Aircraft Jet Engine Health Monitoring Through System Identification Using Ensemble Neural Networks

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ISBN 13 :
Total Pages : 440 pages
Book Rating : 4.:/5 (111 download)

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Book Synopsis Aircraft Jet Engine Health Monitoring Through System Identification Using Ensemble Neural Networks by : Mahdiyeh Amozegar

Download or read book Aircraft Jet Engine Health Monitoring Through System Identification Using Ensemble Neural Networks written by Mahdiyeh Amozegar and published by . This book was released on 2015 with total page 440 pages. Available in PDF, EPUB and Kindle. Book excerpt: In this thesis a new approach for jet engine Fault Detection and Isolation (FDI) is proposed using ensemble neural networks. Ensemble methods combine various model predictions to reduce the modeling error and increase the prediction accuracy. By combining individual models, more robust and accurate representations are almost always achievable without the need of ad-hoc fine tunings that are required for single model-based solutions. For the purpose of jet engine health monitoring, the model of the jet engine dynamics is represented using three different stand-alone or individual neural network learning algorithms. Specifically, a dynamic multi-layer perceptron (MLP), a dynamic radial-basis function (RBF) neural network, and a dynamic support vector machine (SVM) are trained to individually model the jet engine dynamics. The accuracy of each stand-alone model in identification of the jet engine dynamics is evaluated. Next, three ensemble-based techniques are employed to represent jet engine dynamics. Namely, two heterogenous ensemble models (an ensemble model is heterogeneous when different learning algorithms (neural networks) are used for training its members) and a homogeneous ensemble model (all the models are generated using the same learning algorithm (neural network)). It is concluded that the ensemble models improve the modeling accuracy when compared to stand-alone solutions. The best selected stand-alone model (i.e the dynamic radial-basis function neural network in this application) and the best selected ensemble model (i.e. a heterogenous ensemble) in term of the jet engine modeling accuracy are selected for performing the FDI study. Engine residual signals are generated using both single model-based and ensemble-based solutions under various engine health conditions. The obtained residuals are evaluated in order to detect engine faults. Our simulation results demonstrate that the fault detection task using residuals that are obtained from the ensemble model results in more accurate performance. The fault isolation task is performed by evaluating variations in residual signals (before and after a fault detection flag) using a neural network classifier. As in the fault detection results, it is observed that the ensemble-based fault isolation task results in a more promising performance.

AIRCRAFT JET ENGINE CONDITION MONITORING THROUGH SYSTEM IDENTIFICATION BY USING GENETIC PROGRAMMING.

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ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (13 download)

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Book Synopsis AIRCRAFT JET ENGINE CONDITION MONITORING THROUGH SYSTEM IDENTIFICATION BY USING GENETIC PROGRAMMING. by : Seyedhossein Nayyeri

Download or read book AIRCRAFT JET ENGINE CONDITION MONITORING THROUGH SYSTEM IDENTIFICATION BY USING GENETIC PROGRAMMING. written by Seyedhossein Nayyeri and published by . This book was released on 2013 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Hybrid Neural Network-Genetic Algorithm Technique for Aircraft Engine Performance Diagnostics

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ISBN 13 :
Total Pages : 18 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis A Hybrid Neural Network-Genetic Algorithm Technique for Aircraft Engine Performance Diagnostics by : Takahisa Kobayashi

Download or read book A Hybrid Neural Network-Genetic Algorithm Technique for Aircraft Engine Performance Diagnostics written by Takahisa Kobayashi and published by . This book was released on 2001 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt: In this paper, a model-based diagnostic method, which utilizes Neural Networks and Genetic Algorithms, is investigated. Neural networks are applied to estimate the engine internal health, and Genetic Algorithms are applied for sensor bias detection and estimation. This hybrid approach takes advantage of the nonlinear estimation capability provided by neural networks while improving the robustness to measurement uncertainty through the application of Genetic Algorithms. The hybrid diagnostic technique also has the ability to rank multiple potential solutions for a given set of anomalous sensor measurements in order to reduce false alarms and missed detections. The performance of the hybrid diagnostic technique is evaluated through some case studies derived from a turbofan engine simulation. The results show this approach is promising for reliable diagnostics of aircraft engines.

