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Full Length Article | Open Access

Digital twin dynamic-polymorphic uncertainty surrogate model generation using a sparse polynomial chaos expansion with application in aviation hydraulic pump

Dong LIUa,bShaoping WANGa,b( )Jian SHIa,bDi LIUa,b
School of Automation Science and Electrical Engineering, Beihang University, Beijing 100191, China
Tianmushan Laboratory, Hangzhou 310023, China

Peer review under responsibility of Editorial Committee of CJA

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Abstract

Full lifecycle high fidelity digital twin is a complex model set contains multiple functions with high dimensions and multiple variables. Quantifying uncertainty for such complex models often encounters time-consuming challenges, as the number of calculated terms increases exponentially with the dimensionality of the input. This paper based on the multi-stage model and high time consumption problem of digital twins, proposed a sparse polynomial chaos expansions method to generate the digital twin dynamic-polymorphic uncertainty surrogate model, striving to strike a balance between the accuracy and time consumption of models used for digital twin uncertainty quantification. Firstly, an analysis and clarification were conducted on the dynamic-polymorphic uncertainty of the full lifetime running digital twins. Secondly, a sparse polynomial chaos expansions model response was developed based on partial least squares technology with the effectively quantified and selected basis polynomials which sorted by significant influence. In the end, the accuracy of the proxy model is evaluated by leave-one-out cross-validation. The effectiveness of this method was verified through examples, and the results showed that it achieved a balance between maintaining model accuracy and complexity.

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Chinese Journal of Aeronautics
Pages 231-244

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Cite this article:
LIU D, WANG S, SHI J, et al. Digital twin dynamic-polymorphic uncertainty surrogate model generation using a sparse polynomial chaos expansion with application in aviation hydraulic pump. Chinese Journal of Aeronautics, 2024, 37(12): 231-244. https://doi.org/10.1016/j.cja.2024.10.008

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Received: 01 March 2024
Revised: 06 April 2024
Accepted: 23 June 2024
Published: 16 October 2024
© 2024 Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY license (http://creativecommons.org/licenses/by/4.0/).