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稀疏观测模式的“嫦娥四号”中继星轨道确定

Determination of the Orbit of Chang’E-4 Relay Satellite Under Sparse Observation

  • 摘要: “嫦娥四号”中继星于2018年6月14日成功进入地月L2点Halo轨道,承担地面测控站与“嫦娥四号”着陆器的数据传输功能。目前“嫦娥四号”中继星处于稀疏观测模式,平均4~5天进行一次观测。分析了2021年1月“嫦娥四号”中继星绕地月L2点的定轨精度,结果表明:中继星绕L2点轨道精度优于2 km,包含有甚长基线干涉测量技术(Very Long Baseline Interferometry, VLBI)时延和时延率的弧段达到百米量级;在有VLBI观测的前提下,合理分配测距和测速弧段的覆盖时段,能在数据覆盖率相同的情况下有效提高轨道精度。

     

    Abstract: Chang’E-4 relay satellite successfully entered the Earth-Moon L2 Halo orbit on June 14, 2018, and assumed the data transmission function between the ground-based measurement and control station and Chang’E-4 lander. At present, Chang’E-4 relay satellite is in sparse observation mode, with an average of 4~5 days for each observation. This paper analyzes the orbit determination accuracy of Chang’E-4 relay satellite circling the Earth-Moon L2 in January 2021. The orbit accuracy of the relay satellite around the L2 point is better than 2km, and the arc including the VLBI delay and delay rate reaches the level of 100 meters. Under the premise of VLBI observation, reasonable allocation of the coverage period of the ranging and velocity measurement arcs can effectively improve the orbit accuracy under the same data coverage.

     

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