Jet Engine Prognosis Using Dynamic Neural Networks

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ISBN 13 :
Total Pages : 382 pages
Book Rating : 4.:/5 (19 download)

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Book Synopsis Jet Engine Prognosis Using Dynamic Neural Networks by : Saba Kiakojoori

Download or read book Jet Engine Prognosis Using Dynamic Neural Networks written by Saba Kiakojoori and published by . This book was released on 2014 with total page 382 pages. Available in PDF, EPUB and Kindle. Book excerpt: Jet engine related costs and the need for high performance reliability have resulted in considerable interest in advanced health and condition-based maintenance techniques. This thesis attempts to design fault prognosis schemes for aircraft jet engine using intelligent-based methodologies to ensure flight safety and performance. Two different artificial neural networks namely, non-linear autoregressive neural network with exogenous input (NARX) and the Elman neural network are introduced for this purpose. The NARX neural network is constructed by using a tapped-delay line from the inputs and delayed connections from the output layer to the input layer to achieve a dynamic input-output map. Consequently, the current output becomes dependent on the delayed inputs and outputs. On the other hand, the Elman neural network uses the previous values of the hidden layer neurons to build memory in the system. Various degradations may occur in the engine resulting in changes in its components performance. Two main degradations, namely compressor fouling and turbine erosion are modelled under various degradation conditions. The proposed dynamic neural networks are developed and applied to capture the dynamics of these degradations in the jet engine. The health condition of the engine is then predicted subject to occurrence of these deteriorations. In both proposed approaches, various scenarios are considered and extensive simulations are conducted. For each of the scenarios, several neural networks are trained and their performances in predicting multi-flights ahead turbine output temperature are evaluated. The difference between each network output and the measured jet engine output are compared and the best neural network architecture is obtained. The most suitable neural network for prediction is selected by using normalized Bayesian information criterion model selection. Simulation results presented, demonstrate and illustrate the effective performance of the proposed neural network-based prediction and prognosis strategies.

Intelligent Based Aircraft Engine Health Monitoring

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Publisher : LAP Lambert Academic Publishing
ISBN 13 : 9783845419657
Total Pages : 132 pages
Book Rating : 4.4/5 (196 download)

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Book Synopsis Intelligent Based Aircraft Engine Health Monitoring by : Seref Demirci

Download or read book Intelligent Based Aircraft Engine Health Monitoring written by Seref Demirci and published by LAP Lambert Academic Publishing. This book was released on 2011-09 with total page 132 pages. Available in PDF, EPUB and Kindle. Book excerpt: Engine Health monitoring (EHM) has been very popular subject to increase aircraft availability with the minimum maintenance cost. The study is aimed at providing a method to monitor the aircraft engine health during the flight with the aim of providing an opportunity for early fault detection to improve airline maintenance effectiveness and reliability. Since the impending engine failures may cause to change the engine parameters such as Fuel Flow (FF), Exhaust Gas Temperature (EGT), engine fan speed (N1), engine compressor speed (N2), etc., engine deteriorations or faults may be identified before they occur by monitoring them. So as to monitor engine health in flight, the automation of current work for EHM done manually by airlines is developed by using fuzzy logic (FL) and neural network (NN) models. FL is selected to develop automated EHM system (AEHMS), since it is very useful method for automation health monitoring. The fuzzy rule inference system for different engine faults is based on the expert knowledge and real life data in Turkish Airlines fleet. The complete loop of EHM is automatically performed by the visual basic programs and Fuzzy Logic Toolbox in MATLAB.

Aircraft Health and Usage Monitoring Systems

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ISBN 13 :
Total Pages : 100 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Aircraft Health and Usage Monitoring Systems by : Institution of Mechanical Engineers (Great Britain)

Download or read book Aircraft Health and Usage Monitoring Systems written by Institution of Mechanical Engineers (Great Britain) and published by . This book was released on 1996 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt: These proceedings contain a selection of papers from the "Aerotech" event dealing with aircraft health and usage monitoring systems. The topics covered include analysis of usage data, vibration monitoring, neural networks, engine monitoring, predicting structural fatigue and fault diagnosis.

