QPSO-BP Neural Network Model for Actuator Pressure and Friction Torque in Solid Rocket Ball Joint Nozzles

Friction torque is crucial to the overall design, reliability of motion, and accuracy of a rocket nozzle. The accurate prediction of driving pressure is essential for calculating the friction torque. To address this issue, we propose a prediction method based on quantum particle swarm optimization (QPSO) and a back propagation (BP) neural network. We first derive a formula to calculate the friction torque by using a Lagrangian dynamics equation to establish a theoretical foundation for subsequent analysis. We then obtain driving pressure data under different swing commands and various load conditions by conducting a pendulum test of the rocket nozzle. Using the experimental data as the training set, we perform a nonlinear regression of the driving pressure with the QPSO-BP neural network. The results indicate that, for the two actuators, the average relative errors in driving pressure predictions under dynamic friction are 0.486% and 0.879%, respectively; under static friction, the relative errors in these values are 2.614% and 2.669%, respectively. The findings of this study suggest that the QPSO-BP neural network model achieves an average prediction accuracy of 99.317% under kinetic friction and 97.358% under static friction, highlighting its potential for high-precision driving pressure prediction and friction torque calculation.

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Publication Details

Journal
Journal of Aerospace Engineering
Published
2025-11-29
DOI
https://doi.org/10.1061/jaeeez.aseng-6576
Primary Topic
Rocket and propulsion systems research
Type
article
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article

QPSO-BP Neural Network Model for Actuator Pressure and Friction Torque in Solid Rocket Ball Joint Nozzles

Chunyong Zhang, Xin Shan, Jinkui Chu, Ran Zhang et al.
Journal of Aerospace Engineering
Rocket and propulsion systems research
article

QPSO-BP Neural Network Model for Actuator Pressure and Friction Torque in Solid Rocket Ball Joint Nozzles

Chunyong Zhang, Xin Shan, Jinkui Chu, Ran Zhang, Chien‐Chung Fu, Lei Bian, Xiaobo Han
article en

Abstract

Friction torque is crucial to the overall design, reliability of motion, and accuracy of a rocket nozzle. The accurate prediction of driving pressure is essential for calculating the friction torque. To address this issue, we propose a prediction method based on quantum particle swarm optimization (QPSO) and a back propagation (BP) neural network. We first derive a formula to calculate the friction torque by using a Lagrangian dynamics equation to establish a theoretical foundation for subsequent analysis. We then obtain driving pressure data under different swing commands and various load conditions by conducting a pendulum test of the rocket nozzle. Using the experimental data as the training set, we perform a nonlinear regression of the driving pressure with the QPSO-BP neural network. The results indicate that, for the two actuators, the average relative errors in driving pressure predictions under dynamic friction are 0.486% and 0.879%, respectively; under static friction, the relative errors in these values are 2.614% and 2.669%, respectively. The findings of this study suggest that the QPSO-BP neural network model achieves an average prediction accuracy of 99.317% under kinetic friction and 97.358% under static friction, highlighting its potential for high-precision driving pressure prediction and friction torque calculation.

Journal of Aerospace EngineeringVol. 39(2)
Dalian University of Technology (CN), Institute of Agricultural Machinery (JP)
Openalex Percentile: Top 51%
Rocket and propulsion systems research
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QPSO-BP Neural Network Model for Actuator Pressure and Friction Torque in Solid Rocket Ball Joint Nozzles — Chunyong Zhang, Xin Shan, et al. · Journal of Aerospace Engineering (2025) | TGRS Research Map | TGRS