Aeroengine Performance Prediction Using a Physical-Embedded Data-Driven Method

Accurate and efficient prediction of aeroengine performance is of paramount importance for engine design, maintenance, and optimization endeavours. However, existing methodologies often struggle to strike an optimal balance among predictive accuracy, computational efficiency, modelling complexity, and data dependency. To address these challenges, we propose a strategy that synergistically combines domain knowledge from both the aeroengine and neural network realms to enable real-time prediction of engine performance parameters. Leveraging aeroengine domain knowledge, we judiciously design the network structure and regulate the internal information flow. Concurrently, drawing upon neural network domain expertise, we devise four distinct feature fusion methods and introduce an innovative loss function formulation. To rigorously evaluate the effectiveness and robustness of our proposed strategy, we conduct comprehensive validation across two distinct datasets. The empirical results demonstrate :(1) the evident advantages of our tailored loss function; (2) our model's ability to maintain equal or superior performance with a reduced parameter count; (3) our model's reduced data dependency compared to generalized neural network architectures; (4)Our model offers potential interpretability advantages compared to some conventional machine learning approaches.

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Publication Details

Journal
IEEE Transactions on Aerospace and Electronic Systems
Published
2025-05-28
DOI
https://doi.org/10.1109/taes.2025.3574667
Citations
3
Primary Topic
Aerospace and Aviation Technology
Type
article
Field-Weighted Citation Impact
14.98
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article

Aeroengine Performance Prediction Using a Physical-Embedded Data-Driven Method

Shuxiao Li, Xiaomeng Zhu, Tong Mo, Shiran Dai et al.
3 citations
IEEE Transactions on Aerospace and Electronic Systems
Aerospace and Aviation Technology
14.98
article

Aeroengine Performance Prediction Using a Physical-Embedded Data-Driven Method

Shuxiao Li, Xiaomeng Zhu, Tong Mo, Shiran Dai, An Fu
article en
3 citations

Abstract

Accurate and efficient prediction of aeroengine performance is of paramount importance for engine design, maintenance, and optimization endeavours. However, existing methodologies often struggle to strike an optimal balance among predictive accuracy, computational efficiency, modelling complexity, and data dependency. To address these challenges, we propose a strategy that synergistically combines domain knowledge from both the aeroengine and neural network realms to enable real-time prediction of engine performance parameters. Leveraging aeroengine domain knowledge, we judiciously design the network structure and regulate the internal information flow. Concurrently, drawing upon neural network domain expertise, we devise four distinct feature fusion methods and introduce an innovative loss function formulation. To rigorously evaluate the effectiveness and robustness of our proposed strategy, we conduct comprehensive validation across two distinct datasets. The empirical results demonstrate :(1) the evident advantages of our tailored loss function; (2) our model's ability to maintain equal or superior performance with a reduced parameter count; (3) our model's reduced data dependency compared to generalized neural network architectures; (4)Our model offers potential interpretability advantages compared to some conventional machine learning approaches.

IEEE Transactions on Aerospace and Electronic SystemsVol. 61(5)
Chinese Academy of Sciences (CN), Shandong Institute of Automation (CN), Institute of Automation (CN), University of Chinese Academy of Sciences (CN)
Openalex Percentile: Top 2%
Aerospace and Aviation Technology
14.98
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