留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

四体模型下2∶1 DRO附近的拟周期轨道

王明 杨驰航 张皓

王明,杨驰航,张皓. 四体模型下2∶1 DRO附近的拟周期轨道[J]. 北京航空航天大学学报,2026,52(4):1148-1159
引用本文: 王明,杨驰航,张皓. 四体模型下2∶1 DRO附近的拟周期轨道[J]. 北京航空航天大学学报,2026,52(4):1148-1159
WANG M,YANG C H,ZHANG H. Quasi-periodic orbits near 2∶1 resonant DRO in the four-body problem[J]. Journal of Beijing University of Aeronautics and Astronautics,2026,52(4):1148-1159 (in Chinese)
Citation: WANG M,YANG C H,ZHANG H. Quasi-periodic orbits near 2∶1 resonant DRO in the four-body problem[J]. Journal of Beijing University of Aeronautics and Astronautics,2026,52(4):1148-1159 (in Chinese)

四体模型下2∶1 DRO附近的拟周期轨道

doi: 10.13700/j.bh.1001-5965.2024.0061
基金项目: 

中国科学院战略性先导科技专项(XDA30010200)

详细信息
    通讯作者:

    E-mail:hao.zhang.zhr@csu.ac.cn

  • 中图分类号: V221+.3;TB553

Quasi-periodic orbits near 2∶1 resonant DRO in the four-body problem

Funds: 

Strategic Priority Program on Space Science of the Chinese Academy of Sciences(XDA30010200)

More Information
  • 摘要:

    地月空间2∶1共振远距离逆行轨道(DRO)因其长期稳定和全域可达的良好特性,在当前地月空间任务探索中具有重要的战略意义。为进一步理解2∶1 DRO附近的相空间结构,同时提供更多的可供选择的停泊轨道,在双圆限制性四体模型(BCR4BP)下对2种不同构型的2∶1 DRO附近的拟周期轨道进行了计算。针对目前数值延拓计算拟周期轨道过程较为繁复的缺点,提出一种自适应延拓算法,该算法可自动调节延拓步长及添加表征环面所需的离散节点数量,从而在保证环面精度的情况下越过共振区,同时平衡了计算时间。在此基础上,针对BCR4BP中2种不同构型的2∶1 DRO,分别计算了其附近存在的2D拟DRO 族,进一步分析了其稳定特性。仿真结果表明:所提算法能有效差异化处理采样阶次不足与共振奇异,从而得到较为完整的轨道族。

     

  • 图 1  平面双圆限制性四体模型

    Figure 1.  Planar bicircular restricted four-body problem

    图 2  双圆限制性四体模型中的2种2∶1 DRO构型

    Figure 2.  Two different configurations of 2∶1 DRO in BCR4BP

    图 3  2种DRO构型在庞加莱截面上的投影

    Figure 3.  Two different configurations of 2∶1 DRO projected on the Poincaré section

    图 4  周期轨道和拟周期轨道示意图

    Figure 4.  Diagram of periodic and quasi-periodic orbit

    图 5  自适应延拓框架

    Figure 5.  Adaptive continuation framework

    图 6  $ {\rho }_{\text{s,p1}} $所对应的平面拟DRO轨道族在x方向的最小值随$ {\rho }_{\text{s,p1}} $的变化关系图

    Figure 6.  Relationship between the minimum value of plane quasi-DRO corresponding to $ {\rho }_{\text{s,p1}} $ in x direction and rotation angle $ {\rho }_{\text{s,p1}} $

    图 7  与$ {\rho }_{\text{s,p1}} $相对应的平面2D拟DRO族中的4条轨道

    Figure 7.  Four members of 2D plane quasi-DRO family corresponding to $ {\rho }_{\text{s,p1}} $

    图 8  $ {\rho }_{\text{s,p2}} $所对应的平面拟DRO轨道族在x方向的最小值随$ {\rho }_{\text{s,p2}} $的变化关系

    Figure 8.  Relationship between the minimum value of plane quasi-DROs corresponding to $ {\rho }_{\text{s,p2}} $ in x direction and rotation angle $ {\rho }_{\text{s,p2}} $

    图 9  与$ {\rho }_{\text{s,p2}} $相对应的平面2D拟DRO轨道族中的4条轨道

    Figure 9.  Four members of 2D plane quasi-DRO family corresponding to $ {\rho }_{\text{s,p2}} $

    图 10  $ {\rho }_{\text{s,v1}} $所对应的法向拟DRO在月球左侧z方向的最大值随$ {\rho }_{\text{s,v1}} $的变化关系图

    Figure 10.  Relationship between the maximum value of vertical quasi-DROs on left of the Moon in z direction and rotation angle$ {\rho }_{\text{s,v1}} $

    图 11  与$ {\rho }_{\text{s,v1}} $相对应的法向2D拟DRO轨道族中的4条轨道

    Figure 11.  Four members of the 2D vertical quasi-DRO family corresponding to $ {\rho }_{\text{s,v1}} $

