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A mixture non-parametric regression prediction model with its application in the fault prediction of rocket engine thrust

Hao Xiang (Yulin Normal University, Yulin, China)

Journal of Quality in Maintenance Engineering

ISSN: 1355-2511

Article publication date: 1 November 2023

Issue publication date: 23 February 2024

23

Abstract

Purpose

It is of a great significance for the health monitoring of a liquid rocket engine to build an accurate and reliable fault prediction model. The thrust of a liquid rocket engine is an important indicator for its health monitoring. By predicting the changing value of the thrust, it can be judged whether the engine will fail at a certain time. However, the thrust is affected by various factors, and it is difficult to establish an accurate mathematical model. Thus, this study uses a mixture non-parametric regression prediction model to establish the model of the thrust for the health monitoring of a liquid rocket engine.

Design/methodology/approach

This study analyzes the characteristics of the least squares support vector regression (LS-SVR) machine . LS-SVR is suitable to model on the small samples and high dimensional data, but the performance of LS-SVR is greatly affected by its key parameters. Thus, this study implements the advanced intelligent algorithm, the real double-chain coding target gradient quantum genetic algorithm (DCQGA), to optimize these parameters, and the regression prediction model LSSVRDCQGA is proposed. Then the proposed model is used to model the thrust of a liquid rocket engine.

Findings

The simulation results show that: the average relative error (ARE) on the test samples is 0.37% when using LS-SVR, but it is 0.3186% when using LSSVRDCQGA on the same samples.

Practical implications

The proposed model of LSSVRDCQGA in this study is effective to the fault prediction on the small sample and multidimensional data, and has a certain promotion.

Originality/value

The original contribution of this study is to establish a mixture non-parametric regression prediction model of LSSVRDCQGA and properly resolve the problem of the health monitoring of a liquid rocket engine along with modeling the thrust of the engine by using LSSVRDCQGA.

Keywords

Citation

Xiang, H. (2024), "A mixture non-parametric regression prediction model with its application in the fault prediction of rocket engine thrust", Journal of Quality in Maintenance Engineering, Vol. 30 No. 1, pp. 120-132. https://doi.org/10.1108/JQME-08-2023-0070

Publisher

:

Emerald Publishing Limited

Copyright © 2023, Emerald Publishing Limited

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