Aircraft Turbine Engine Monitoring Systems

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ISBN 13 :
Total Pages : 40 pages
Book Rating : 4.3/5 (9 download)

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Book Synopsis Aircraft Turbine Engine Monitoring Systems by : J. L. Birkler

Download or read book Aircraft Turbine Engine Monitoring Systems written by J. L. Birkler and published by . This book was released on 1979 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Prognostics and Health Management of Electronics

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Publisher : John Wiley & Sons
ISBN 13 : 1119515300
Total Pages : 800 pages
Book Rating : 4.1/5 (195 download)

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Book Synopsis Prognostics and Health Management of Electronics by : Michael G. Pecht

Download or read book Prognostics and Health Management of Electronics written by Michael G. Pecht and published by John Wiley & Sons. This book was released on 2018-08-15 with total page 800 pages. Available in PDF, EPUB and Kindle. Book excerpt: An indispensable guide for engineers and data scientists in design, testing, operation, manufacturing, and maintenance A road map to the current challenges and available opportunities for the research and development of Prognostics and Health Management (PHM), this important work covers all areas of electronics and explains how to: assess methods for damage estimation of components and systems due to field loading conditions assess the cost and benefits of prognostic implementations develop novel methods for in situ monitoring of products and systems in actual life-cycle conditions enable condition-based (predictive) maintenance increase system availability through an extension of maintenance cycles and/or timely repair actions; obtain knowledge of load history for future design, qualification, and root cause analysis reduce the occurrence of no fault found (NFF) subtract life-cycle costs of equipment from reduction in inspection costs, downtime, and inventory Prognostics and Health Management of Electronics also explains how to understand statistical techniques and machine learning methods used for diagnostics and prognostics. Using this valuable resource, electrical engineers, data scientists, and design engineers will be able to fully grasp the synergy between IoT, machine learning, and risk assessment.

Improving Aircraft Engine Maintenance Effectiveness and Reliability Using Intelligent Based Health Monitoring

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ISBN 13 :
Total Pages : 113 pages
Book Rating : 4.:/5 (85 download)

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Book Synopsis Improving Aircraft Engine Maintenance Effectiveness and Reliability Using Intelligent Based Health Monitoring by : Şeref Demirci

Download or read book Improving Aircraft Engine Maintenance Effectiveness and Reliability Using Intelligent Based Health Monitoring written by Şeref Demirci and published by . This book was released on 2009 with total page 113 pages. Available in PDF, EPUB and Kindle. Book excerpt: Engine Health monitoring (EHM) has been a very popular subject to increase aircraft availability with minimum maintenance cost. The study is aimed at providing a method to monitor the aircraft engine health during the flight with the aim of providing an opportunity for early fault detection to improve airline maintenance effectiveness and reliability. Since the impending engine failures may cause to change the engine parameters such as Fuel Flow (FF), Exhaust Gas Temperature (EGT), engine fan speed (N1), engine compressor speed (N2), etc., engine deteriorations or faults may be identified before they occur by monitoring them. So as to monitor engine health in flight, the automation of current work for EHM which is done manually by airlines is developed by using fuzzy logic (FL) and neural network (NN) models. FL is selected to develop an Automated EHM system (AEHMS), since it is very useful method for automation health monitoring. The fuzzy rule inference system for different engine faults is based on the expert knowledge and real life data in Turkish Airlines fleet. The complete loop of EHM is automatically performed by visual basic programs and Fuzzy Logic Toolbox in MATLAB. Finally, the method is utilized to run for monitoring the engines in Turkish Airlines fleet. This study has shown that AEHMS can be used by airlines or engine manufacturers efficiently to simplify the EHM system and minimize the drawbacks of it, such as extra labor hour, human error and requirement for engineering expertise. This method may also be applicable other than aircraft engines such as auxiliary power unit, structures. Since every engine type has different characters, it is required to revise the fuzzy rules for the concerning engine types.

FAULT DETECTION AND ISOLATION OF JET ENGINES USING NEURAL NETWORKS.

