2020
DOI: 10.1016/j.ast.2020.105775
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A modeling method for aero-engine by combining stochastic gradient descent with support vector regression

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Cited by 47 publications
(8 citation statements)
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References 12 publications
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“…46 As for SVR-SMO, it has been recently used in aero-engine aerodynamic models. 56 An SVR-PUK was used to predict daily cloud free sea surface temperature from a sensor 57 and to spectra. 48 Finally, an SVR-SMO-PUK has been used to predict the wrinkle-based age, 49 and for snow depth retrieval.…”
Section: Studies On Software Effort Prediction Techniquesmentioning
confidence: 99%
“…46 As for SVR-SMO, it has been recently used in aero-engine aerodynamic models. 56 An SVR-PUK was used to predict daily cloud free sea surface temperature from a sensor 57 and to spectra. 48 Finally, an SVR-SMO-PUK has been used to predict the wrinkle-based age, 49 and for snow depth retrieval.…”
Section: Studies On Software Effort Prediction Techniquesmentioning
confidence: 99%
“…The overall classification accuracy of all algorithms was 87% in the diabetes dataset, 95% in the healthcare stroke prediction dataset, and 82% in the adult dataset. Ren et al [33] proposed a data-driven modeling approach for aeroengine aerodynamic models combining stochastic gradient descent with support vector regression. The modeling method was validated using simulation data from an aero-engine component-level model and flight data from a type of aircraft, and it provided better performance compared with the traditional method.…”
Section: Introductionmentioning
confidence: 99%
“…Asgari et al 19 applied NARX neural network to simulate the start-up procedure of a single-shaft gas turbine and the findings demonstrate that NARX neural network models are capable of satisfactory prediction of the start-up behavior. Ren et al 20 proposed a novel online Support Vector Regression (SVR) by introducing Stochastic Gradient Descent (SGD) as the nonlinear function of NARX models, and the online SVR was applied to online modeling with the online flight data of a two-rotor turbojet engine.…”
Section: Introductionmentioning
confidence: 99%