• Journal of Atmospheric and Environmental Optics
  • Vol. 18, Issue 4, 281 (2023)
LI Yingjie, GUAN Xin, WEN Yuan, ZHANG Miaomiao, GUI Lijia, and LI Yunduan*
Author Affiliations
  • Shanghai Institute of Satellite Engineering, Shanghai 201109, China
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    DOI: 10.3969/j.issn.1673-6141.2023.04.003 Cite this Article
    Yingjie LI, Xin GUAN, Yuan WEN, Miaomiao ZHANG, Lijia GUI, Yunduan LI. Design of lunar calibration mode of hyperspectral observation satellite[J]. Journal of Atmospheric and Environmental Optics, 2023, 18(4): 281 Copy Citation Text show less
    The relationship between the white, the ecliptic and the earth's equator
    Fig. 1. The relationship between the white, the ecliptic and the earth's equator
    Diagram of lunar phase
    Fig. 2. Diagram of lunar phase
    The diagram of lunar phase angle
    Fig. 3. The diagram of lunar phase angle
    The curve diagram of lunar phase angle of hyperspectral observation satellite throughout the year
    Fig. 4. The curve diagram of lunar phase angle of hyperspectral observation satellite throughout the year
    Satellite-moon vector diagram
    Fig. 5. Satellite-moon vector diagram
    Geometric relationship diagram of rolling attitude maneuver to the moon
    Fig. 6. Geometric relationship diagram of rolling attitude maneuver to the moon
    Schematic diagram of rolling attitude maneuvering lunar calibration window
    Fig. 7. Schematic diagram of rolling attitude maneuvering lunar calibration window
    Angle between earth-moon vector and satellite orbital plane
    Fig. 8. Angle between earth-moon vector and satellite orbital plane
    Geometric relationship diagram of pitch attitude maneuver to the moon
    Fig. 9. Geometric relationship diagram of pitch attitude maneuver to the moon
    Lunar calibration observation window and maneuvering angle
    Fig. 10. Lunar calibration observation window and maneuvering angle
    Attitude angle
    Fig. 11. Attitude angle
    Attitude angle velocity
    Fig. 12. Attitude angle velocity
    The angle between star sensor optical axis vector and the sun vector
    Fig. 13. The angle between star sensor optical axis vector and the sun vector
    The illumination angle of the nightside during attitude maneuver
    Fig. 14. The illumination angle of the nightside during attitude maneuver
    The illumination angle of solar panel during attitude maneuver
    Fig. 15. The illumination angle of solar panel during attitude maneuver
    Lunar calibration timing chart
    Fig. 16. Lunar calibration timing chart

    Rolling attitude

    maneuver angle/(°)

    Beta angle/(°)

    Lunar phase angle in light

    area/(°)

    Lunar phase angle in shadow area/(°)
    -62.322.5-39.8-95.2
    -64.222.5-41.7-93.3
    -66.6322.5-44.13-90.87
    -6722.5-44.5-90.5
    -7022.5-47.5-87.5
    62.322.584.8140.2
    64.222.586.7138.3
    66.6322.589.13135.87
    6722.589.5135.5
    7022.592.5132.5
    Table 1. Lunar phase angle under different rolling maneuver angles
    Satellite external surfaceNormal external heat/WExternal heat during lunar calibration/WChange/%
    Propelling module floor150.9150.0-0.61
    Propelling module III quadrant side plate49.251.85.29
    Propelling module IV quadrant side plate22.023.04.53
    Service module I quadrant side plate77.870.7-9.01
    Service module III quadrant side plate135.6142.45.00
    Service module IV quadrant side plate90.894.94.52
    Payload module III quadrant side plate39.841.85.03
    Payload module IV quadrant side plate89.793.84.57
    Sum684.6698.62.04
    Table 2. External heat curve of the satellite
    Yingjie LI, Xin GUAN, Yuan WEN, Miaomiao ZHANG, Lijia GUI, Yunduan LI. Design of lunar calibration mode of hyperspectral observation satellite[J]. Journal of Atmospheric and Environmental Optics, 2023, 18(4): 281
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