• Infrared and Laser Engineering
  • Vol. 52, Issue 5, 20220671 (2023)
Liang Xu1, Luyang Wang1, Ziming Wan2, Shiwei Zhao1..., Liye Zhou1 and Tao Wang3,*|Show fewer author(s)
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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    DOI: 10.3788/IRLA20220671 Cite this Article
    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 Copy Citation Text show less
    Flowchart of numerical simulation of computational fluid dynamics
    Fig. 1. Flowchart of numerical simulation of computational fluid dynamics
    (a) 2D model; (b) 3D model; (c) Meshing of 3D model
    Fig. 2. (a) 2D model; (b) 3D model; (c) Meshing of 3D model
    Three-dimensional relative motion relationship between the missile and the target
    Fig. 3. 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)
    Fig. 4. 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)
    Fig. 5. 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)
    Fig. 6. Refractive index distributions of backward ray tracing at different altitudes (Sample 3)
    Aero-optics imaging deviation (Sample 4)
    Fig. 7. Aero-optics imaging deviation (Sample 4)
    Aero-optics imaging deviation slope (Sample 4)
    Fig. 8. Aero-optics imaging deviation slope (Sample 4)
    Aero-optics imaging deviation (Sample 5)
    Fig. 9. Aero-optics imaging deviation (Sample 5)
    Aero-optics imaging deviation slope (Sample 5)
    Fig. 10. Aero-optics imaging deviation slope (Sample 5)
    Aero-optics imaging deviation (Sample 6)
    Fig. 11. Aero-optics imaging deviation (Sample 6)
    Aero-optics imaging deviation slope (Sample 6)
    Fig. 12. Aero-optics imaging deviation slope (Sample 6)
    ${{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 1. Distribution of pressure, temperature, and density with altitudes
    Flight parametersRangeInterval
    Altitude0-25/km5
    Mach number0.5-30.5
    AOA0-15/(°)1
    LOSR angle/(°)5
    LOS angle/(°)35
    Table 2. Range of flight parameters calculated by simulation
    SampleAltitude/ km Mach number/MaAOA/ (°) LOSR angle/(°) LOS angle/(°)
    10-251.55535
    210
    320
    41.50-15
    52
    63
    Table 3. Flight condition
    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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