• Laser & Optoelectronics Progress
  • Vol. 58, Issue 4, 0428002 (2021)
Mu Yang*, Shaoyuan Cheng, Chengguang Cui, Hongchen Tang, and Zhihao Zhu
Author Affiliations
  • Beijing Institute of Space Mechanics and Electricity, Beijing 100094, China
  • show less
    DOI: 10.3788/LOP202158.0428002 Cite this Article Set citation alerts
    Mu Yang, Shaoyuan Cheng, Chengguang Cui, Hongchen Tang, Zhihao Zhu. Ground Experimental System for Satellite Dynamic Imaging Mode[J]. Laser & Optoelectronics Progress, 2021, 58(4): 0428002 Copy Citation Text show less
    Schematic diagram of the experimental system. (a) Geometric relationship of the on-orbit imaging; (b) top view
    Fig. 1. Schematic diagram of the experimental system. (a) Geometric relationship of the on-orbit imaging; (b) top view
    Relationship between target rotation speed and satellite maneuvering angular speed along flight direction
    Fig. 2. Relationship between target rotation speed and satellite maneuvering angular speed along flight direction
    Schematic of the ground experiment system
    Fig. 3. Schematic of the ground experiment system
    Static imageing of the target. (a) Design drawing of the target; (b) physical photo corresponding to the dotted frame
    Fig. 4. Static imageing of the target. (a) Design drawing of the target; (b) physical photo corresponding to the dotted frame
    Relationship between dynamic MTF and light intensity
    Fig. 5. Relationship between dynamic MTF and light intensity
    Dynamic imaging of the target. (a) Change of dynamic MTF with the angular velocity of the target; (b) dynamic image with 128 levels and a rotation speed of 800 (°)/s
    Fig. 6. Dynamic imaging of the target. (a) Change of dynamic MTF with the angular velocity of the target; (b) dynamic image with 128 levels and a rotation speed of 800 (°)/s
    Result of the dynamic imaging. (a) Variation curve of the integration time ; (b) partial images of the target dynamic imaging
    Fig. 7. Result of the dynamic imaging. (a) Variation curve of the integration time ; (b) partial images of the target dynamic imaging
    Index nameIndex value
    Pixel size of detector/μm7
    Focal length of camera/mm4400
    Camera aperture/mm440
    Focal length of collimator/mm6000
    Collimator aperture/mm600
    Target radius/ mm160
    Spatial frequency of target pair/(lp·mm-1)26.31
    Target rotation speed/[ (°)·s-1]17.9-1791.4
    Table 1. Main parameters of the experimental system
    Speed/[(°)·s-1]326496128
    130180-34290-17160-11445-85
    170720-798210-399140-266105-199
    230780-1482390-741260-494195-370
    7603960-75241980-37621320-2508990-1881
    8004200-79802100-39901400-26601050-1995
    Table 2. Linear regions under different parameter combinations
    Detector stageMean valueStandard deviation
    320.10240.0120
    640.10540.0173
    960.10000.0124
    1280.09180.0128
    Table 3. Mean value and standard deviation value of dynamic MTF at different detector stage
    Mu Yang, Shaoyuan Cheng, Chengguang Cui, Hongchen Tang, Zhihao Zhu. Ground Experimental System for Satellite Dynamic Imaging Mode[J]. Laser & Optoelectronics Progress, 2021, 58(4): 0428002
    Download Citation