Intelligent multi-fault diagnosis for a simplified aircraft fuel system

Date published

2025-02-01

Free to read from

2025-03-04

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Journal Title

Journal ISSN

Volume Title

Publisher

MDPI

Department

Type

Article

ISSN

1999-4893

Format

Citation

Li J, King S, Jennions I. (2025) Intelligent multi-fault diagnosis for a simplified aircraft fuel system. Algorithms, Volume 18, Issue 2, February 2025, Article number 73

Abstract

Machine learning (ML) techniques are increasingly used to diagnose faults in aerospace applications, but diagnosing multiple faults in aircraft fuel systems (AFSs) remains challenging due to complex component interactions. This paper evaluates the accuracy and introduces an innovative approach to quantify and compare the interpretability of four ML classification methods—artificial neural networks (ANNs), support vector machines (SVMs), decision trees (DTs), and logistic regressions (LRs)—for diagnosing fault combinations present in AFSs. While the ANN achieved the highest diagnostic accuracy at 90%, surpassing other methods, its interpretability was limited. By contrast, the decision tree model showed an 82% consistency between global explanations and engineering insights, highlighting its advantage in interpretability despite the lower accuracy. Interpretability was assessed using two widely accepted tools, LIME and SHAP, alongside engineering understanding. These findings underscore a trade-off between prediction accuracy and interpretability, which is critical for trust in ML applications in aerospace. Although an ANN can deliver high diagnostic accuracy, a decision tree offers more transparent results, facilitating better alignment with engineering expectations even at a slight cost to accuracy.

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Software Description

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Github

Keywords

46 Information and Computing Sciences, 40 Engineering, 4001 Aerospace Engineering, Machine Learning and Artificial Intelligence, 40 Engineering, 46 Information and computing sciences, 49 Mathematical sciences

DOI

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Attribution 4.0 International

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