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Publishing Language: Chinese

Optimal design of hydrogen-powered UAV based on multi-source domain fusion surrogate model

Rongzu LI, Li LIU( ), Dun YANG
School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China
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Abstract

This paper addresses the optimization problem of the overall design stage of Hydrogen-powered Unmanned Aerial Vehicles (H-UAVs) in the context of heterogeneous multi-source domains. It explores how to effectively utilize the transfer learning technology to establish a surrogate model and optimize H-UAVs in the presence of heterogeneous samples. To solve the problem of high cost of building a surrogate model due to heterogeneous samples during the evolution of hydrogen-powered UAVs, a framework for establishing a Multi-Source domain Fusion (DG-MSF) surrogate model is proposed based on Data Generation. The geodesic flow kernel method is used to map the heterogeneous source and target domains to a high-dimensional space to determine the relationship between multi-source domains. The marginal distribution-based data generation method is used to effectively integrate source domain information. A multi-layer perceptron neural network is built as a surrogate model, and is trained and fine-tuned through pre-training and fine-tuning methods to achieve efficient prediction of performance of H-UAVs. Finally, the optimization design of the H-UAV is carried out. The analysis results show that the proposed method can effectively utilize multi-source domain data to improve the efficiency of model training and prediction accuracy and the overall performance of H-UAVs, providing powerful technical support for the development of H-UAVs.

CLC number: V221+.6 Document code: A Article ID: 1000-6893(2025)09-630979-13

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Acta Aeronautica et Astronautica Sinica

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Cite this article:
LI R, LIU L, YANG D. Optimal design of hydrogen-powered UAV based on multi-source domain fusion surrogate model. Acta Aeronautica et Astronautica Sinica, 2025, 46(9). https://doi.org/10.7527/S1000-6893.2024.30979

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Received: 22 July 2024
Revised: 10 October 2024
Accepted: 22 November 2024
Published: 06 December 2024
© 2025 The Journal of Acta Aeronautica et Astronautica Sinica