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ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (13 download)

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Book Synopsis FAULT DETECTION AND ISOLATION OF JET ENGINES USING NEURAL NETWORKS. by : Seyed Sina Tayarani Bathaie

Download or read book FAULT DETECTION AND ISOLATION OF JET ENGINES USING NEURAL NETWORKS. written by Seyed Sina Tayarani Bathaie and published by . This book was released on 2012 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Information and Communication Technologies in Education, Research, and Industrial Applications

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Publisher : Springer Nature
ISBN 13 : 3031483251
Total Pages : 373 pages
Book Rating : 4.0/5 (314 download)

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Book Synopsis Information and Communication Technologies in Education, Research, and Industrial Applications by : Grigoris Antoniou

Download or read book Information and Communication Technologies in Education, Research, and Industrial Applications written by Grigoris Antoniou and published by Springer Nature. This book was released on with total page 373 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Development of an Artificial Neural Network Damage Detection Module for a Structural Health Monitoring System

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ISBN 13 :
Total Pages : 109 pages
Book Rating : 4.:/5 (697 download)

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Book Synopsis Development of an Artificial Neural Network Damage Detection Module for a Structural Health Monitoring System by : Zachary Tyler Kral

Download or read book Development of an Artificial Neural Network Damage Detection Module for a Structural Health Monitoring System written by Zachary Tyler Kral and published by . This book was released on 2009 with total page 109 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aircraft, wind turbines, or space stations are expected to remain in service well beyond their designed performance lifetime. Consequently, maintenance is an important issue for aircraft or aerospace structures. This is accomplished through inspecting for damage at scheduled times and replacing damaged parts before failure. Ground inspections of aircraft, even using simple nondestructive testing techniques, generally require the aircraft be pulled from operation so that its components can be inspected for damage. Structural components are replaced if sufficient damage is found. Research is underway to develop a structural health monitoring (SHM) system as a means to improve the current maintenance routine. This system would consist of an array of sensors and associated analysis codes which would scan for damage in-flight and perform real-time damage analysis of an aircraft's structure. If damage is recognized long before failure occurs, then a damage tolerance and prognostic assessment could be implemented, allowing for a determination of the remaining life of components. The current method of inspecting aircraft, consisting of ground inspections for damage after a set number of flight hours, works well from an aircraft safety point of view. However, an in-flight SHM system would allow for better use of components, as specific lifetimes could be determined; and, could be less costly, since an SHM system could be embedded into the aircraft structure, thereby reducing or eliminating the need to tear down the aircraft to scan for damage during the ground inspection and would ultimately lead to fewer required ground inspections. General theory for material mechanics, fracture mechanics, waveform theory, and artificial neural networks are presented in this paper. Among these, a simple triangulation method is developed to locate a crack tip position and a procedure of combining the theory of fracture mechanics with waveform theories is introduced. These components were used collectively in a series of experiments to investigate the possibility of using them in a future SHM system. Flat aluminum panels, similar in thickness to those found in many aerospace structures, were subjected to increasing static loading during laboratory tests. As the load increased, a designed crack in the panel increased in size, releasing strain waves into the material. These waves were then detected by acoustic emission sensors, and artificial neural networks were implemented to analyze the received strain waves. From a feed-forward neural network, the crack length was approximated. Next, similar aluminum panels were placed in a simply supported beam configuration with ultrasonic actuators attached at various positions. These actuators created multiple point source locations, which was received by multiple acoustic emission sensors. The location of the source was calculated by both triangulation method and an vi artificial neural network. A theory of plastic zone interference with strain waves released from crack tip extension was introduced and shown as a possibility during the analysis of a final experiment. Sensors placed behind the crack front were observed to detect waves with smaller amplitudes than the sensors placed in locations in front of the crack during crack extension due to increasing, pseudo-static applied load. The effect of the acoustic emission sensor placement relative to crack tip growth detections was determined to be possibly integrated with an artificial neural network in future research. Experiments were conducted to determine the crack length and location, using artificial neural network analyses of acoustic emission signals. Artificial neural networks were developed which were trained with an existing dataset of crack properties. These neural networks were applied to new situations that were not part of the training dataset. The approximated crack growth of the artificial neural networks was around 10% shorter than the actual measured crack growth length for an extension of around 0.8 in. Finally, some SHM analysis systems were proposed, based on the conclusions made in the experiments. The artificial neural networks performed well at approximating both the crack extension and location, using acoustic emission detections. These artificial neural networks in combination with an acoustic emission system are reasonable candidate for the initial stages of a feasible structural health monitoring system to determine the location and severity of structural damage within an aerospace structure.

