Hardware-in-Loop Semi-physical Simulation Research on Aviation Permanent Magnet Synchronous Motor Drive System

Ning Li; Xinyuan Wang; Ming Yan; Shuang Li; Xiaoli Duan; Yang Qi

doi:10.1007/978-981-95-7652-4_62

Hardware-in-Loop Semi-physical Simulation Research on Aviation Permanent Magnet Synchronous Motor Drive System

Ning Li
, Xinyuan Wang
, Ming Yan
, Shuang Li
, Xiaoli Duan
, Yang Qi

School of Automation

Ltd.

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

Abstract

A high-confidence hardware-in-loop (HIL) semi-physical simulation platform was developed to address the high cost and energy consumption of physical testing of aviation permanent magnet synchronous motor (PMSM) drive systems. Taking the aviation electro-actuated PMSM drive system as the research object, a semi-physical simulation model of permanent magnet synchronous motor, inverter and electro-actuated load was established; Control strategy research and hardware implementation were carried out, the system HIL semi-physical simulation platform was built, and simulation tests of steady-state, fast start-up and two typical electro-actuated load characteristics were conducted. The accuracy of the simulation test results compared with the full physical test results reached 80%. It was verified that the established HIL semi-physical simulation platform has a high level of confidence, which can not only reflect the steady-state performance of the system, but also well reflect the dynamic performance of the system under complex conditions, and can provide accurate model support for the subsequent analysis and research of other complex conditions of PMSM drive systems.

Original language	English
Title of host publication	The Proceedings of the 20th Annual Conference of China Electrotechnical Society
Editors	Qingxin Yang, Dianguo Xu, Xuerong Ye, Qiuyue Nie, Yueshi Guan
Publisher	Springer Science and Business Media Deutschland GmbH
Pages	596-614
Number of pages	19
ISBN (Print)	9789819576517
DOIs	https://doi.org/10.1007/978-981-95-7652-4_62
State	Published - 2026
Event	20th Annual Conference of China Electrotechnical Society, ACCES 2025 - Harbin, China Duration: 19 Sep 2025 → 21 Sep 2025

Publication series

Name	Lecture Notes in Electrical Engineering
Volume	1581 LNEE
ISSN (Print)	1876-1100
ISSN (Electronic)	1876-1119

Conference

Conference	20th Annual Conference of China Electrotechnical Society, ACCES 2025
Country/Territory	China
City	Harbin
Period	19/09/25 → 21/09/25

UN SDGs

This output contributes to the following UN Sustainable Development Goals (SDGs)

SDG 7 Affordable and Clean Energy

Keywords

Permanent magnet synchronous motor
electro-actuation
hardware in-loop
load characteristics

Access to Document

10.1007/978-981-95-7652-4_62

Cite this

Li, N., Wang, X., Yan, M., Li, S., Duan, X., & Qi, Y. (2026). Hardware-in-Loop Semi-physical Simulation Research on Aviation Permanent Magnet Synchronous Motor Drive System. In Q. Yang, D. Xu, X. Ye, Q. Nie, & Y. Guan (Eds.), The Proceedings of the 20th Annual Conference of China Electrotechnical Society (pp. 596-614). (Lecture Notes in Electrical Engineering; Vol. 1581 LNEE). Springer Science and Business Media Deutschland GmbH. https://doi.org/10.1007/978-981-95-7652-4_62

Li, Ning ; Wang, Xinyuan ; Yan, Ming et al. / Hardware-in-Loop Semi-physical Simulation Research on Aviation Permanent Magnet Synchronous Motor Drive System. The Proceedings of the 20th Annual Conference of China Electrotechnical Society. editor / Qingxin Yang ; Dianguo Xu ; Xuerong Ye ; Qiuyue Nie ; Yueshi Guan. Springer Science and Business Media Deutschland GmbH, 2026. pp. 596-614 (Lecture Notes in Electrical Engineering).

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title = "Hardware-in-Loop Semi-physical Simulation Research on Aviation Permanent Magnet Synchronous Motor Drive System",

abstract = "A high-confidence hardware-in-loop (HIL) semi-physical simulation platform was developed to address the high cost and energy consumption of physical testing of aviation permanent magnet synchronous motor (PMSM) drive systems. Taking the aviation electro-actuated PMSM drive system as the research object, a semi-physical simulation model of permanent magnet synchronous motor, inverter and electro-actuated load was established; Control strategy research and hardware implementation were carried out, the system HIL semi-physical simulation platform was built, and simulation tests of steady-state, fast start-up and two typical electro-actuated load characteristics were conducted. The accuracy of the simulation test results compared with the full physical test results reached 80\%. It was verified that the established HIL semi-physical simulation platform has a high level of confidence, which can not only reflect the steady-state performance of the system, but also well reflect the dynamic performance of the system under complex conditions, and can provide accurate model support for the subsequent analysis and research of other complex conditions of PMSM drive systems.",

