Stability Analysis and Energy Management of a Novel Electric Power System Unit in All-Electric Aircraft

Qidong Wen; Zhe Liang; Lishi Zhang; Deliang Liang; Yang Liang; Shuzhou Yang

doi:10.1109/ECCE53617.2023.10362594

Stability Analysis and Energy Management of a Novel Electric Power System Unit in All-Electric Aircraft

Qidong Wen
, Zhe Liang
, Lishi Zhang
, Deliang Liang
, Yang Liang
, Shuzhou Yang

School of Electrical Engineering

Xi'an Jiaotong University

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

2 Scopus citations

Abstract

All-electric aircraft (AEA) power system architecture design is a major area of interest within the field of aviation industry. A critical issue when considering AEA power system architecture design is to ensure high reliability. To address this issue, this paper presents a novel electric power system unit that including a battery, a supercapacitor (SC), dual active bridge (DAB) converters, and a dual three phase (DTP) permanent magnet synchronous motor (PMSM) system. The proposed system unit features a high reliability due to the fault tolerance of the DTP-PMSM system and the isolation of the DAB, as well as a high-power transmission rating of the DAB. Furthermore, a complete power system can be derived by combining multiple units with optimal design. Apart from power system architecture design, a decentralized mixed droop control method is proposed to allocate different frequency power to battery and SC. In addition, corresponding impedance-based stability analysis is conducted to ensure system stability. Finally, the simulation results validate the stability of the system in various circumstances and the efficacy of the proposed control method.

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	1857-1862
Number of pages	6
ISBN (Electronic)	9798350316445
DOIs	https://doi.org/10.1109/ECCE53617.2023.10362594
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

All-electric aircraft (AEA)
dual three phase PMSM system
mixed droop control method
stability analysis theory

Access to Document

10.1109/ECCE53617.2023.10362594

Cite this

Wen, Q., Liang, Z., Zhang, L., Liang, D., Liang, Y., & Yang, S. (2023). Stability Analysis and Energy Management of a Novel Electric Power System Unit in All-Electric Aircraft. In 2023 IEEE Energy Conversion Congress and Exposition, ECCE 2023 (pp. 1857-1862). (2023 IEEE Energy Conversion Congress and Exposition, ECCE 2023). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/ECCE53617.2023.10362594

@inproceedings{086a5f58517248a897739048a6102a31,

title = "Stability Analysis and Energy Management of a Novel Electric Power System Unit in All-Electric Aircraft",

abstract = "All-electric aircraft (AEA) power system architecture design is a major area of interest within the field of aviation industry. A critical issue when considering AEA power system architecture design is to ensure high reliability. To address this issue, this paper presents a novel electric power system unit that including a battery, a supercapacitor (SC), dual active bridge (DAB) converters, and a dual three phase (DTP) permanent magnet synchronous motor (PMSM) system. The proposed system unit features a high reliability due to the fault tolerance of the DTP-PMSM system and the isolation of the DAB, as well as a high-power transmission rating of the DAB. Furthermore, a complete power system can be derived by combining multiple units with optimal design. Apart from power system architecture design, a decentralized mixed droop control method is proposed to allocate different frequency power to battery and SC. In addition, corresponding impedance-based stability analysis is conducted to ensure system stability. Finally, the simulation results validate the stability of the system in various circumstances and the efficacy of the proposed control method.",

keywords = "All-electric aircraft (AEA), dual three phase PMSM system, mixed droop control method, stability analysis theory",

author = "Qidong Wen and Zhe Liang and Lishi Zhang and Deliang Liang and Yang Liang and Shuzhou Yang",

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/ECCE53617.2023.10362594",

language = "英语",

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

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

pages = "1857--1862",

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

}

Wen, Q, Liang, Z, Zhang, L, Liang, D, Liang, Y & Yang, S 2023, Stability Analysis and Energy Management of a Novel Electric Power System Unit 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. 1857-1862, 2023 IEEE Energy Conversion Congress and Exposition, ECCE 2023, Nashville, United States, 29/10/23. https://doi.org/10.1109/ECCE53617.2023.10362594

Stability Analysis and Energy Management of a Novel Electric Power System Unit in All-Electric Aircraft. / Wen, Qidong; Liang, Zhe; Zhang, Lishi et al.
2023 IEEE Energy Conversion Congress and Exposition, ECCE 2023. Institute of Electrical and Electronics Engineers Inc., 2023. p. 1857-1862 (2023 IEEE Energy Conversion Congress and Exposition, ECCE 2023).

