Journal of Applied Optics, Volume. 43, Issue 4, 592(2022)

Target location accuracy analysis on loitering missile platform

Zhaoqing LIU... Fang ZHANG*, Lei ZHU, Zhaohui JIA, Jianghua WEN, Chuan QIN and Lanlan ZHANG |Show fewer author(s)
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    Figures & Tables(8)
    Relative position of target and electro-optical system in airborne coordinate system
    Influence of horizontal positioning error of global positioning system on CEP
    Influence of course error of inertial navigation system on CEP
    Influence of rangefinder on CEP
    Influence of angle measurement error on CEP
    • Table 1. Positioning error and weight analysis caused by each parameter error

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      Table 1. Positioning error and weight analysis caused by each parameter error

      Parametererror(1σ)CEP/ mInfluence weight/%Influence weight/%
      level error=5 mlevel error=1 m
      Aircraft longitude5 m815.53-
      1 m2.7-6.63
      Aircraft latitude5 m917.47-
      1 m3.5-8.60
      INS heading0.1°713.5917.19
      Rangefinder ranging1 m2.75.246.63
      Pitching angle0.003°2.354.565.77
      Azimuth angle0.003°2.224.305.45
    • Table 2. Target location error (satellite horizontal positioning error is 5 m)

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      Table 2. Target location error (satellite horizontal positioning error is 5 m)

      NOTarget longitude/(°)Target latitude/(°)Longitude error/(°)Latitude error/(°)Longitude absolute error/mLatitude absolute error/°
      1109.588799840.87350362.35639E-05−0.0001465452.115.8
      2109.588784840.87349998.56389E-06−0.0001502450.816.2
      3109.588773540.8733537−2.73611E-06−0.0002964450.232.0
      4109.588773440.8733853−2.83611E-06−0.0002648450.328.6
      5109.588780040.87334333.76389E-06−0.0003068450.333.1
      6109.588781940.87335505.66389E-06−0.0002951450.531.9
      7109.588750640.8732282−2.56361E-05−0.0004219452.345.6
      8109.588747940.8732207−2.83361E-05−0.0004294452.646.4
      9109.588731340.8731303−4.49361E-05−0.0005198454.056.1
      10109.588709540.8730071−6.67361E-05−0.0006430456.069.4
    • Table 3. Target location error (satellite horizontal positioning error is 1 m)

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      Table 3. Target location error (satellite horizontal positioning error is 1 m)

      NOTarget longitude/(°)Target latitude/(°)Longitude error/(°)Latitude error/(°)Longitude absolute error/mLatitude absolute error/m
      1109.588789640.87393231.33639E-050.0002821551.230.5
      2109.588795940.87395721.96639E-050.0003070551.833.2
      3109.588801340.87391002.50639E-050.0002598552.328.1
      4109.588792540.87392421.62639E-050.0002740551.529.6
      5109.588783140.87377976.86389E-060.0001295550.614.0
      6109.588790340.87391501.40639E-050.0002648551.328.6
      7109.588783240.87386636.96389E-060.0002161550.623.3
      8109.588776140.8738237−1.36111E-070.0001735550.018.7
      9109.588763440.8737240−1.28361E-057.38550E-051.28.0
      10109.588772940.8738116−3.33611E-060.0001614550.317.4
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    Zhaoqing LIU, Fang ZHANG, Lei ZHU, Zhaohui JIA, Jianghua WEN, Chuan QIN, Lanlan ZHANG. Target location accuracy analysis on loitering missile platform[J]. Journal of Applied Optics, 2022, 43(4): 592

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    Paper Information

    Category: OE SYSTEM AND ENGINEERING

    Received: May. 19, 2022

    Accepted: --

    Published Online: Aug. 10, 2022

    The Author Email: ZHANG Fang (zf2511@163.com)

    DOI:10.5768/JAO202243.0401002

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