Infrared and Laser Engineering, Volume. 52, Issue 5, 20220671(2023)

Influence of different altitudes on deviation of aero-optics imaging of 0°-15° angle of attack

Liang Xu1, Luyang Wang1, Ziming Wan2, Shiwei Zhao1, Liye Zhou1, and Tao Wang3、*
Author Affiliations
  • 1Tianjin Key Laboratory of Complex Control Theory and Application, School of Electronic Engineering and Automation, Tianjin University of Technology, Tianjin 300384, China
  • 2Beijing Institute of General Electronics Engineering, Beijing 100039, China
  • 3School of Intelligent Engineering, Sun Yat-sen University, Shenzhen 518107, China
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    Figures & Tables(15)
    Flowchart of numerical simulation of computational fluid dynamics
    (a) 2D model; (b) 3D model; (c) Meshing of 3D model
    Three-dimensional relative motion relationship between the missile and the target
    Average flow field density distribution in the head of the vehicle at different altitudes (Sample 1)
    Average flow field density distribution in the head of the vehicle at different altitudes (Sample 2)
    Refractive index distributions of backward ray tracing at different altitudes (Sample 3)
    Aero-optics imaging deviation (Sample 4)
    Aero-optics imaging deviation slope (Sample 4)
    Aero-optics imaging deviation (Sample 5)
    Aero-optics imaging deviation slope (Sample 5)
    Aero-optics imaging deviation (Sample 6)
    Aero-optics imaging deviation slope (Sample 6)
    • Table 1. Distribution of pressure, temperature, and density with altitudes

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      Table 1. Distribution of pressure, temperature, and density with altitudes

      ${{Z/\rm km} }$${{p/\rm Pa} }$${{T/\rm K} }$$\rho /{\rm{kg} }\cdot{ {\rm{m} }^{-3}}$
      01.01325×105288.1501.2250
      55.4048×104255.6767.3643×10−1
      102.6499×104223.2524.1351×10−1
      151.2111×104216.6501.9476×10−1
      205.5293×103216.6508.8910×10−2
      252.5492×103221.5524.0084×10−2
    • Table 2. Range of flight parameters calculated by simulation

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      Table 2. Range of flight parameters calculated by simulation

      Flight parametersRangeInterval
      Altitude0-25/km5
      Mach number0.5-30.5
      AOA0-15/(°)1
      LOSR angle/(°)5
      LOS angle/(°)35
    • Table 3. Flight condition

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      Table 3. Flight condition

      SampleAltitude/ km Mach number/MaAOA/ (°) LOSR angle/(°) LOS angle/(°)
      10-251.55535
      210
      320
      41.50-15
      52
      63
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    Liang Xu, Luyang Wang, Ziming Wan, Shiwei Zhao, Liye Zhou, Tao Wang. Influence of different altitudes on deviation of aero-optics imaging of 0°-15° angle of attack[J]. Infrared and Laser Engineering, 2023, 52(5): 20220671

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    Paper Information

    Category: Photoelectric measurement

    Received: Sep. 15, 2022

    Accepted: --

    Published Online: Jul. 4, 2023

    The Author Email:

    DOI:10.3788/IRLA20220671

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