    图 12  不稳定构型附近的拟DRO的几何参数随旋转相角的变化关系

    Figure 12.  Relationship between the geometric parameters of quasi-DRO families near the unstable 2∶1 DRO and rotation phase angles

    图 13  $ {\rho }_{\text{u,p1}} $所对应的平面拟周期轨道族中的拟DRO示例

    Figure 13.  Example of plane quasi-DRO corresponding to $ {\rho }_{\text{u,p1}} $

    图 14  $ {\rho }_{\text{u,v1}} $所对应的法向拟周期轨道族中的拟DRO示例

    Figure 14.  Example of vertical quasi-DRO corresponding to $ {\rho }_{\text{u,v1}} $

    图 15  构型2附近2类2D拟周期轨道的稳定性指数关于旋转相角的变化关系

    Figure 15.  Relationship between stability index of two types of 2D quasi-DROs with respect to rotation phase angle near unstable 2∶1 DRO

    表  1  地月系统相关物理常数

    Table  1.   Physical constants in the Earth-Moon system

    物理常数 数值
    地月质量参数$ \mu $ 0.0125
    无量纲太阳质量$ {m}_{\text{S}} $ 328900.541
    无量纲太阳角速度$ {\omega }_{\text{S}} $ 0.92520
    无量纲太阳-地月质心距离$ {r}_{\text{S}} $ 388.81114
    地月距离$ {D}_{\text{U}} $/km 384405
    归一化时间$ {T}_{\text{U}} $/s 375197.58323
    归一化速度$ {V}_{\text{U}} $/(km·s−1) 1.02454
    下载: 导出CSV

    表  2  BCR4BP中2种2∶1 DRO的单值矩阵特征值及中心流形相角

    Table  2.   Eigenvalues and types of center manifolds associated with two types of 2∶1 DRO in BCR4BP

    DRO构型 单值矩阵的特征值 中心流形
    相角/rad
    中心流形
    方向

    构型1
    $ {\lambda }_{1,2}=0.460\;64\pm 0.895\;00\;{\mathrm{i}} $ 1.10843 平面
    $ {\lambda }_{3,4}=-0.758\;00\pm 0.652\;25\;{\mathrm{i}} $ 2.43104 平面
    $ {\lambda }_{5,6}=-0.978\;14\pm 0.207\;95\;{\mathrm{i}} $ 2.93211 法向

    构型2
    $ {\lambda }_{1,2}=0.460\;64\pm 0.895\;00\;{\mathrm{i}} $ 1.68608 平面
    $ {\lambda }_{3,4}=-0.915\;50\pm 0.402\;31\;{\mathrm{i}} $ 2.72755 法向
    $ {\lambda }_{5}=10.823\;37,{\lambda }_{6}=0.092\;39 $
    下载: 导出CSV
  • [1] BEZROUK C J, PARKER J. Long duration stability of distant retrograde orbits[C]//Proceedings of the AIAA/AAS Astrodynamics Specialist Conference. Reston: AIAA, 2014.
    [2] DAWN T F, GUTKOWSKI J, BATCHA A, et al. Trajectory design considerations for exploration mission 1[C]//Proceedings of the Space Flight Mechanics Meeting. Reston: AIAA, 2018.
    [3] 张晨. 基于数值延拓的日月综合借力DRO入轨策略[J]. 北京航空航天大学学报, 2024, 50(4): 1176-1186.

    ZHANG C. Low-energy transfer from Earth into DRO with hybrid gravity assist and numerical continuation[J]. Journal of Beijing University of Aeronautics and Astronautics, 2024, 50(4): 1176-1186(in Chinese).
    [4] 陈冠华, 杨驰航, 张晨, 等. 地月空间的远距离逆行轨道族及其分岔研究[J]. 北京航空航天大学学报, 2022, 48(12): 2576-2588.

