{"title":"基于神经网络的二体问题求解","authors":"Zhuojun Hou, Qinbo Sun, Zhaohui Dang","doi":"10.1007/s42064-024-0230-8","DOIUrl":null,"url":null,"abstract":"<div><p>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.\n</p><div><figure><div><div><picture><source><img></source></picture></div></div></figure></div></div>","PeriodicalId":52291,"journal":{"name":"Astrodynamics","volume":"9 4","pages":"537 - 564"},"PeriodicalIF":6.5000,"publicationDate":"2025-08-26","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Neural networks-based solution of the two-body problem\",\"authors\":\"Zhuojun Hou, Qinbo Sun, Zhaohui Dang\",\"doi\":\"10.1007/s42064-024-0230-8\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><p>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.\\n</p><div><figure><div><div><picture><source><img></source></picture></div></div></figure></div></div>\",\"PeriodicalId\":52291,\"journal\":{\"name\":\"Astrodynamics\",\"volume\":\"9 4\",\"pages\":\"537 - 564\"},\"PeriodicalIF\":6.5000,\"publicationDate\":\"2025-08-26\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Astrodynamics\",\"FirstCategoryId\":\"1087\",\"ListUrlMain\":\"https://link.springer.com/article/10.1007/s42064-024-0230-8\",\"RegionNum\":1,\"RegionCategory\":\"物理与天体物理\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q2\",\"JCRName\":\"ASTRONOMY & ASTROPHYSICS\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Astrodynamics","FirstCategoryId":"1087","ListUrlMain":"https://link.springer.com/article/10.1007/s42064-024-0230-8","RegionNum":1,"RegionCategory":"物理与天体物理","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q2","JCRName":"ASTRONOMY & ASTROPHYSICS","Score":null,"Total":0}
Neural networks-based solution of the two-body problem
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.
期刊介绍:
Astrodynamics is a peer-reviewed international journal that is co-published by Tsinghua University Press and Springer. The high-quality peer-reviewed articles of original research, comprehensive review, mission accomplishments, and technical comments in all fields of astrodynamics will be given priorities for publication. In addition, related research in astronomy and astrophysics that takes advantages of the analytical and computational methods of astrodynamics is also welcome. Astrodynamics would like to invite all of the astrodynamics specialists to submit their research articles to this new journal. Currently, the scope of the journal includes, but is not limited to:Fundamental orbital dynamicsSpacecraft trajectory optimization and space mission designOrbit determination and prediction, autonomous orbital navigationSpacecraft attitude determination, control, and dynamicsGuidance and control of spacecraft and space robotsSpacecraft constellation design and formation flyingModelling, analysis, and optimization of innovative space systemsNovel concepts for space engineering and interdisciplinary applicationsThe effort of the Editorial Board will be ensuring the journal to publish novel researches that advance the field, and will provide authors with a productive, fair, and timely review experience. It is our sincere hope that all researchers in the field of astrodynamics will eagerly access this journal, Astrodynamics, as either authors or readers, making it an illustrious journal that will shape our future space explorations and discoveries.