 305 - 310
Main Authors Setlak, Lucjan, Kowalik, Rafal, Redo, Wojciech
Format Conference Proceeding
LanguageEnglish
Published IEEE 01.11.2017
Subjects
AC/DC and DC/DC processing
Aircraft
Mathematical model
Military aircraft
more/all electric aircraft
power electronics systems
Power harmonic filters
Pulse width modulation
Rectifiers
study
Voltage control
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DOI10.1109/EECS.2017.63

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Summary:The paper presents analysis, simulations and a mathematical model of transducers in the field of processing (conversion) of AC/DC and DC/DC. The proposed transducer model is designed for use in aviation, among others, it may be considered for use on both civil aircrafts of Airbus and Boeing companies (A-380 and A-350XWB, B-787) and Lockheed Martin (JSF F-35 and F-22 Raptor) military aircrafts compatible with the concept of more/all electric aircraft. The subject, and also the aim of this paper is to analyze and present the mathematical model and simulations of selected transducers in AC/DC and DC/DC processing. Based on the above, the final part of the paper presents an analysis of waveform simulations of selected transducers in the field of AC/DC and DC/DC processing performed in the Matlab/Simulink programming environment. In the final part the paper presents the main conclusions arising from the study of the basic component in terms of PES system, namely transducers AC/DC and DC/DC.
DOI:10.1109/EECS.2017.63