Control-Based Stabilization of DC Microgrid for More Electric Aircraft

作     者：YANG Jiajun BUTICCHI Giampaolo GU Chunyang WHEELER Pat ZHANG He GERADA Chris 杨佳俊;BUTICCHI Giampaolo;顾春阳;WHEELER Pat;张何;GERADA Chris

作者机构：Key Laboratory of More Electric Aircraft Technology of Zhejiang ProvinceUniversity of Nottingham Ningbo ChinaNingbo 315000P.R.China Power ElectronicsMachines and Control GroupUniversity of NottinghamNottingham NG72RDU.K. 

基　　金：supported by Ministry of Science&Technology under National Key R&D Program of China(No.2021YFE0108600) Ningbo Science and Technology Bureau under S&T Innovation 2025 Major Special Program(No.2019B10071) Key International Cooperation of National Natural Science Foundation of China(No.51920105011) 

出 版 物：《Transactions of Nanjing University of Aeronautics and Astronautics》 (南京航空航天大学学报（英文版）)

年 卷 期：2021年第38卷第5期

页      码：737-746页

摘      要：Electrifying the on-board subsystems of aircraft becomes an inevitable process as being faced with the environmental pollution,along with the proposed concept called more electric aircraft(MEA).With the increasing number of on-board power electronic based devices,the distribution system of the aircraft can be regarded as an onboard *** it is known that the load power electronic converters can exhibit constant power load(CPL)characteristics and reduce the system stability,it is necessary to accurately predict and enhance the system stability in designing *** paper firstly analyzes the stability of an on-board DC microgrid with the presence of ***,discusses the reasons behind instability and proposes a control strategy to enhance system ***,the simulation results are worked out to validate the analysis and the effect of the proposed control strategy.

主 题 词：DC microgrid stability analysis impedance model constant power load more electric aircraft dual active bridge converter permanent magnet synchronous generator 

学科分类：08[工学] 0825[工学-环境科学与工程类] 

核心收录：

D　O　I：10.16356/j.1005-1120.2021.05.003

馆 藏 号：203106286...