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An adaptive physics-informed graph neural network-based method for aero-engine gas path estimation

delete2026-08-22
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DOI:10.1016/j.ast.2026.113604delete
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Abstract

Abstract

En 中文
• Customized architecture tailored for aero-engine characteristics. • Directed topology graphs encode physical information explicitly. • Explicit memory units preserve critical temporal information. • Different flight phases are processed through separate channels. • Efficient parameter updates mitigate performance degradation.

Journal

Aerospace Science and Technology cover
Aerospace Science and Technology
IF:
5.8
Papers:
1.0W
Citations:
3.0W

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