    CHEN G H, YANG C H, ZHANG C, et al. Distant retrograde orbits and its bifurcations in Earth-Moon system[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(12): 2576-2588(in Chinese).
    [5] MCCARTHY B P, HOWELL K C. Leveraging quasi-periodic orbits for trajectory design in cislunar space[J]. Astrodynamics, 2021, 5(2): 139-165.
    [6] MCCARTHY B P, HOWELL K C. Trajectory design using quasi-periodic orbits in the multi-body problem[C]//Proceedings of the 29th AAS/AIAA space flight mechanics meeting. Reston: AIAA, 2019.
    [7] WANG M, YANG C H, SUN Y, et al. Family of 2: 1 resonant quasi-periodic distant retrograde orbits in cislunar space[J]. Advances in Space Research, 2024, 73(12): 6166-6181.
    [8] FARQUHAR R W, KAMEL A A. Quasi-periodic orbits about the translunar libration point[J]. Celestial Mechanics, 1973, 7(4): 458-473.
    [9] RICHARDSON D L, CARY N D. A uniformly valid solution for motion about the interior libration point of the perturbed elliptic-restricted problem[C]//Proceedings of the AIAA Conference on the Exploration of the Outer Planets. Reston: AIAA, 1975.
    [10] GÓMEZ G, MASDEMONT J, SIMÓ C. Quasihalo orbits associated with libration points[J]. The Journal of the Astronautical Sciences, 1998, 46(2): 135-176.
    [11] JORBA À, MASDEMONT J. Dynamics in the center manifold of the collinear points of the restricted three body problem[J]. Physica D: Nonlinear Phenomena, 1999, 132(1-2): 189-213.
    [12] GÓMEZ G, NOGUERA M. Some manifolds of periodic orbits in the restricted three-body problem[J]. Celestial Mechanics, 1985, 35(3): 235-255.
    [13] HOWELL K C, PERNICKA H J. Numerical determination of Lissajous trajectories in the restricted three-body problem[J]. Celestial Mechanics, 1987, 41(1): 107-124.
    [14] KOLEMEN E, KASDIN N J, GURFIL P. Quasi-periodic orbits of the restricted three-body problem made easy[J]. AIP Conference Proceedings, 2007, 886(1): 68-77.
    [15] KOLEMEN E, KASDIN N J, GURFIL P. Multiple Poincaré sections method for finding the quasiperiodic orbits of the restricted three body problem[J]. Celestial Mechanics and Dynamical Astronomy, 2012, 112(1): 47-74.
    [16] GÓMEZ G, MONDELO J M. The dynamics around the collinear equilibrium points of the RTBP[J]. Physica D: Nonlinear Phenomena, 2001, 157(4): 283-321.
    [17] OLIKARA Z P, SCHEERES D J. Numerical method for computing quasi-periodic orbits and their stability in the restricted three-body problem[J]. Advances in the Astronautical Sciences, 2012, 145: 911-930.
    [18] BARESI N, OLIKARA Z P, SCHEERES D J. Fully numerical methods for continuing families of quasi-periodic invariant tori in astrodynamics[J]. The Journal of the Astronautical Sciences, 2018, 65(2): 157-182.
    [19] OLIKARA Z P, HOWELL K C. Computation of quasi-periodic invariant tori in the restricted three-body problem[C]//Proceedings of the AIAA Space Flight Mechanics Meeting. Reston: AIAA, 2010.
    [20] JORBA À, JORBA-CUSCÓ M, ROSALES J J. The vicinity of the Earth-Moon L1 point in the bicircular problem[J]. Celestial Mechanics and Dynamical Astronomy, 2020, 132(2): 11.
    [21] LUJAN D, SCHEERES D J. Earth-Moon L2 quasi-halo orbit family: characteristics and manifold applications[J]. Journal of Guidance, Control, and Dynamics, 2022, 45(11): 2029-2045.
    [22] ROSALES J J, JORBA À, JORBA-CUSCÓ M. Families of halo-like invariant tori around L2 in the Earth-Moon bicircular problem[J]. Celestial Mechanics and Dynamical Astronomy, 2021, 133(4): 16.
    [23] MCCARTHY B P, HOWELL K C. Quasi-periodic orbits in the Sun-Earth-Moon bicircular restricted four-body problem[C]//Proceedings of the 31st AAS/AIAA Space Flight Mechanics Meeting. Reston: AIAA, 2021.
    [24] JORBA À, NICOLÁS B. Transport and invariant manifolds near L3 in the Earth-Moon bicircular model[J]. Communications in Nonlinear Science and Numerical Simulation, 2020, 89: 105327.
    [25] 李瑞龙, 朱战霞. 一种适用于大幅值Quasi周期轨道的数值构造方法[J]. 宇航学报, 2023, 44(1): 52-61.

    LI R L, ZHU Z X. A numerical construction method for large-amplitude Quasi periodic orbits[J]. Journal of Astronautics, 2023, 44(1): 52-61(in Chinese).
    [26] CIRCI C, TEOFILATTO P. On the dynamics of weak stability boundary lunar transfers[J]. Celestial Mechanics and Dynamical Astronomy, 2001, 79(1): 41-72.
    [27] SÁNCHEZ J, NET M. A parallel algorithm for the computation of invariant tori in large-scale dissipative systems[J]. Physica D: Nonlinear Phenomena, 2013, 252: 22-33.
    [28] VILLEGAS-PINTO D, BARESI N, HESTROFFER D, et al. On the numerical computation of quasi-periodic families and applications to the Martian Moons exploration mission[C]//Proceedings of the International Conference on Astrodynamics Tools and Techniques. Paris : European Space Agency , 2021.
  • 加载中
图(15) / 表(2)
计量
  • 文章访问数:  348
  • HTML全文浏览量:  125
  • PDF下载量:  40
  • 被引次数: 0
出版历程
  • 收稿日期:  2024-01-25
  • 录用日期:  2024-03-13
  • 网络出版日期:  2024-03-27
  • 整期出版日期:  2026-04-30

目录

    /

    返回文章
    返回
    常见问答