A hybrid ARIMA–SVM model for the study of the remaining useful life of aircraft engines

In this research, an algorithm is presented for predicting the remaining useful life (RUL) of aircraft engines from a set of predictor variables measured by several sensors located in the engine. RUL prediction is essential for the safety of those aboard, but also to reduce engine maintenance and re...

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Published inJournal of computational and applied mathematics Vol. 346; pp. 184 - 191
Main Authors Ordóñez, Celestino, Sánchez Lasheras, Fernando, Roca-Pardiñas, Javier, Juez, Francisco Javier de Cos
Format Journal Article
LanguageEnglish
Published Elsevier B.V 15.01.2019
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Online AccessGet full text
ISSN0377-0427
1879-1778
1879-1778
DOI10.1016/j.cam.2018.07.008

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Abstract In this research, an algorithm is presented for predicting the remaining useful life (RUL) of aircraft engines from a set of predictor variables measured by several sensors located in the engine. RUL prediction is essential for the safety of those aboard, but also to reduce engine maintenance and repair costs. The algorithm combines time series analysis methods to forecast the values of the predictor variables with machine learning techniques to predict RUL from those variables. First, an auto-regressive integrated moving average (ARIMA) model is used to estimate the values of the predictor variables in advance. Then, we use the result of the previous step as the input of a support vector regression model (SVM), where RUL is the response variable. The validity of the method was checked on an extensive public database, and the results compared with those obtained using a vector auto-regressive moving average (VARMA) model. Our algorithm showed a high prediction capability, far greater than that provided by the VARMA model. •A method to forecast the remaining useful life of aircraft engines is proposed.•The predictor variables were obtained from sensors located in the engine.•The proposed method combines ARIMA and SVM models.•Results of our method unsurpassed those obtained using a VARMA model.
AbstractList In this research, an algorithm is presented for predicting the remaining useful life (RUL) of aircraft engines from a set of predictor variables measured by several sensors located in the engine. RUL prediction is essential for the safety of those aboard, but also to reduce engine maintenance and repair costs. The algorithm combines time series analysis methods to forecast the values of the predictor variables with machine learning techniques to predict RUL from those variables. First, an auto-regressive integrated moving average (ARIMA) model is used to estimate the values of the predictor variables in advance. Then, we use the result of the previous step as the input of a support vector regression model (SVM), where RUL is the response variable. The validity of the method was checked on an extensive public database, and the results compared with those obtained using a vector auto-regressive moving average (VARMA) model. Our algorithm showed a high prediction capability, far greater than that provided by the VARMA model. •A method to forecast the remaining useful life of aircraft engines is proposed.•The predictor variables were obtained from sensors located in the engine.•The proposed method combines ARIMA and SVM models.•Results of our method unsurpassed those obtained using a VARMA model.
Author Roca-Pardiñas, Javier
Juez, Francisco Javier de Cos
Ordóñez, Celestino
Sánchez Lasheras, Fernando
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Keywords Remaining useful life (RUL)
Genetic algorithms (GA)
Aircraft engines
Vector autoregression moving-average (VARMA)
Support vector machines (SVM)
Language English
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Snippet In this research, an algorithm is presented for predicting the remaining useful life (RUL) of aircraft engines from a set of predictor variables measured by...
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SubjectTerms Aircraft engines
Genetic algorithms (GA)
Remaining useful life (RUL)
Support vector machines (SVM)
Vector autoregression moving-average (VARMA)
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Title A hybrid ARIMA–SVM model for the study of the remaining useful life of aircraft engines
URI https://dx.doi.org/10.1016/j.cam.2018.07.008
http://hdl.handle.net/10651/49435
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