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Article | Open Access

PRIME: A Physics-Guided Residual Integrated Framework for Multi-Task Aircraft Engine Diagnostics

Ouail Mjahed1( )Soukaina Mjahed2
Faculty of Sciences and Technology, Department of Computer Sciences, L2IS Laboratory, Cadi Ayyad University, Marrakech, Morocco
Faculty of Sciences Semlalia, Department of Computer Sciences, LISI Laboratory, Cadi Ayyad University, Marrakech, Morocco
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Abstract

Accurate aircraft engine diagnostics is essential for ensuring operational safety and enabling predictive maintenance under heterogeneous operating conditions. Although deep learning models can effectively capture high-dimensional multivariate sensor dynamics, purely data-driven approaches often entangle operating-condition variability with degradation-sensitive patterns, which limits robustness and generalization. This paper introduces PRIME, a physics-guided residual integrated framework for multi-task aircraft engine diagnostics. Rather than embedding explicit thermodynamic equations or physical constraints into the optimization process, PRIME relies on a physically motivated residual decomposition strategy that separates operating-condition-driven nominal behavior from degradation-sensitive sensor deviations. Specifically, nominal responses are estimated from operating-condition representations and subtracted from observed sensor signals to isolate fault-relevant residual patterns. These residual representations are then processed by a hybrid temporal architecture combining temporal convolutional networks and transformer-based self-attention, enabling joint modeling of local degradation signatures and long-range temporal dependencies. Within a unified optimization framework, PRIME simultaneously performs Fault Detection (FD), Fault Type Classification (FTC), and Health State Estimation (HSE). Extensive experiments on NASA C-MAPSS, N-CMAPSS, and the ALFA dataset show consistent and statistically significant improvements over strong baseline models. For FD and FTC, PRIME achieves gains of approximately 2%–4% over the strongest neural baselines evaluated under the same protocol, with larger margins over classical machine learning approaches. For HSE, PRIME yields more faithful degradation trajectories, leading to systematic reductions in estimation error across single- and multi-regime datasets. When Remaining Useful Life (RUL) is projected from the learned health trajectory through a threshold-based mechanism, the resulting estimates also improve substantially, with RMSE reductions of up to about 22% under complex operating conditions. These results show that physics-guided residual disentanglement improves robustness, interpretability, and multi-task diagnostic performance. More broadly, they support the view that HSE provides a useful latent degradation representation for downstream prognostic assessment, even though RUL is not directly optimized by the model.

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Computer Modeling in Engineering & Sciences
Article number: 14

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Cite this article:
Mjahed O, Mjahed S. PRIME: A Physics-Guided Residual Integrated Framework for Multi-Task Aircraft Engine Diagnostics. Computer Modeling in Engineering & Sciences, 2026, 147(3): 14. https://doi.org/10.32604/cmes.2026.083272

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Received: 31 March 2026
Accepted: 14 May 2026
Published: 30 June 2026
© The Author 2026.

This work is licensed under a Creative Commons Attribution 4.0 International License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.