• Infrared and Laser Engineering
  • Vol. 49, Issue 5, 20190457 (2020)
Lu Qiang1、2、*
Author Affiliations
  • 1[in Chinese]
  • 2[in Chinese]
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    DOI: 10.3788/irla20190457 Cite this Article
    Lu Qiang. Thermal radiation stray light integration method of infrared camera in geostationary orbit[J]. Infrared and Laser Engineering, 2020, 49(5): 20190457 Copy Citation Text show less
    Schematic diagram of light path
    Fig. 1. Schematic diagram of light path
    Calculating process of instrument background radiation stray light for TRSLIM
    Fig. 2. Calculating process of instrument background radiation stray light for TRSLIM
    Thermal network model
    Fig. 3. Thermal network model
    External heat flow into the hood
    Fig. 4. External heat flow into the hood
    Temperature curve of primary mirror in one day
    Fig. 5. Temperature curve of primary mirror in one day
    Temperature gradient curve of primary mirror in one day
    Fig. 6. Temperature gradient curve of primary mirror in one day
    Radiation curve of instrument background radiation produced by primary mirror on detector in one day
    Fig. 7. Radiation curve of instrument background radiation produced by primary mirror on detector in one day
    Total instrument background radiation curve generated by optical-mechanical components on detector in one day
    Fig. 8. Total instrument background radiation curve generated by optical-mechanical components on detector in one day
    SCR curve formed by instrument background radiation in one day
    Fig. 9. SCR curve formed by instrument background radiation in one day
    Variation curve of SCR at band 3 in one day
    Fig. 10. Variation curve of SCR at band 3 in one day
    TimeTemperature/°CEmissivityM/( W/m2)
    12:00−1.30.040.049 0
    20:00−5.60.040.040 5
    6:002.30.040.057 2
    Table 1. Radiation calculation of primary mirror at different time in infrared band
    Cond_idNode 1Node 2Area*e*BijBijBji
    1COMET.9284COMET.67902.728 026e-050.018 5320.012 89
    2COMET.9284COMET.67915.640 484e-070.003 455 9210.002 322 2
    3COMET.9284COMET.73081.156 538e-060.013 559 960.001 076
    4COMET.9284COMET.73091.401 487e-060.007 363 9610.003 127 9
    ……
    N-3 COMET.9310COMET.73096.087 829E-085.18E-050.001 187
    N-2 COMET.9310COMET.73101.103 783E-060.009 397 840.004 149
    N-1 COMET.9310COMET.73116.306 837E-070.005 369 770.001 819
    NCOMET.9310COMET.73122.469 422E-060.002 102 5180.007 124
    Table 2. Energy transfer factor Bijof nodes of primary mirror to detector
    Cond_idNode 1Node 2BijEj/ (W/m2) E/(W/m2)
    1COMET.9284COMET.67790.005 853 20.000 7263.712E-04
    2COMET.9284COMET.67800.000 345 592 10.000 135
    3COMET.9284COMET.72700.003 559 960.000 532
    4COMET.9284COMET.72710.001 363 9610.000 289
    ……
    N-3 COMET.9310COMET.72715.18E-052.03E-06
    N-2 COMET.9310COMET.72720.009 397 840.000 368
    N-1 COMET.9310COMET.72730.000 536 9770.000 21
    NCOMET.9310COMET.72740.002 102 5188.24E-05
    Table 3. Radiation calculation of nodes of primary mirror on detector at 12:00
    Cond_idNode 1Node 2BijEj/(W/m2) E/(W/m2)
    1COMET.9284COMET.67790.005 853 20.000 5951.820E-04
    2COMET.9284COMET.67800.000 345 592 10.000 111
    3COMET.9284COMET.72700.003 559 960.000 435
    4COMET.9284COMET.72710.001 363 9610.000 236
    ……
    N-3 COMET.9310COMET.72715.18E-051.66E-06
    N-2 COMET.9310COMET.72720.009 397 840.000 302
    N-1 COMET.9310COMET.72730.000 536 9770.000 172
    NCOMET.9310COMET.72740.002 102 5186.75E-05
    Table 4. Radiation calculation of nodes of primary mirror on detector at 20:00
    Cond_idNode 1Node 2BijEj//(W/m2) E/(W/m2)
    1COMET.9284COMET.67790.005 853 20.000 8545.855E-04
    2COMET.9284COMET.67800.000 345 592 10.000 159
    3COMET.9284COMET.72700.003 559 960.000 625
    4COMET.9284COMET.72710.001 363 9610.000 339
    ……
    N-3 COMET.9310COMET.72715.18E-052.39E-06
    N-2 COMET.9310COMET.72720.009 397 840.000 433
    N-1 COMET.72730.000 536 9770.000 248
    NCOMET.9310COMET.72740.002 102 5189.69E-05
    Table 5. Radiation calculation of nodes of primary mirror on detector at 6:00
    TimeOn-orbit test valuesTRSLIMTSLAM
    Simulation valueErrors from on-orbit test valuesSimulation valueErrors from on-orbit test values
    3:000.0590.061.69%0.11289.83%
    8:000.0640.07415.63%0.13103.13%
    12:000.0780.09116.67%0.14484.62%
    15:000.0890.10315.73%0.189112.36%
    18:000.0950.10914.74%0.204114.74%
    22:000.0890.09810.11%0.179101.12%
    Table 6. Comparison of SCR from on-orbit measured, TRSLIM and TSLAM
    Lu Qiang. Thermal radiation stray light integration method of infrared camera in geostationary orbit[J]. Infrared and Laser Engineering, 2020, 49(5): 20190457
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