Spacecraft Recovery & Remote Sensing, Volume. 45, Issue 2, 53(2024)

Visibility Analysis of the Cislunar Periodic Orbit for the Halo Orbits near the Earth-Moon L1 and L2 Points

Xingming LI, Linli GUO, Ruimin FU, Guoxian ZHENG, Peipei WANG, and Lianqing DONG
Author Affiliations
  • Beijing Institute of Space Mechanics & Electricity, Beijing 100094, China
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    Figures & Tables(15)
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    • Table 1. The selected cislunar periodic orbit related indicators

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      Table 1. The selected cislunar periodic orbit related indicators

      轨道编号1T内卫星覆盖目标区域时间占比/%最大连续观测间隔/d1T内目标最佳探测时间占比/%观测角度范围/(°)
      L1L2L1L2L1L2L1L2
      165.1677.397.057.08010.93[7.7, 42.4][6.7, 145.2]
      276.8280.4610.0710.0812.488.91[8.0, 98.2][7.0, 83.5]
      359.8872.0732.5932.6019.5110.54[9.0, 152.4][7.6, 175.4]
    • Table 2. Initial state of the selected cislunar periodic orbit

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      Table 2. Initial state of the selected cislunar periodic orbit

      轨道编号${{{x}}_0}$/LU${{{y}}_0}$/LU${{\textit{z}}_0}$/LU${{\dot {{x}}}_0}$/VU${{\dot {{y}}}_0}$/VU${{{{\dot{ \textit {z}}}}}_0}$/VU${{{T}}_0}$/TU
      11.200 0000−1.049 606.192
      20.976 5000−1.677 3012.331
      31.000 0000−1.497 6017.785
    • Table 3. Summary of activities around the Halo Orbit

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      Table 3. Summary of activities around the Halo Orbit

      国家时间卫星轨道及任务类型
      美国2007年ARTEMIS P1/P2卫星位于L2李萨如轨道,验证轨道稳定性并观测月球磁场
      美国2022年CAPSTONE立方星运行于近直线Halo轨道,验证稳定性
      美国2022年Orion 多用途飞船运行于DRO轨道及绕月轨道,实现载人登月
      美国2022年Lunar Flashlight立方星拟运行于NRHO轨道,寻找月球水冰
      美国计划2025年Lunar Gateway空间站运行于NRHO轨道,提供地月空间驻留
      中国2018年“鹊桥”中继卫星位于L2 Halo轨道运行,提供中继通信支持
      中国2024年“鹊桥”通导遥星座系统“鹊桥二号”卫星位于大椭圆近月轨道上,提供中继通信服务,协同的“天都一号”、“天都二号”立方星用于开展轨道高精度定轨等技术验证
    • Table 4. Initial state of the selected Halo Orbit

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      Table 4. Initial state of the selected Halo Orbit

      轨道名称${{{x}}_0}$/LU${{{y}}_0}$/LU${{\textit{z}}_0}$/LU${{\dot {{x}}}_0}$/VU${{\dot{{ y}}}_0}$/VU${{\dot {\textit{z}}}_0}$/VU${{{T}}_0}$/TU
      L1 Halo轨道0.835 500.142 400.256 702.760
      L2 Halo轨道1.179 200.040 00−0.164 503.402
    • Table 5. Lunar motion parameter configuration

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      Table 5. Lunar motion parameter configuration

      名称数值
      轨道半径/km390 877.415 821 268 572 472
      轨道半径变化率/(km∙s−1)0
      偏心率0
      偏心率变化率/s−10
      轨道倾角/(°)21.681 031 148 349 923
      轨道倾角变化率/((°)/s)0
      升交点赤经/(°)12.619 042 020 544 290
      升交点赤经变化率/((°)/s)0
      近心点经度/(°)127.822 863 094 449 474
      近心点经度变化率/((°)/s)0
      平经度/(°)323.551 110 877 871 110
      平经度变化率/((°)/s)0.000 148 023 494 422 999
    • Table 6. Effect of natural body exclusion angles %

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      Table 6. Effect of natural body exclusion angles %

      轨道编号影响类别自然天体排斥角
      太阳排斥角地球排斥角月球排斥角排斥角影响总计
      轨道1L1 Halo轨道受影响占比16.4719.2921.7657.52
      L2 Halo轨道受影响占比16.9417.5435.7670.24
      轨道2L1 Halo轨道受影响占比16.0121.7220.0457.77
      L2 Halo轨道受影响占比16.0421.6933.7771.50
      轨道3L1 Halo轨道受影响占比17.166.3522.7646.27
      L2 Halo轨道受影响占比16.116.4340.1562.69
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    Xingming LI, Linli GUO, Ruimin FU, Guoxian ZHENG, Peipei WANG, Lianqing DONG. Visibility Analysis of the Cislunar Periodic Orbit for the Halo Orbits near the Earth-Moon L1 and L2 Points[J]. Spacecraft Recovery & Remote Sensing, 2024, 45(2): 53

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    Paper Information

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    Received: Dec. 5, 2023

    Accepted: --

    Published Online: May. 29, 2024

    The Author Email:

    DOI:10.3969/j.issn.1009-8518.2024.02.005

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