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导弹与制导技术

基于Battin-Vaughan算法的轨道机动任务规划

  • 李新三 ,
  • 王明建 ,
  • 闫循良
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  • 1 第二炮兵士官学校,山东青州 262500
    2 西北工业大学,西安 710072

李新三(1982-),男,湖北广水人,硕士研究生,研究方向:飞行器飞行动力学与控制。

收稿日期: 2009-12-15

  网络出版日期: 2025-05-28

Mission Llanning of Orbital Maneuver Based on Battin-Vaughan Algorithm

  • LI Xinsan ,
  • WANG Mingjian ,
  • YAN Xunliang
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  • 1 The Second Artillery NCO School, Shandong Qingzhou 262500, China
    2 Northwestern Polytechnical University, Xi'an 710072, China

Received date: 2009-12-15

  Online published: 2025-05-28

摘要

研究了空间交会远程导引阶段的轨道机动任务规划。将双冲量空间交会转化为高斯问题进行求解。采用Battin-Vaughan算法对机动初始位置和飞行时间的组合进行遍历计算,并做出机动时间、追踪器初始真近点角、所需特征速度的三维曲面图以及△v等值线图,进行航天器空间拦截交会的任务规划。仿真结果表明了采用Battin-Vaughan算法求解高斯问题的优越性;对空间拦截交会等飞行任务而言,将绘制和分析Av等值线图作为任务规划的辅助工具能直观快速的为工程应用提供参考。

本文引用格式

李新三 , 王明建 , 闫循良 . 基于Battin-Vaughan算法的轨道机动任务规划[J]. 弹箭与制导学报, 2010 , 30(6) : 56 -59 . DOI: 10.15892/j.cnki.djzdxb.2010.06.008

Abstract

The space rendezvous and remote-guided mission planning methold of the orbital maneuver is researched in this thesis. The matter is resolved by translating double impulse problem into gaussian problem. the initial position and the flighting time is ergodic caculated by Battin-Vaughan algorithm. The three-dimensional surface map and contour map of the maneuver time, the tracker initial true anomaly and the required characteristic velocity is made in this thesis. The mission of spacecraft rendezvous and intercept in space is planned. Simulation results show that the using of Battin-Vaughan for solving the Gaussian question is effective. Such as space rendezvous and interception mission analysis, the mapping and analysis of the contour map as a mission planning support tool can intuitively and quickly provide a reference for engineering applications.

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