Design and Implementation of Active PFC Rectifier Topology for Avionic and Fleet Electrification-Reference-Cited by-同舟云学术

Design and Implementation of Active PFC Rectifier Topology for Avionic and Fleet Electrification

Published:2023-07-15 Issue:4 Volume:47 Page:1405-1416
ISSN:2228-6179
Container-title:Iranian Journal of Science and Technology, Transactions of Electrical Engineering
language:en
Short-container-title:Iran J Sci Technol Trans Electr Eng

Author:

Jeyapradha R. B.^ORCID,Rajini V.,Vikram A. S.

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Computer Networks and Communications,Computer Vision and Pattern Recognition,Energy Engineering and Power Technology,Signal Processing

Link

https://link.springer.com/content/pdf/10.1007/s40998-023-00636-3.pdf

Reference20 articles.

1. Ali A, Chuanwen J, Yan Z, Habib S, Khan MM (2021) An efficient soft-switched Vienna rectifier topology for EV battery chargers. Energy Rep 7:5059–5073. https://doi.org/10.1016/j.egyr.2021.08.105

2. Borovic U et al. (2016) Comparison of three-phase active rectifier solutions for avionic applications: impact of the avionic standard DO-160 F and failure modes. In: IEEE Energy Conversion Congress and Exposition (ECCE), USA. pp 1–8. https://doi.org/10.1109/ECCE.2016.7854943.

3. Channegowda J, Pathipati VK, Williamson SS (2015) Comprehensive review and comparison of DC fast charging converter topologies: improving electric vehicle plug-to-wheels efficiency. In: IEEE 24th international symposium on industrial electronics (ISIE), Brazil pp 263–268. https://doi.org/10.1109/ISIE.2015.7281479.

4. Ding W, Zhang C, Gao F, Duan B, Qiu H (2018) A zero-sequence component injection modulation method with compensation for current harmonic mitigation of a VIENNA rectifier. IEEE Trans Ind Electron 34(1):801–814. https://doi.org/10.1109/TPEL.2018.2812810

5. Gong G, Heldwein ML, Drofenik U, Miniböck J, Mino K, Kolar JW (2005) Comparative evaluation of three-phase high-power-factor AC–DC converter concepts for application in future more electric aircraft. IEEE Trans Ind Electron 52(3):727–737. https://doi.org/10.1109/TIE.2005.843957