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

TY - GEN

T1 - Stability Analysis and Energy Management of a Novel Electric Power System Unit in All-Electric Aircraft

AU - Wen, Qidong

AU - Liang, Zhe

AU - Zhang, Lishi

AU - Liang, Deliang

AU - Liang, Yang

AU - Yang, Shuzhou

PY - 2023

Y1 - 2023

N2 - All-electric aircraft (AEA) power system architecture design is a major area of interest within the field of aviation industry. A critical issue when considering AEA power system architecture design is to ensure high reliability. To address this issue, this paper presents a novel electric power system unit that including a battery, a supercapacitor (SC), dual active bridge (DAB) converters, and a dual three phase (DTP) permanent magnet synchronous motor (PMSM) system. The proposed system unit features a high reliability due to the fault tolerance of the DTP-PMSM system and the isolation of the DAB, as well as a high-power transmission rating of the DAB. Furthermore, a complete power system can be derived by combining multiple units with optimal design. Apart from power system architecture design, a decentralized mixed droop control method is proposed to allocate different frequency power to battery and SC. In addition, corresponding impedance-based stability analysis is conducted to ensure system stability. Finally, the simulation results validate the stability of the system in various circumstances and the efficacy of the proposed control method.

AB - All-electric aircraft (AEA) power system architecture design is a major area of interest within the field of aviation industry. A critical issue when considering AEA power system architecture design is to ensure high reliability. To address this issue, this paper presents a novel electric power system unit that including a battery, a supercapacitor (SC), dual active bridge (DAB) converters, and a dual three phase (DTP) permanent magnet synchronous motor (PMSM) system. The proposed system unit features a high reliability due to the fault tolerance of the DTP-PMSM system and the isolation of the DAB, as well as a high-power transmission rating of the DAB. Furthermore, a complete power system can be derived by combining multiple units with optimal design. Apart from power system architecture design, a decentralized mixed droop control method is proposed to allocate different frequency power to battery and SC. In addition, corresponding impedance-based stability analysis is conducted to ensure system stability. Finally, the simulation results validate the stability of the system in various circumstances and the efficacy of the proposed control method.

KW - All-electric aircraft (AEA)

KW - dual three phase PMSM system

KW - mixed droop control method

KW - stability analysis theory

UR - https://www.scopus.com/pages/publications/85182930458

U2 - 10.1109/ECCE53617.2023.10362594

DO - 10.1109/ECCE53617.2023.10362594

M3 - 会议稿件

AN - SCOPUS:85182930458

T3 - 2023 IEEE Energy Conversion Congress and Exposition, ECCE 2023

SP - 1857

EP - 1862

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

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 2023 IEEE Energy Conversion Congress and Exposition, ECCE 2023

Y2 - 29 October 2023 through 2 November 2023

ER -

Wen Q, Liang Z, Zhang L, Liang D, Liang Y, Yang S. Stability Analysis and Energy Management of a Novel Electric Power System Unit in All-Electric Aircraft. In 2023 IEEE Energy Conversion Congress and Exposition, ECCE 2023. Institute of Electrical and Electronics Engineers Inc. 2023. p. 1857-1862. (2023 IEEE Energy Conversion Congress and Exposition, ECCE 2023). doi: 10.1109/ECCE53617.2023.10362594

Stability Analysis and Energy Management of a Novel Electric Power System Unit in All-Electric Aircraft

Abstract

Publication series

Conference

UN SDGs

Keywords

Access to Document

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