AEROSPACE SHANGHAI, Volume. 41, Issue 5, 44(2024)

Research on Optimal Selection of Optical Information Under the Fusion Positioning of Angle Measurement and Navigation Satellite Ranging for Deep Space Probe

Jing LIU*... Shengying ZHU, Pingyuan CUI and Yanjie LIU |Show fewer author(s)
Author Affiliations
  • School of Aerospace Engineering,Beijing Institute of Technology, Beijing100081, China
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    Figures & Tables(7)
    The positioning scheme
    The astronomical angle measurement navigation
    Position error ellipse for angle measurement positioning
    Effect of optimal selection on the angle measurement positioning
    Position error ellipse under the fusion positioning of angle measurement and navigation satellite ranging
    Effect of optimal selection under the fusion positioning
    • Table 1. Simulation parameter setting

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      Table 1. Simulation parameter setting

      参数数值
      探测器位置/m[-3 349 050.00,-10 307 316.05,2 774 088.80]
      初始位置偏差/m[5 000,5 000,5 000]
      导航星位置/m[-1 158 839.20,-3 236 512.38,1 610 345.85]
      远天体数量15
      近天体数量5
      初始种群数量30
      遗传代数30
      交叉概率0.8
      变异概率0.1
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    Jing LIU, Shengying ZHU, Pingyuan CUI, Yanjie LIU. Research on Optimal Selection of Optical Information Under the Fusion Positioning of Angle Measurement and Navigation Satellite Ranging for Deep Space Probe[J]. AEROSPACE SHANGHAI, 2024, 41(5): 44

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    Paper Information

    Category: Deep-Space Exploration

    Received: Jul. 4, 2024

    Accepted: --

    Published Online: Jan. 15, 2025

    The Author Email:

    DOI:10.19328/j.cnki.2096-8655.2024.05.005

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