Chinese Journal of Lasers, Volume. 49, Issue 9, 0910001(2022)

Pitch Attitude Sensitivity of Photon Detection Echo of Moving Airborne Targets

Fanghui Qu1,2、*, Yihua Hu1,2、**, Shilong Xu1,2、***, and Ahui Hou1,2
Author Affiliations
  • 1State Key Laboratory of Pulsed Power Laser Technology, National University of Defense Technology, Hefei 230037, Anhui, China
  • 2Anhui Key Laboratory of Electronic Control Technology, National University of Defense Technology, Hefei 230037, Anhui, China
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    Figures & Tables(12)
    Extended target coordinate system for photon ranging
    Three kinds of targets and their respective photon echoes in the attitude angle range from 0° to 90°. (a) Three kinds of targets; (b) target echoes in the range from 0° to 30°;(c) target echoes in the range from 30° to 60°;(d) target echoes in the range from 60° to 90°
    Waveform similarity of any two photon echoes at 0°360° attitude angle. (a) F18; (b) F22; (c) F35
    Variation of average echo waveform difference of three targets with attitude angle interval
    Attitude influence level of echo waveform difference. (a) Photon echo waveform difference at any attitude angle interval; (b) attitude influence level distribution function
    Attitude influence level of kurtosis difference. (a) Photon echo kurtosis difference at any attitude angle interval; (b) attitude influence level distribution function
    Attitude influence level of skewness difference. (a) Photon echo skewness difference at any attitude angle interval; (b) attitude influence level distribution function
    Attitude influence level of central moment difference. (a) Central moment difference of photon echo at any attitude angle interval; (b) attitude influence level distribution function
    Experimental equipment and target models. (a) Experimental field photo; (b) three-dimensional point cloud image of J-15; (c) three-dimensional point cloud image of SU-35
    Attitude influence level of echo difference of experimental targets. (a) Attitude influence level distribution function of echo waveform difference;(b) attitude influence level distribution function of central moment difference; (c) attitude influence level distribution function of kurtosis difference; (d) attitude influence level distribution function of skewness difference
    • Table 1. Parameters of target model

      View table

      Table 1. Parameters of target model

      ModelModel size /(mm×mm×mm)
      F1816.49×4.65×11.55
      F2219.62×4.5×14.3
      F3515.73×3.96×10.83
    • Table 2. Influence level analysis of photon echo attitude

      View table

      Table 2. Influence level analysis of photon echo attitude

      Attitude influence levelF18F22F35
      Photon echo waveformMean0.34820.39490.2783
      Median0.32540.41980.2708
      Standard deviation0.17920.17500.1409
      KurtosisMean0.18230.20100.0930
      Median0.18240.21280.0962
      Standard deviation0.07490.07110.0309
      SkewnessMean0.14380.13740.0661
      Median0.14420.13950.0702
      Standard deviation0.05460.05060.0222
      Second momentMean0.19590.16020.0821
      Median0.21590.18460.0832
      Standard deviation0.21590.18460.0832
      Third momentMean0.39510.31390.1763
      Median0.42100.36090.1807
      Standard deviation0.17920.14150.0673
      Fourth momentMean0.48530.41510.2314
      Median0.51730.46210.2369
      Standard deviation0.21660.15610.0865
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    Fanghui Qu, Yihua Hu, Shilong Xu, Ahui Hou. Pitch Attitude Sensitivity of Photon Detection Echo of Moving Airborne Targets[J]. Chinese Journal of Lasers, 2022, 49(9): 0910001

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    Paper Information

    Received: Aug. 25, 2021

    Accepted: Oct. 25, 2021

    Published Online: Apr. 22, 2022

    The Author Email: Qu Fanghui (qfh_goubaby@163.com), Hu Yihua (skl_hyh@163.com), Xu Shilong (xushi1988@yeah.net)

    DOI:10.3788/CJL202149.0910001

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