Power management control and delivery module for a hybrid electric aircraft using fuel cell and battery

Author:

Hoenicke Pia,Ghosh Debjani,Muhandes Adel,Bhattacharya Sumantra,Bauer Christiane,Kallo Josef,Willich Caroline

Funder

European Commission

Publisher

Elsevier BV

Subject

Energy Engineering and Power Technology,Fuel Technology,Nuclear Energy and Engineering,Renewable Energy, Sustainability and the Environment

Reference23 articles.

Cited by 35 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Constrained exploration method for optimal energy management in hybrid multi-stack fuel cell vehicles;Energy Conversion and Management;2024-09

2. Optimizing the control strategy of redundant motor-inverter systems for aircraft propulsion application;Journal of Physics: Conference Series;2024-06-01

3. Optimal Sizing of Fuel Cell and Battery in a Direct-Hybrid for Electric Aircraft;Aerospace;2024-02-23

4. Analysis of Power Losses and Evaluation Model for SiC MOSFET-based Triple Active Bridge Converter in Hybrid Electric Aircraft Applications;2024 International Conference on Artificial Intelligence, Computer, Data Sciences and Applications (ACDSA);2024-02-01

5. Power Management Control for Hybrid Electric Aircraft Propulsion Drive Based on Triple Active Bridge DC-DC Converter;2024 International Conference on Artificial Intelligence, Computer, Data Sciences and Applications (ACDSA);2024-02-01

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