AI Chat Paper
Note: Please note that the following content is generated by AMiner AI. SciOpen does not take any responsibility related to this content.
{{lang === 'zh_CN' ? '文章概述' : 'Summary'}}
{{lang === 'en_US' ? '中' : 'Eng'}}
Chat more with AI
Article Link
Collect
Submit Manuscript
Show Outline
Outline
Show full outline
Hide outline
Outline
Show full outline
Hide outline
Research Article

Neural networks-based solution of the two-body problem

Zhuojun Hou1Qinbo Sun1Zhaohui Dang1,2( )
School of Astronautics, Northwestern Polytechnical University, Xi’an 710072, China
National Key Laboratory of Aerospace Flight Dynamics, Xi’an 710072, China
Show Author Information

Abstract

This paper presents a novel machine learning approach designed to efficiently solve the classical two-body problem. The inherent structure of the two-body problem involves the integration of a system of second-order nonlinear ordinary differential equations. Conventional numerical integration techniques that rely on small computation steps result in a prolonged computational time. Moreover, calculus has limitations in resolving the two-body problem, inevitably converging towards an unresolved Kepler equation of a transcendental nature. To address this issue, we integrate the conventional analytical solution based on true anomaly with a deep neural network representation of the Kepler equation. This results in a highly accurate closed-form solution that is solely dependent on time, which is termed a learning-based solution to the two-body problem. To enhance the precision, a correction module based on Halley iteration is introduced, which substantially improves the final solution in terms of precision and computational cost. Compared to state-of-the-art methods such as the piecewise Padé approximation, Adomian decomposition method, and modified Mikkola’s method, our approach achieves a computational speedup of several thousand to tens of thousands, while maintaining accuracy in large-scale orbit propagation scenarios. Empirical validation under simulated conditions underscores its effectiveness and potential value for long-term orbit determination.

Graphical Abstract

References

【1】
【1】
 
 
Astrodynamics
Pages 537-564

{{item.num}}

Comments on this article

Go to comment

< Back to all reports

Review Status: {{reviewData.commendedNum}} Commended , {{reviewData.revisionRequiredNum}} Revision Required , {{reviewData.notCommendedNum}} Not Commended Under Peer Review

Review Comment

Close
Close
Cite this article:
Hou Z, Sun Q, Dang Z. Neural networks-based solution of the two-body problem. Astrodynamics, 2025, 9(4): 537-564. https://doi.org/10.1007/s42064-024-0230-8

957

Views

5

Crossref

4

Web of Science

4

Scopus

0

CSCD

Received: 08 January 2024
Accepted: 03 June 2024
Published: 26 August 2025
© Tsinghua University Press 2025