@inproceedings{ee281b2d03e44487a97c3e33b4469395,
title = "Semi-physical real-time test platform for aviation power system",
abstract = "Prototyping and proper testing of the electrical control unit of more electric aircraft (MEA) under various load profiles and fault conditions is necessary to ensure the performance of the controller. In order to solve the problems such as complicated operation, high experiment cost and long development period in aircraft power system traditional test method, this paper presents a semi-physical real-time test platform for aircraft power system testing and presents results and design principles of a three-stage brushless excitation power system emulation using HIL simulation.",
keywords = "MEA, hardware-in-the-loop, real-time simulation, semi-physical, starter/generator",
author = "Meiqi Wang and Lingquan Zeng and Lie Xu and Kui Wang and Zedong Zheng and Yongdong Li and Yue Ma",
note = "Publisher Copyright: {\textcopyright} 2017 IEEE.; 3rd IEEE International Future Energy Electronics Conference and ECCE Asia, IFEEC - ECCE Asia 2017 ; Conference date: 03-06-2017 Through 07-06-2017",
year = "2017",
month = jul,
day = "25",
doi = "10.1109/IFEEC.2017.7992297",
language = "English",
series = "2017 IEEE 3rd International Future Energy Electronics Conference and ECCE Asia, IFEEC - ECCE Asia 2017",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
pages = "1665--1669",
booktitle = "2017 IEEE 3rd International Future Energy Electronics Conference and ECCE Asia, IFEEC - ECCE Asia 2017",
address = "United States",
}