Technical Papers
Jul 9, 2024

Neural Network Reentry Guidance for Reusable Launch Vehicle Based on Sample Dimensionality Reduction

Publication: Journal of Aerospace Engineering
Volume 37, Issue 5

Abstract

In this paper, a neural network guidance based on sample dimension reduction is proposed for a reusable launch vehicle. Different from previous works, the training samples of neural networks use Pearson correlation matrix analysis for dimension reduction, which significantly reduces the data volume of training samples and improves the efficiencies of sample construction, data storage, and neural network training. First, the analytical samples are generated by integrating dimensionless energy longitudinal motion equations. Then, the input parameters are processed by Pearson correlation matrix analysis, significantly reducing the data volume of training samples while ensuring the training effectiveness. Furthermore, the neural network is utilized to learn the mapping relationship between reduced-dimension flight states and predictive range-to-go, eliminating numerical integration calculations and improving the real-time performance of guidance. Finally, an extended Kalman filter (EKF) is implemented online for aerodynamic parameter identification, which dramatically enhances the adaptability to internal uncertainties and external disturbances. Compared with the traditional numerical guidance method, simulation results demonstrate that the proposed guidance exhibits superior real-time performance and faster computation speed while ensuring high accuracy and strong robustness to perturbations.

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Data Availability Statement

All data, models, and code generated or used during the study appear in the published article.

Acknowledgments

This work was partly supported by the National Natural Science Foundation of China, Grant 11202024.

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Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 37Issue 5September 2024

History

Received: Jun 5, 2023
Accepted: Mar 18, 2024
Published online: Jul 9, 2024
Published in print: Sep 1, 2024
Discussion open until: Dec 9, 2024

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Qian Xu
Senior Engineer, Beijing Institute of Astronautical System Engineering, No. 1, Donggaodi South St., Fengtai District, Beijing 100076, China.
Ph.D. Candidate, School of Aerospace Engineering, Beijing Institute of Technology, No. 5, Zhongguancun South St., Haidian District, Beijing 100081, China; Key Laboratory of Dynamics and Control of Flight Vehicle, Ministry of Education, No. 5, Zhongguancun South St., Haidian District, Beijing 100081, China. ORCID: https://orcid.org/0000-0003-2391-9178
Engineer, Xi’an Modern Control Technology Research Institute, No. 10, Zhangba East Rd., Yanta District, Xi’an 710065, China (corresponding author). Email: [email protected]
Yufei Zhang
Senior Engineer, Science and Technology on Space Physics Laboratory, No. 1, Donggaodi South St., Fengtai District, Beijing 100076, China.

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