Modeling and stability enhancement of a permanent magnet synchronous generator based DC system for More Electric Aircraft
The concept of the More Electric Aircraft (MEA) is aimed at electrifying the mechanical, hydraulic, and pneumatic subsystems on aircraft. With increasing usage of power electronics, the architecture of on-board electrical power distribution systems (EPDS) becomes more complicated. Therefore, it is n...
| Main Authors: | , , , , , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Institute of Electrical and Electronics Engineers Inc.
2021
|
| Subjects: | |
| Online Access: | https://eprints.nottingham.ac.uk/65092/ |
| _version_ | 1848800185540411392 |
|---|---|
| author | Yang, Jiajun Yan, Hao Gu, Chunyang Wang, Shuo Zhao, Weiduo Wheeler, Patrick Buticchi, Giampaolo |
| author_facet | Yang, Jiajun Yan, Hao Gu, Chunyang Wang, Shuo Zhao, Weiduo Wheeler, Patrick Buticchi, Giampaolo |
| author_sort | Yang, Jiajun |
| building | Nottingham Research Data Repository |
| collection | Online Access |
| description | The concept of the More Electric Aircraft (MEA) is aimed at electrifying the mechanical, hydraulic, and pneumatic subsystems on aircraft. With increasing usage of power electronics, the architecture of on-board electrical power distribution systems (EPDS) becomes more complicated. Therefore, it is necessary to analyze the stability of the system. This paper firstly presents and validates an impedance model of a permanent magnet synchronous generator (PMSG) as a source and dual active bridge (DAB) converter as a load. These models are used for the stability analysis of a simple DC power system. In addition, two new control strategies are proposed to enhance the stability of the system. The stabilization effects of the new control strategies are verified with experimental results. |
| first_indexed | 2025-11-14T20:47:33Z |
| format | Article |
| id | nottingham-65092 |
| institution | University of Nottingham Malaysia Campus |
| institution_category | Local University |
| language | English |
| last_indexed | 2025-11-14T20:47:33Z |
| publishDate | 2021 |
| publisher | Institute of Electrical and Electronics Engineers Inc. |
| recordtype | eprints |
| repository_type | Digital Repository |
| spelling | nottingham-650922021-04-12T07:02:45Z https://eprints.nottingham.ac.uk/65092/ Modeling and stability enhancement of a permanent magnet synchronous generator based DC system for More Electric Aircraft Yang, Jiajun Yan, Hao Gu, Chunyang Wang, Shuo Zhao, Weiduo Wheeler, Patrick Buticchi, Giampaolo The concept of the More Electric Aircraft (MEA) is aimed at electrifying the mechanical, hydraulic, and pneumatic subsystems on aircraft. With increasing usage of power electronics, the architecture of on-board electrical power distribution systems (EPDS) becomes more complicated. Therefore, it is necessary to analyze the stability of the system. This paper firstly presents and validates an impedance model of a permanent magnet synchronous generator (PMSG) as a source and dual active bridge (DAB) converter as a load. These models are used for the stability analysis of a simple DC power system. In addition, two new control strategies are proposed to enhance the stability of the system. The stabilization effects of the new control strategies are verified with experimental results. Institute of Electrical and Electronics Engineers Inc. 2021-03-23 Article PeerReviewed application/pdf en cc_by https://eprints.nottingham.ac.uk/65092/1/Modeling%20and%20Stability%20Enhancement%20of%20a%20Permanent%20Magnet%20Synchronous%20Generator%20Based%20DC%20System%20for%20More%20Electric%20Aircraft.pdf Yang, Jiajun, Yan, Hao, Gu, Chunyang, Wang, Shuo, Zhao, Weiduo, Wheeler, Patrick and Buticchi, Giampaolo (2021) Modeling and stability enhancement of a permanent magnet synchronous generator based DC system for More Electric Aircraft. IEEE Transactions on Industrial Electronics . p. 1. ISSN 0278-0046 DC microgrid; more electric aircraft; impedance; stability analysis; permanent magnet synchronous generator; dual active bridge converter http://dx.doi.org/10.1109/TIE.2021.3066934 doi:10.1109/TIE.2021.3066934 doi:10.1109/TIE.2021.3066934 |
| spellingShingle | DC microgrid; more electric aircraft; impedance; stability analysis; permanent magnet synchronous generator; dual active bridge converter Yang, Jiajun Yan, Hao Gu, Chunyang Wang, Shuo Zhao, Weiduo Wheeler, Patrick Buticchi, Giampaolo Modeling and stability enhancement of a permanent magnet synchronous generator based DC system for More Electric Aircraft |
| title | Modeling and stability enhancement of a permanent magnet synchronous generator based DC system for More Electric Aircraft |
| title_full | Modeling and stability enhancement of a permanent magnet synchronous generator based DC system for More Electric Aircraft |
| title_fullStr | Modeling and stability enhancement of a permanent magnet synchronous generator based DC system for More Electric Aircraft |
| title_full_unstemmed | Modeling and stability enhancement of a permanent magnet synchronous generator based DC system for More Electric Aircraft |
| title_short | Modeling and stability enhancement of a permanent magnet synchronous generator based DC system for More Electric Aircraft |
| title_sort | modeling and stability enhancement of a permanent magnet synchronous generator based dc system for more electric aircraft |
| topic | DC microgrid; more electric aircraft; impedance; stability analysis; permanent magnet synchronous generator; dual active bridge converter |
| url | https://eprints.nottingham.ac.uk/65092/ https://eprints.nottingham.ac.uk/65092/ https://eprints.nottingham.ac.uk/65092/ |