The research, led by Anuj Mangal of GLA University in Mathura, India, together with colleagues from several Indian engineering institutions, tackles a persistent gap in aviation diagnostics. Deep learning has transformed fields such as object identification and computer vision over the past decade, and convolutional neural networks have recently surged in popularity for diagnosing rotating machinery of all kinds. Yet gas turbine diagnosis remains an area where these powerful techniques have seen comparatively limited adoption. The authors argue that the complexity of engine thermodynamics, the sheer variety of operating conditions, and the difficulty of obtaining labeled fault data have all slowed progress, and their framework is an attempt to close that gap with tools that are both data-driven and grounded in engine physics.

At the heart of the approach is a two-stage architecture. The first stage is a physics-driven efficiency trend-monitoring system that tracks how engine performance degrades over time. Rather than waiting for a hard failure, the system continuously compares observed sensor readings against expected values, records degradation-related performance changes, and creates a new performance baseline whenever the engine’s condition shifts in a lasting way. This baseline management is critical, because an engine that has slowly lost a fraction of its efficiency through normal wear is not malfunctioning, while a sudden deviation from the current baseline may signal a genuine fault. The trend monitor also produces fault signatures, the characteristic patterns that specific gas path problems leave in the sensor data.

Those physics-based fault signatures then serve a second purpose: they train the fault detection and isolation system. Because real engine failures are rare and dangerous, researchers cannot simply wait for engines to break in order to gather training data. By using a physics-based model to generate realistic fault signatures for a range of gas path problems, the team could teach their diagnostic networks to recognize and categorize faults at the component level, distinguishing, for example, between degradation in a compressor and trouble in a turbine. This marriage of simulation and machine learning is a growing trend in aerospace engineering, where digital models supply the labeled examples that real-world operations cannot provide safely or economically.

The second stage of the framework is built around a radial basis function, or RBF, neural network, a type of network whose hidden neurons respond to inputs based on their distance from learned center points. RBF networks are prized for fast training and strong local approximation abilities, making them well suited to mapping the nonlinear relationships between engine sensor readings and engine health. The proposed pipeline integrates sensor-based degradation indicators with normalization, sliding window feature extraction, and outlier detection, a sequence designed to improve prediction reliability when raw data are noisy or incomplete. Sliding windows allow the network to see not just instantaneous readings but the shape of their evolution over time, which is often where degradation reveals itself first.

To evaluate the system rigorously, the researchers turned to the NASA C-MAPSS turbofan engine simulation dataset, a widely used benchmark that models the behavior of a three-shaft turbofan under realistic operating profiles. Crucially, the team deliberately tested their methods under conditions of substantial measurement noise to guarantee model robustness, since real aircraft sensors rarely deliver clean signals. Multiple failure scenarios were simulated, and the fault detection and isolation performance was assessed against a convolutional neural network-based classification approach and a deep long short-term memory, or LSTM, method, allowing a direct comparison of how different neural architectures handle the same diagnostic task.

The results were measured using root mean square error, or RMSE, along with score and average score metrics, the standard yardsticks in the remaining useful life prediction community. The proposed RBF neural network model achieved improved prediction performance compared with conventional approaches such as multilayer perceptrons and support vector machines. In practical terms, that means the network could estimate how much useful life remained in an engine more accurately, giving maintenance planners a tighter, more trustworthy window in which to schedule inspections and part replacements. Accurate remaining useful life estimation is one of the central goals of prognostics, because it converts maintenance from a calendar-driven ritual into a condition-driven decision.

The study also introduces a dedicated health assessment model built around exhaust gas temperature, one of the most telling indicators of gas turbine condition. An artificial neural network was used to identify the EGT parameter, while multiple regression analysis quantified how flight factors influence it. By the end of the research, the team had constructed a network capable of forecasting the EGT variable with minimal error. The engine’s state can be monitored instantly through an interface created in MATLAB Simulink, where performance degradation appears as a numerical value or a graphical representation that is easy to interpret. The authors even suggest the model may serve as a new kind of indicator that alerts pilots when the EGT sensor itself develops a fault in flight, a sensor-of-sensors safeguard that could add another layer of redundancy to cockpit instrumentation.

The motivation behind all of this is threefold: reduce fuel consumption, improve aircraft safety, and lower maintenance costs. Engines that run efficiently burn less fuel, and fuel is one of the largest operating expenses for any airline. Early fault detection prevents small defects from cascading into in-flight shutdowns or unscheduled landings. And condition-based maintenance, in which components are serviced when their actual condition warrants it rather than on fixed schedules, can trim billions from global maintenance budgets while keeping aircraft in revenue service longer. Performance degradation in gas turbine engines, as the literature defines it, is a function of vibration, oil pressure, motor fan velocity, oil temperatures, exhaust gas temperature, and fuel flow, and the framework monitors precisely these channels.

The broader significance of the work lies in its demonstration that hybrid approaches, pairing physics-based models with neural networks, can outperform purely data-driven methods in domains where training data are scarce and safety margins are unforgiving. As aviation moves toward more autonomous health management systems, and as digital twins of individual engines become standard practice, frameworks like the one described here may become as routine a part of an airliner’s ground infrastructure as the weather radar. The next time a flight lands smoothly and the passengers disembark unaware, there is a reasonable chance that a network of artificial neurons has already been quietly reviewing the engine’s every breath, deciding whether it is fit to fly again tomorrow.

Subject of Research: Machine learning-based performance monitoring and fault diagnosis of aircraft gas turbine engines

Article Title: Performance Monitoring and Fault Diagnosis of Aircraft Engines via RBF Neural Network Models

Article References: Mangal, A., Sanmugam, S., Alagarsamy, M., Murugan, J. S., Kuppusamy, S., & Rajaram, A. (2026). Performance Monitoring and Fault Diagnosis of Aircraft Engines via RBF Neural Network Models. International Journal of Aeronautical and Space Sciences. https://doi.org/10.1007/s42405-026-01225-4

Image Credits: AI Generated

DOI: 10.1007/s42405-026-01225-4

Keywords: aircraft engines, gas turbines, RBF neural network, fault diagnosis, engine health monitoring, remaining useful life, NASA C-MAPSS, exhaust gas temperature, machine learning, turbofan, predictive maintenance, convolutional neural networks