Sensor-only system identification for structural health monitoring of advanced aircraft

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ISBN 13 :
Total Pages : 15 pages
Book Rating : 4.:/5 (848 download)

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Book Synopsis Sensor-only system identification for structural health monitoring of advanced aircraft by : Sunil L. Kukreja

Download or read book Sensor-only system identification for structural health monitoring of advanced aircraft written by Sunil L. Kukreja and published by . This book was released on 2012 with total page 15 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Application of Neural Networks to the F/A-18 Engine Condition Monitoring System

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ISBN 13 :
Total Pages : 125 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Application of Neural Networks to the F/A-18 Engine Condition Monitoring System by : Joseph Thomas Gengo

Download or read book Application of Neural Networks to the F/A-18 Engine Condition Monitoring System written by Joseph Thomas Gengo and published by . This book was released on 1989 with total page 125 pages. Available in PDF, EPUB and Kindle. Book excerpt: Neural networks were applied to the Engine Condition and Monitoring System of the F/A-18 aircraft. Due to recent fleet experience with compressor blade failures in flight, neural networks were applied to three engine conditions, flameout due to compressor failures, normal operating conditions, and low oil pressure conditions. An attempt was made to predict compressor failure using the neural networks. A back propagation and back propagation/Kohonen network were successfully tested in recognizing the various conditions with data previously unseen by the networks. Both networks demonstrated promise in predicting failures although not enough data was available for conclusive results. Keywords: Theses; Data acquisition; Fortran; Naval aircraft. (kr).

Health Monitoring of an Aircraft Fuel System Using Artificial Intelligence Techniques

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ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (139 download)

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Book Synopsis Health Monitoring of an Aircraft Fuel System Using Artificial Intelligence Techniques by : Vijaylakshmi S. S Jigajinni

Download or read book Health Monitoring of an Aircraft Fuel System Using Artificial Intelligence Techniques written by Vijaylakshmi S. S Jigajinni and published by . This book was released on 2018 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aircraft is a non-linear complex system and is need of regular monitoring. Integrated Vehicle Health Management (IVHM) is a process of health management paradigm, which involves system parameter monitoring, assessment of current, future conditions through diagnostic and prognostic approaches by providing required maintenance activities. Deployment of diagnostic, prognostic and health management processes enable to improve the system reliability and reduces the operating cost of the aircraft. Health monitoring and management plays a vibrant role in safe operation and maintenance of aircraft. Soft computing methodologies such as Artificial Neural Networks (ANN) and Adaptive Neuro-Fuzzy Inference System (ANFIS) are used to estimate the health status of fuel system by developing model of a typical pump feed, twin-engine, four-tank small aircraft fuel system using Simulink in the laboratory environment. The controller is designed to generate the signals of the fuel tanks based on the fuel requirement of the engine. The ANFIS based management system helps to detect the faults existing in the fuel system and diagnose those faults using the expert,Äôs logical rules. During a fault ailment, the controller,Äôs performance is evaluated. The efficacy of this intelligent controller is verified with the present fuel control system and ANN controller.

Intelligent and Fuzzy Systems

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Publisher : Springer Nature
ISBN 13 : 3031671953
Total Pages : 812 pages
Book Rating : 4.0/5 (316 download)

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Book Synopsis Intelligent and Fuzzy Systems by : Cengiz Kahraman

Download or read book Intelligent and Fuzzy Systems written by Cengiz Kahraman and published by Springer Nature. This book was released on with total page 812 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Application of Neural Networks to the F/A-18 Engine Condition Monitoring System

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Publisher :
ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Application of Neural Networks to the F/A-18 Engine Condition Monitoring System by :

Download or read book Application of Neural Networks to the F/A-18 Engine Condition Monitoring System written by and published by . This book was released on 1989 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: Neural networks were applied to the Engine Condition and Monitoring System of the F/A-18 aircraft. Due to recent fleet experience with compressor blade failures in flight, neural networks were applied to three engine conditions, flameout due to compressor failures, normal operating conditions, and low oil pressure conditions. An attempt was made to predict compressor failure using the neural networks. A back propagation and back propagation/Kohonen network were successfully tested in recognizing the various conditions with data previously unseen by the networks. Both networks demonstrated promise in predicting failures although not enough data was available for conclusive results. Keywords: Theses; Data acquisition; Fortran; Naval aircraft. (kr).