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Research Article Peer ReviewedAt least two reviewers Open Access

Bidirectional Active Rectifier Phase Lock Loop Software Design for More Electric Aircraft

1Avionics Engineering MSc. at Yıldız Technical University
2Electrical Engineering Department, Yıldız Technical University
✉ Corresponding author: İ. Ethem Demiralay · ethem.demiralay@std.yildiz.edu.tr
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Abstract

The next generation aircraft will be operated first with hybrid technology and then with purely electric technology, just like in the automobile industry. More electric aircraft concepts today have brought about a reorganization of the generation, transmission and distribution of electric power. Power electronics technology plays a key role in connecting new electrical loads to the new aircraft electrical power system. One of the most important tasks of power electronics circuits in MEA is to convert aircraft variable frequency AC voltage to DC voltage of different level. Converters that perform the task are commonly known as "rectifiers". The aim of this study is to develop the grid synchronization code for a bidirectional three-phase active rectifier, which can meet the advanced requirements of more electric aircraft applications using digital signal processors. In order to test the developed code on a real microcontroller, hardware in the loop (HiL) test was carried out.

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Cite this article

Demiralay, İ. E., & Bakan, A. F. (2022). Bidirectional Active Rectifier Phase Lock Loop Software Design for More Electric Aircraft. In Proceeding of the 5th International Symposium on Innovative Approaches in Smart Technologies (pp. 19–23). SET Technology. https://doi.org/10.36287/setsci.5.1.004

Article History

Published
1 Jun 2022

License

© 2022 SET Technology. This article is distributed under the terms of the CC BY 4.0.

Research Contributions (2019+)Peer reviewed by at least two reviewers
Open AccessCC BY 4.0
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