a droop control based three phase bidirectional ac-dc converter for more electric aircraft applications

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ID: 236627
2017
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Abstract
This paper addresses the design and implementation of a droop controlled three phase bidirectional AC-DC converter for more electric aircraft (MEA) applications. A unified control strategy using a droop characteristic is presented to achieve the bidirectional power flow between the AC and DC source while maintaining a stable DC output voltage. Based on the rigorous control design, the converter is capable of operating over a wide frequency range with a unity power factor. The key findings obtained from the theoretical analysis are confirmed by simulation studies and further validated by a scaled down laboratory prototype. The practical results show good performance of the bidirectional converter and demonstrate the effectiveness of the proposed control strategies.
Reference Key
zheng2017energiesa Use this key to autocite in the manuscript while using SciMatic Manuscript Manager or Thesis Manager
Authors ;Xiancheng Zheng;Fei Gao;Husan Ali;Huamei Liu
Journal acs combinatorial science
Year 2017
DOI
10.3390/en10030400
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