Infrared and Laser Engineering, Volume. 50, Issue 4, 20200241(2021)

Optimal calculation method of aircraft infrared physical imaging simulation

Kun Yu, Yuhan Duan, Mingyu Cong, and Wencong Dai
Author Affiliations
  • Research Center for Space Optical Engineering, School of Astronautics, Harbin Institute of Technology, Harbin 150006, China
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    Figures & Tables(18)
    Schematic diagram of aircraft infrared imaging radiance transmission
    Flow chart of direct lighting reflection radiance calculation using multi-importance sampling
    Sampling distance distribution of line-of-sight transmittance sampling
    Schematic diagram of path radiance integral calculation based on line integration method
    Flow chart of exhaust plume radiance calculation using combining integration method
    Calculation relative errors of emissive radiation intensity experiments of skin
    Calculation relative errors of reflective radiation intensity experiments of skin
    Reflective radiance simulation images of skin
    Calculation relative errors of emissive radiation intensity experiments of thick medium
    Calculation relative errors of emissive radiation intensity experiments of thin medium
    Emissive radiance simulation images of exhaust plume
    Simulation calculation results of stealth aircraft flow field
    Geometric relationship of stealth aircraft simulation imaging. (a) Ground-based detection scene; (b) Air-based detection scene; (c) Line of detection sight
    Simulation calculation results of infrared radiation intensity of stealth aircraft
    Infrared radiance simulation images of stealth aircraft
    • Table 1. [in Chinese]

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      Table 1. [in Chinese]

      Number of sampling rays/pixelRRMSE by BRDF samplingRRMSE by direct lighting sampling
      1114.289%49.394%
      1093.754%16.324%
      10031.998%5.222%
      100010.353%1.785%
      100003.640%0.852%
    • Table 2. [in Chinese]

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      Table 2. [in Chinese]

      Number of sampling rays/pixelRRMSE by point integration RRMSE by line integrationRRMSE by combining integration
      1191.570%6.715%5.580%
      10113.819%1.687%1.620%
      10058.461%0.652%0.638%
      100019.159%0.299%0.020%
    • Table 3. [in Chinese]

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      Table 3. [in Chinese]

      ParameterValue
      Atmospheric pressure/Pa3×104
      Atmospheric temperature/K255
      Atmospheric compositionFluent ideal atmosphere model
      Short-waveband solar radiance/W·sr−1·m−210.0
      Short-waveband solar direction-Z axis of target body coordinate system
      Flight height/km10
      Flight speed/Ma1.0
      Skin BRDFLambert
      Skin materialAluminum alloy
      Engine inlet diameter/m1.4
      Engine inlet temperature/K650
      Engine inlet pressure/Pa2×105
      Engine outlet diameter/m0.5
      Fuel typeC5H12
      Fuel temperature/K300
      Fuel mass flow/kg·s−10.15
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    Kun Yu, Yuhan Duan, Mingyu Cong, Wencong Dai. Optimal calculation method of aircraft infrared physical imaging simulation[J]. Infrared and Laser Engineering, 2021, 50(4): 20200241

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    Paper Information

    Category: Infrared technology and application

    Received: Jun. 22, 2020

    Accepted: --

    Published Online: Jul. 30, 2021

    The Author Email:

    DOI:10.3788/IRLA20200241

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