Acta Photonica Sinica, Volume. 53, Issue 8, 0811003(2024)

Analysis of Imaging Limit Capability for Natural Rendezvous of Low Earth Orbit Debris

Yaru LI1...2,3, Liang ZHOU1,3,*, Zhaohui LIU1,3, Wenji SHE1,3, and Kai CUI1,23 |Show fewer author(s)
Author Affiliations
  • 1Xi′an Institute of Optics and Precision Mechanics of Chinese Academy of Sciences, Xi'an 710119, China
  • 2University of Chinese Academy of Sciences, Beijing 100049, China
  • 3Key Laboratory of Space Precision Measurement Technology, Chinese Academy of Sciences, Xi'an 710119, China
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    Figures & Tables(12)
    Schematic diagram of the close-range imaging scene before and after the moment of rendezvous
    The target state under the camera line-of-sight direction before and after the rendezvous moment
    Flow chart of coordinate transformation from spatial target points to image points
    The relationship betweenVr,Laxis,ωrot and p within ±10 s of rendezvous moment
    The relationship between different variables and image motion
    Comparison of theoretical calculated values and fitted values of image motion for different orbits
    Different image motion correspond to imaging results
    The relationship between spatial resolution and intrinsic image motion
    • Table 1. Imaging platform and space target orbit parameters used for model construction

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      Table 1. Imaging platform and space target orbit parameters used for model construction

      OrbitSemi major axis a/kmEccentricity eInclination i/(°)Argument of perigee ω/(°)Right ascension of the ascending node Ω/(°)Mean anomaly M/(°)
      Platform (A)7 103.4900.053 256 498.566 538.606 03.375 218.970 0
      Target (A)7 006.7070.052 186 297.864 1120.527 7325.149 0278.301 8
      Platform (B)7 005.4900.053 256 498.566 538.606 03.375 2309.860 0
      Target (B)6 994.3370.051 489 297.892 9128.579 490.906 4224.438 0
      Platform (C)6 968.4900.053 256 498.566 538.606 03.375 2315.880 0
      Target (C)6 782.4780.001 680 773.566 1228.144 399.822 3349.244 8
    • Table 2. Fitting accuracy of image motion for respective orbits

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      Table 2. Fitting accuracy of image motion for respective orbits

      Orbitθ/Sres/pτ/Sres/pτ/Sres/pω/θ/p
      R2RMSER2RMSER2RMSER2RMSE
      A0.9990.0830.9990.1460.9970.0640.9950.043
      B0.9950.0960.9940.2170.9840.0790.9860.029
      C0.9970.0590.9980.1630.9900.0480.9830.028
    • Table 3. MTF reduction under different image motion

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      Table 3. MTF reduction under different image motion

      Image motion/pixelPercentage declineImage motion/pixelPercentage decline
      0.21.64%0.824.3%
      0.33.66%136.32%
      0.59.96%1.569.96%
    • Table 4. Imaging platform and target orbit parameters used for model accuracy verification

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      Table 4. Imaging platform and target orbit parameters used for model accuracy verification

      Orbita/kmei/(°)ω/(°)Ω/(°)M/(°)
      Platform6 775.4900.003 256 438.566 538.606 03.375 2326.400 0
      Target6 801.6760.003 753 597.098 3192.342 819.794 0166.801 0
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    Yaru LI, Liang ZHOU, Zhaohui LIU, Wenji SHE, Kai CUI. Analysis of Imaging Limit Capability for Natural Rendezvous of Low Earth Orbit Debris[J]. Acta Photonica Sinica, 2024, 53(8): 0811003

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    Paper Information

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    Received: Dec. 27, 2023

    Accepted: Mar. 11, 2024

    Published Online: Oct. 15, 2024

    The Author Email: ZHOU Liang (zhouliang@opt.ac.cn)

    DOI:10.3788/gzxb20245308.0811003

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