Hybrid Power System Topology and Energy Management Scheme Design for Hydrogen-Powered Aircraft
文献类型：期刊论文
| 作者 | Li, Shuangqi1,2; Zhao, Pengfei3,4; Gu, Chenghong1; Bu, Siqi5,6; Pei, Xiaoze1,7; Zeng, Xianwu1,7; Li, Jianwei1 ; Cheng, Shuang1
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| 刊名 | IEEE TRANSACTIONS ON SMART GRID
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| 出版日期 | 2024-03-01 |
| 卷号 | 15期号:2页码:1201-1212 |
| 关键词 | Aircraft Batteries Topology Energy management Hydrogen Aircraft propulsion Power systems Transportation electrification electric aircraft hybrid energy storage system power system topology energy management strategy |
| ISSN号 | 1949-3053 |
| DOI | 10.1109/TSG.2023.3292088 |
| 通讯作者 | Gu, Chenghong(C.Gu@bath.ac.uk) |
| 英文摘要 | The electrification of the aviation industry is a major challenge to realizing net-zero in the global energy sector. Fuel cell (FC) hybrid electric aircraft (FCHEV) demonstrate remarkable competitiveness in terms of cruise range and total economy. However, the process of simply hybridizing different power supplies together does not lead to an improvement in the aircraft economy, since a carefully designed power system topology and energy management scheme are also necessary to realize the full benefit of FCHEV. This paper provides a new approach towards the configuration of the optimal power system and proposes a novel energy management scheme for FCHEA. Firstly, four different topologies of aircraft power systems are designed to facilitate flexible power flow control and energy management. Then, an equivalent model of aircraft hydrogen consumption is formulated by analyzing the FC efficiency, FC aging, and BESS aging. Using the newly established model, the performance of aircraft can be quantitatively evaluated in detail to guide FCHEA design. The optimal aircraft energy management is realized by establishing a mathematical optimization model with the reduction of hydrogen consumption and aging costs as objectives. An experimental aircraft, NASA X-57 Maxwell, is used to provide a detailed performance evaluation of different power system topologies and validate the effectiveness of the energy management scheme. The new approach represents a guide for future power system design and energy management of electric aircraft. |
| WOS关键词 | MODEL-PREDICTIVE CONTROL ; SPARSE IDENTIFICATION ; GOVERNING EQUATIONS ; STABILITY ANALYSIS ; VIRTUAL INERTIA ; INVERTER ; FILTER |
| WOS研究方向 | Engineering |
| 语种 | 英语 |
| WOS记录号 | WOS:001174148100001 |
| 出版者 | IEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INC |
| 源URL | [http://ir.ia.ac.cn/handle/173211/58015]  |
| 专题 | 舆论大数据科学与技术应用联合实验室 |
| 通讯作者 | Gu, Chenghong |
| 作者单位 | 1.Univ Bath, Dept Elect & Elect Engn, Bath BA2 7AY, Avon, England 2.Hong Kong Polytech Univ, Dept Elect Engn, Hong Kong, Peoples R China 3.Chinese Acad Sci, Inst Automat, Beijing 100090, Peoples R China 4.Univ Chinese Acad Sci, Sch Artificial Intelligence, Beijing 100190, Peoples R China 5.Hong Kong Polytech Univ, Dept Elect Engn, Shenzhen Res Inst, Ctr Adv Reliabil & Safety, Hong Kong, Peoples R China 6.Hong Kong Polytech Univ, Res Inst Smart Energy, Hong Kong, Peoples R China 7.Univ Bath, Inst Adv Automot Prop Syst, Bath BA2 7AY, Avon, England |
| 推荐引用方式 GB/T 7714 | Li, Shuangqi,Zhao, Pengfei,Gu, Chenghong,et al. Hybrid Power System Topology and Energy Management Scheme Design for Hydrogen-Powered Aircraft[J]. IEEE TRANSACTIONS ON SMART GRID,2024,15(2):1201-1212. |
| APA | Li, Shuangqi.,Zhao, Pengfei.,Gu, Chenghong.,Bu, Siqi.,Pei, Xiaoze.,...&Cheng, Shuang.(2024).Hybrid Power System Topology and Energy Management Scheme Design for Hydrogen-Powered Aircraft.IEEE TRANSACTIONS ON SMART GRID,15(2),1201-1212. |
| MLA | Li, Shuangqi,et al."Hybrid Power System Topology and Energy Management Scheme Design for Hydrogen-Powered Aircraft".IEEE TRANSACTIONS ON SMART GRID 15.2(2024):1201-1212. |
入库方式： OAI收割
来源：自动化研究所
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