An Intelligent Fault Diagnosis Method for General Aviation Aircraft Based on Multi-Fidelity Digital Twin and FMEA Knowledge Enhancement
Zhihuan Wei, Yang Hu, Xinhang Chen, Yiming Zhang, Jie Liu, Wei Wang

TL;DR
This paper introduces an advanced fault diagnosis framework for general aviation aircraft using multi-fidelity digital twins, FMEA knowledge, and LLMs to improve accuracy, interpretability, and real-time performance.
Contribution
It develops a novel multi-fidelity residual computation framework and integrates LLMs with FMEA knowledge for interpretable fault diagnosis reports.
Findings
Paired-mirror residual scheme achieves 96.2% Macro-F1 on 20 fault classes.
GRU surrogate reduces inference time by 4.3x with minimal performance loss.
Residual feature quality impacts diagnosis more than classifier architecture.
Abstract
Fault diagnosis of general aviation aircraft faces challenges including scarce real fault data, diverse fault types, and weak fault signatures. This paper proposes an intelligent fault diagnosis framework based on multi-fidelity digital twin, integrating four modules: high-fidelity flight dynamics simulation, FMEA-driven fault injection, multi-fidelity residual feature extraction, and large language model (LLM)-enhanced interpretable report generation. A digital twin is constructed using the JSBSim six-degree-of-freedom (6-DoF) flight dynamics engine, generating 23-channel engine health monitoring data via semi-empirical sensor synthesis equations. A three-layer fault injection engine based on failure mode and effects analysis (FMEA) models the physical causal propagation of 19 engine fault types. A multi-fidelity residual computation framework comprising paired-mirror residuals and GRU…
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