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.
Authors
- Chunyong Zhang (ORCID: https://orcid.org/0000-0002-7372-1760)
- Xin Shan (ORCID: https://orcid.org/0000-0003-2012-2497)
- Jinkui Chu (ORCID: https://orcid.org/0000-0001-5742-8460)
- Ran Zhang (ORCID: https://orcid.org/0000-0002-0506-1334)
- Chien‐Chung Fu (ORCID: https://orcid.org/0000-0002-3789-228X)
- Lei Bian (ORCID: https://orcid.org/0000-0001-9574-7673)
- Xiaobo Han (ORCID: https://orcid.org/0000-0002-0722-7246)
Institutions
- Dalian University of Technology (CN)
- Institute of Agricultural Machinery (JP)
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
- Field-Weighted Citation Impact
- 0.00