Infrared and Laser Engineering, Volume. 54, Issue 6, 20240574(2025)

Research on the on-orbit calibration method for spaceborne infrared spectral imager using dual blackbodies

Yunmeng LIU1,2,3, Yang WANG1,3, Lei DING1,3、*, Huixian DUAN1,3, and Jinguang CHAI1,3
Author Affiliations
  • 1Shanghai Institute of Technical Physics Chinese Academy of Sciences, Shanghai 200083, China
  • 2University of Chinese Academy of Sciences, Beijing 100049, China
  • 3Technology Innovation Center of Metrology Technology of Infrared Remote Sensing, State Administration for Market Regulation, Beijing 102200, China
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    Figures & Tables(14)
    The positions of on-board blackbody and low-temperature blackbody on the equipment
    Two-point linear fitting result through "low-temperature blackbody + on-board blackbody"
    The temperature deviation of different radiation targets through "low-temperature blackbody (240 K)+on-board blackbody (290 K)"
    The temperature deviation of different radiation targets through "low-temperature blackbody (250 K)+on-board blackbody (290 K)"
    Two-point linear fitting result through "on-board blackbody (290 K)+ cold space"
    The temperature deviation of different radiation targets through "on-board blackbody (290 K) +cold space"
    Two-point linear fitting result through "low-temperature blackbody (250 K)+ cold space"
    The temperature deviation of different radiation targets through "low-temperature blackbody (250 K) +cold space"
    The signals of cold space,low-temperature blackbody and on-board blackbody
    The temperature difference distribution for the multiple Earth targets between Method 2-Method 1 and Method 3-Method 1
    The temperature difference distribution for the Earth target between Method 2-Method 1 and Method 3-Method 1
    The temperature difference distribution for the multiple Earth targets between Method 2-Method 1 and Method 3-Method 1
    The temperature difference distribution for the Earth target between Method 2-Method 1 and Method 3-Method 1
    • Table 1. The responsive ratio consistency of the dual blackbody before and after launch

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      Table 1. The responsive ratio consistency of the dual blackbody before and after launch

      Comparison10.8 μm12 μm
      On orbitVacuumOn orbitVacuum
      Responsivity of on-board blackbody19.0418.8117.5817.08
      Responsivity of low-temperature blackbody18.8618.7317.4617.01
      Γ1.00971.00451.0071.004
      H1.0051.003
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    Yunmeng LIU, Yang WANG, Lei DING, Huixian DUAN, Jinguang CHAI. Research on the on-orbit calibration method for spaceborne infrared spectral imager using dual blackbodies[J]. Infrared and Laser Engineering, 2025, 54(6): 20240574

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    Paper Information

    Category: Infrared

    Received: Jan. 12, 2025

    Accepted: --

    Published Online: Jul. 1, 2025

    The Author Email:

    DOI:10.3788/IRLA20240574

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