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Publishing Language: Chinese

Research progress and key technologies of hydrogen fuel cell UAVs

Weiqiang XU1,2( ), Bingxin ZHANG2, He ZHU1, Li CHEN3
Tianmushan Laboratory,Hangzhou 311115,China
School of Aeronautic Science and Engineering,Beihang University,Beijing 100191,China
School of Energy and Power Engineering,Xi’an Jiaotong University,Xi’an 710049,China
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Abstract

Due to their high energy density and zero emissions, hydrogen fuel cell UAVs have become a vital means of overcoming the endurance limitations of traditional lithium-battery-powered UAVs in the context of a growing low-altitude economy and the development of green aviation. This paper provides a comprehensive review and systematic categorization of the development and key technologies of hydrogen-fuel cell UAVs, along with a reasonable outlook on their future evolution, to serve as a valuable reference for related research. In particular, the paper starts with a summary of the scientific advancements and developmental history of hydrogen-powered aircraft, the inherent benefits of hydrogen fuel cell powertrain systems, and the state of the art in hydrogen fuel cell unmanned aerial vehicles. Subsequently, a systematic analysis is conducted on the core technologies involved in hydrogen fuel cell UAVs, including hydrogen fuel cell technology, multi-source hybrid energy systems, airborne hydrogen storage technology, energy management strategies, and thermal management strategies. Lastly, a summary of the study’s significant findings is provided, and future research directions are indicated by matching the state of these important technologies' research with the real-world difficulties they face.

CLC number: V279 Document code: A Article ID: 1001-5965(2026)10-3563-17

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Journal of Beijing University of Aeronautics and Astronautics
Pages 3563-3579

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Cite this article:
XU W, ZHANG B, ZHU H, et al. Research progress and key technologies of hydrogen fuel cell UAVs. Journal of Beijing University of Aeronautics and Astronautics, 2026, 52(10): 3563-3579. https://doi.org/10.13700/j.bh.1001-5965.2026.0440

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Received: 29 June 2026
Accepted: 21 August 2026
Published: 28 August 2026
© Journal of Beijing University of Aeronautics and Astronautics