keywords = "Permanent magnet synchronous motor, electro-actuation, hardware in-loop, load characteristics",

author = "Ning Li and Xinyuan Wang and Ming Yan and Shuang Li and Xiaoli Duan and Yang Qi",

note = "Publisher Copyright: {\textcopyright} Beijing Paike Culture Commu. Co., Ltd. 2026.; 20th Annual Conference of China Electrotechnical Society, ACCES 2025 ; Conference date: 19-09-2025 Through 21-09-2025",

year = "2026",

doi = "10.1007/978-981-95-7652-4\_62",

language = "英语",

isbn = "9789819576517",

series = "Lecture Notes in Electrical Engineering",

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Li, N, Wang, X, Yan, M, Li, S, Duan, X & Qi, Y 2026, Hardware-in-Loop Semi-physical Simulation Research on Aviation Permanent Magnet Synchronous Motor Drive System. in Q Yang, D Xu, X Ye, Q Nie & Y Guan (eds), The Proceedings of the 20th Annual Conference of China Electrotechnical Society. Lecture Notes in Electrical Engineering, vol. 1581 LNEE, Springer Science and Business Media Deutschland GmbH, pp. 596-614, 20th Annual Conference of China Electrotechnical Society, ACCES 2025, Harbin, China, 19/09/25. https://doi.org/10.1007/978-981-95-7652-4_62

Hardware-in-Loop Semi-physical Simulation Research on Aviation Permanent Magnet Synchronous Motor Drive System. / Li, Ning; Wang, Xinyuan; Yan, Ming et al.
The Proceedings of the 20th Annual Conference of China Electrotechnical Society. ed. / Qingxin Yang; Dianguo Xu; Xuerong Ye; Qiuyue Nie; Yueshi Guan. Springer Science and Business Media Deutschland GmbH, 2026. p. 596-614 (Lecture Notes in Electrical Engineering; Vol. 1581 LNEE).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

TY - GEN

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AU - Li, Ning

AU - Wang, Xinyuan

AU - Yan, Ming

AU - Li, Shuang

AU - Duan, Xiaoli

AU - Qi, Yang

N1 - Publisher Copyright: © Beijing Paike Culture Commu. Co., Ltd. 2026.

PY - 2026

Y1 - 2026

N2 - A high-confidence hardware-in-loop (HIL) semi-physical simulation platform was developed to address the high cost and energy consumption of physical testing of aviation permanent magnet synchronous motor (PMSM) drive systems. Taking the aviation electro-actuated PMSM drive system as the research object, a semi-physical simulation model of permanent magnet synchronous motor, inverter and electro-actuated load was established; Control strategy research and hardware implementation were carried out, the system HIL semi-physical simulation platform was built, and simulation tests of steady-state, fast start-up and two typical electro-actuated load characteristics were conducted. The accuracy of the simulation test results compared with the full physical test results reached 80%. It was verified that the established HIL semi-physical simulation platform has a high level of confidence, which can not only reflect the steady-state performance of the system, but also well reflect the dynamic performance of the system under complex conditions, and can provide accurate model support for the subsequent analysis and research of other complex conditions of PMSM drive systems.

AB - A high-confidence hardware-in-loop (HIL) semi-physical simulation platform was developed to address the high cost and energy consumption of physical testing of aviation permanent magnet synchronous motor (PMSM) drive systems. Taking the aviation electro-actuated PMSM drive system as the research object, a semi-physical simulation model of permanent magnet synchronous motor, inverter and electro-actuated load was established; Control strategy research and hardware implementation were carried out, the system HIL semi-physical simulation platform was built, and simulation tests of steady-state, fast start-up and two typical electro-actuated load characteristics were conducted. The accuracy of the simulation test results compared with the full physical test results reached 80%. It was verified that the established HIL semi-physical simulation platform has a high level of confidence, which can not only reflect the steady-state performance of the system, but also well reflect the dynamic performance of the system under complex conditions, and can provide accurate model support for the subsequent analysis and research of other complex conditions of PMSM drive systems.

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KW - hardware in-loop

KW - load characteristics

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A2 - Guan, Yueshi

PB - Springer Science and Business Media Deutschland GmbH

T2 - 20th Annual Conference of China Electrotechnical Society, ACCES 2025

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ER -

Li N, Wang X, Yan M, Li S, Duan X, Qi Y. Hardware-in-Loop Semi-physical Simulation Research on Aviation Permanent Magnet Synchronous Motor Drive System. In Yang Q, Xu D, Ye X, Nie Q, Guan Y, editors, The Proceedings of the 20th Annual Conference of China Electrotechnical Society. Springer Science and Business Media Deutschland GmbH. 2026. p. 596-614. (Lecture Notes in Electrical Engineering). doi: 10.1007/978-981-95-7652-4_62

Hardware-in-Loop Semi-physical Simulation Research on Aviation Permanent Magnet Synchronous Motor Drive System

Abstract

Publication series

Conference

UN SDGs

Keywords

Access to Document

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