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An adaptive physics-informed graph neural network-based method for aero-engine gas path estimation
DOI:10.1016/j.ast.2026.113604.png)
Abstract
En 中文
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Customized architecture tailored for aero-engine characteristics.
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Directed topology graphs encode physical information explicitly.
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Explicit memory units preserve critical temporal information.
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Different flight phases are processed through separate channels.
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Efficient parameter updates mitigate performance degradation.
Journal
IF:
5.8
Papers:
1.0W
Citations:
3.0W
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