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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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References

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  3. Gangavarapu, S. “Analysis and Design of Discontinuous Conduction Mode AC-DC Power Factor Correction Converters”. PhD. Eng. thesis, Concordia University, Montréal, Québec, Canada, Feb. 2020.
  4. Faundez, M. “Isolated swiss-forward three-phase rectifier for aircraft applications: analysis, design and validation”. PhD. Eng. thesis, Madrid Polytechnic University, Madrid, Spain, 2018.
  5. Borovic, U. “Contributions to The Design Methodology of Three-phase Active Rectifiers to Comply with Avionic Standards: Input Voltage Distortion and Phase Loss”. PhD. Eng. thesis, Madrid Polytechnic University, Madrid, Spain, 2019.
  6. Larsson C., Johansson O., “Active Power Factor Correction for Airborne Applications”. M. Eng. thesis, Chalmers University of Technology, Gothenburg, Sweden, 2012.
  7. Hartmann, M. “Ultra-compact and ultra-efficient three-phase PWM rectifier systems for more electric aircraft”. PhD. Eng. thesis, ETH Zurich, 2011.
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  9. Abu-Rub H., Malinowski M., Al-Haddad K., "Power Electronics for More Electric Aircraft," in Power Electronics for Renewable Energy Systems, Transportation and Industrial Applications , IEEE, 2014, pp.365-386, doi: 10.1002/9781118755525.ch12
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Research Contributions (2019+)Peer reviewed by at least two reviewers
Open AccessCC BY 4.0
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