Design of a 20 kW Bidirectional Dual Active Bridge Converter for Aerospace Applications
Author:
Affiliation:
1. McMaster Automotive Resource Centre (MARC), McMaster University,Hamilton,ON,Canada
2. Eaton Research Labs,Menomonee Falls,WI,USA
3. Eaton Corporation,Aerospace Group, Fluid, and Electrical Distribution Division,Torrance,CA,USA
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10131044/10130846/10131638.pdf?arnumber=10131638
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3. Mil-std-810h: Environmental engineering considerations and laboratory tests;U S Department of Defense,2016
4. Design Optimization Methodology for Planar Transformers for More Electric Aircraft
5. Overview of Dual-Active-Bridge Isolated Bidirectional DC–DC Converter for High-Frequency-Link Power-Conversion System
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