Development of a Hardware-in-the-Loop Testbed for Distributed Electric Propulsion System in All-Electric Aircraft

Cong Yuan; Heyu Gao; Sheng Quan; Kai Han; Yuhua Du; Yigeng Huangfu; Fei Gao; Jun Zhao; Ziqiao Wang

doi:10.1109/ECCE53617.2023.10362217

Development of a Hardware-in-the-Loop Testbed for Distributed Electric Propulsion System in All-Electric Aircraft

Cong Yuan
, Heyu Gao
, Sheng Quan
, Kai Han
, Yuhua Du
, Yigeng Huangfu
, Fei Gao
, Jun Zhao
, Ziqiao Wang

School of Automation

Northwestern Polytechnical University Xian
University of Technology of Belfort-Montbéliard
China Aviation Industry Corporation
China Eastern Airline

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

1 Scopus citations

Abstract

This paper proposes a kW-level Hardware-in-the-loop (HIL) testbed to validate the performance of the distributed electric propulsion system (DEPS) as part of the all-electric aircraft design. The aircraft's flight dynamics and left-wing onboard power grid are replicated using detailed models in a real-time simulator, while the operating characteristics of DEPS are studied using both controller HIL (C-HIL) and power HIL (P-HIL). Some flight tests have been conducted on the developed testbed for validation.

Original language	English
Title of host publication	2023 IEEE Energy Conversion Congress and Exposition, ECCE 2023
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	1876-1882
Number of pages	7
ISBN (Electronic)	9798350316445
DOIs	https://doi.org/10.1109/ECCE53617.2023.10362217
State	Published - 2023
Event	2023 IEEE Energy Conversion Congress and Exposition, ECCE 2023 - Nashville, United States Duration: 29 Oct 2023 → 2 Nov 2023

Publication series

Name	2023 IEEE Energy Conversion Congress and Exposition, ECCE 2023

Conference

Conference	2023 IEEE Energy Conversion Congress and Exposition, ECCE 2023
Country/Territory	United States
City	Nashville
Period	29/10/23 → 2/11/23

UN SDGs

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

SDG 7 Affordable and Clean Energy

Keywords

Distributed Electric Propulsion System
Electric Aircraft
Hardware-in-the-loop

Access to Document

10.1109/ECCE53617.2023.10362217

Cite this

Yuan, C., Gao, H., Quan, S., Han, K., Du, Y., Huangfu, Y., Gao, F., Zhao, J., & Wang, Z. (2023). Development of a Hardware-in-the-Loop Testbed for Distributed Electric Propulsion System in All-Electric Aircraft. In 2023 IEEE Energy Conversion Congress and Exposition, ECCE 2023 (pp. 1876-1882). (2023 IEEE Energy Conversion Congress and Exposition, ECCE 2023). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/ECCE53617.2023.10362217

@inproceedings{8fdf021de7a841f5ba61e0d82c3cb78f,

title = "Development of a Hardware-in-the-Loop Testbed for Distributed Electric Propulsion System in All-Electric Aircraft",

abstract = "This paper proposes a kW-level Hardware-in-the-loop (HIL) testbed to validate the performance of the distributed electric propulsion system (DEPS) as part of the all-electric aircraft design. The aircraft's flight dynamics and left-wing onboard power grid are replicated using detailed models in a real-time simulator, while the operating characteristics of DEPS are studied using both controller HIL (C-HIL) and power HIL (P-HIL). Some flight tests have been conducted on the developed testbed for validation.",

keywords = "Distributed Electric Propulsion System, Electric Aircraft, Hardware-in-the-loop",

author = "Cong Yuan and Heyu Gao and Sheng Quan and Kai Han and Yuhua Du and Yigeng Huangfu and Fei Gao and Jun Zhao and Ziqiao Wang",

note = "Publisher Copyright: {\textcopyright} 2023 IEEE.; 2023 IEEE Energy Conversion Congress and Exposition, ECCE 2023 ; Conference date: 29-10-2023 Through 02-11-2023",

year = "2023",

doi = "10.1109/ECCE53617.2023.10362217",

language = "英语",

series = "2023 IEEE Energy Conversion Congress and Exposition, ECCE 2023",

publisher = "Institute of Electrical and Electronics Engineers Inc.",

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booktitle = "2023 IEEE Energy Conversion Congress and Exposition, ECCE 2023",

}

Yuan, C, Gao, H, Quan, S, Han, K, Du, Y , Huangfu, Y, Gao, F, Zhao, J & Wang, Z 2023, Development of a Hardware-in-the-Loop Testbed for Distributed Electric Propulsion System in All-Electric Aircraft. in 2023 IEEE Energy Conversion Congress and Exposition, ECCE 2023. 2023 IEEE Energy Conversion Congress and Exposition, ECCE 2023, Institute of Electrical and Electronics Engineers Inc., pp. 1876-1882, 2023 IEEE Energy Conversion Congress and Exposition, ECCE 2023, Nashville, United States, 29/10/23. https://doi.org/10.1109/ECCE53617.2023.10362217

Development of a Hardware-in-the-Loop Testbed for Distributed Electric Propulsion System in All-Electric Aircraft. / Yuan, Cong; Gao, Heyu; Quan, Sheng et al.
2023 IEEE Energy Conversion Congress and Exposition, ECCE 2023. Institute of Electrical and Electronics Engineers Inc., 2023. p. 1876-1882 (2023 IEEE Energy Conversion Congress and Exposition, ECCE 2023).

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

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AU - Du, Yuhua

AU - Huangfu, Yigeng

AU - Gao, Fei

AU - Zhao, Jun

AU - Wang, Ziqiao

PY - 2023

Y1 - 2023

N2 - This paper proposes a kW-level Hardware-in-the-loop (HIL) testbed to validate the performance of the distributed electric propulsion system (DEPS) as part of the all-electric aircraft design. The aircraft's flight dynamics and left-wing onboard power grid are replicated using detailed models in a real-time simulator, while the operating characteristics of DEPS are studied using both controller HIL (C-HIL) and power HIL (P-HIL). Some flight tests have been conducted on the developed testbed for validation.

AB - This paper proposes a kW-level Hardware-in-the-loop (HIL) testbed to validate the performance of the distributed electric propulsion system (DEPS) as part of the all-electric aircraft design. The aircraft's flight dynamics and left-wing onboard power grid are replicated using detailed models in a real-time simulator, while the operating characteristics of DEPS are studied using both controller HIL (C-HIL) and power HIL (P-HIL). Some flight tests have been conducted on the developed testbed for validation.

KW - Distributed Electric Propulsion System

KW - Electric Aircraft

KW - Hardware-in-the-loop

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BT - 2023 IEEE Energy Conversion Congress and Exposition, ECCE 2023

PB - Institute of Electrical and Electronics Engineers Inc.

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ER -

Yuan C, Gao H, Quan S, Han K, Du Y , Huangfu Y et al. Development of a Hardware-in-the-Loop Testbed for Distributed Electric Propulsion System in All-Electric Aircraft. In 2023 IEEE Energy Conversion Congress and Exposition, ECCE 2023. Institute of Electrical and Electronics Engineers Inc. 2023. p. 1876-1882. (2023 IEEE Energy Conversion Congress and Exposition, ECCE 2023). doi: 10.1109/ECCE53617.2023.10362217

Development of a Hardware-in-the-Loop Testbed for Distributed Electric Propulsion System in All-Electric Aircraft

Abstract

Publication series

Conference

UN SDGs

Keywords

Access to Document

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