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积分修正类轨道计算方法研究综述

王昌涛,代洪华,董一超,石琳,杨文传,岳晓奎   

  1. 西北工业大学
  • 收稿日期:2025-07-08 修回日期:2025-09-29 出版日期:2025-10-09 发布日期:2025-10-09
  • 通讯作者: 代洪华
  • 基金资助:
    国家杰出青年科学基金;科技部重点研发计划项目;西北工业大学博士论文创新基金

Review of integral correction methods for orbit calculation

  • Received:2025-07-08 Revised:2025-09-29 Online:2025-10-09 Published:2025-10-09

摘要: 针对航天器轨道的快速计算问题,综述了积分修正类轨道算法的相关研究。首先在统一的配点符号体系下系统介绍了不同的积分修正类算法,并进行了分类与对比;然后聚焦该类算法的大步长和并行计算优势,梳理了其在参数优化和并行加速方面的研究进展;而后在航天器轨道设计、高精度轨道递推和飞行器制导等典型应用中阐述了积分修正类算法的特有优势;最后,结合算法特点与轨道计算需求分析了未来发展趋势,提出了值得研究的方向。

关键词: 轨道快速计算, 轨道递推, 积分修正, 参数优化, 并行计算

Abstract: Aiming at the high-efficiency orbit calculation problem of spacecraft, the research about integral correction methods is reviewed. First, a variety of integral correction methods based on different principles are systematically introduced within a unified notation framework, and a classification comparison is conducted. Then, focusing on the large-step and parallel computing ad-vantages of these methods, the research progress in their parameter optimization and parallel acceleration is summarized. Then, the unique superiority of integral correction methods is elaborated by typical applications such as spacecraft orbit design, high-precision orbit propagation, and spacecraft guidance. Finally, combining the methods’ characteristics and the orbit calculation requirements, the development trends and directions worth studying are analyzed and proposed.

Key words: high-efficiency orbit calculation, orbit propagation, integral correction, parameter optimization, parallel computation

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