• Acta Optica Sinica
  • Vol. 40, Issue 21, 2122002 (2020)
Kexin Song1, Lei Zhang1、2, Xuezhi Jia1、2、*, and Zhiqiang Su1
Author Affiliations
  • 1Chang Guang Satellite Technology Co., Ltd., Changchun, Jilin 130102, China
  • 2Changchun Institute of Optics, Fine Mechanics and Physics, Chinese Academy of Sciences, Changchun, Jilin 130022, China
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    DOI: 10.3788/AOS202040.2122002 Cite this Article Set citation alerts
    Kexin Song, Lei Zhang, Xuezhi Jia, Zhiqiang Su. Carbon Fiber Truss Support Technology for JL-1 Light High Resolution Space Camera[J]. Acta Optica Sinica, 2020, 40(21): 2122002 Copy Citation Text show less
    Schematic of positional relationship between primary and secondary mirrors
    Fig. 1. Schematic of positional relationship between primary and secondary mirrors
    Configuration of secondary mirror support structure. (a) Thin-walled tube type; (b) thin-walled tube truss combined type
    Fig. 2. Configuration of secondary mirror support structure. (a) Thin-walled tube type; (b) thin-walled tube truss combined type
    Size optimization strategy of main bearing system. (a) Main bearing structure; (b) tube wall structure; (c) limit force state of thin-walled tube; (d) truss cross-sectional configuration; (e) single truss limit force state
    Fig. 3. Size optimization strategy of main bearing system. (a) Main bearing structure; (b) tube wall structure; (c) limit force state of thin-walled tube; (d) truss cross-sectional configuration; (e) single truss limit force state
    1st order shape of truss
    Fig. 4. 1st order shape of truss
    Stability detection device of CFRP truss structure
    Fig. 5. Stability detection device of CFRP truss structure
    Randomly scan vibration data
    Fig. 6. Randomly scan vibration data
    Satellite remote sensing image
    Fig. 7. Satellite remote sensing image
    Dynamic MTF curves
    Fig. 8. Dynamic MTF curves
    Structure typeMaterialMass /kgBase frequency /HzPower /W
    Cylinder typeTC442885.2
    Cylinder/truss typeTC432541.4
    Table 1. Comparison of performance parameters of secondary mirror support structure
    LoadParameterXYZ
    GravityPosition /μm3.13.95.0
    Title /(″)2.62.90.7
    ThermalPosition /μm0.70.65.8
    Title /(″)0.91.11.2
    Table 2. Central position of subreflector changes in different directions under action of gravity and thermal loads
    Frequency /HzX /μmY /μmR /μm
    1860.050.240.25
    2200.020.100.10
    2870.301.821.84
    4930.010.290.29
    Table 3. Jitter results of visual axis in image plane coordinate system
    StageAngleGravity loadThermal loadBefore vibrationAfter vibration
    InitialPitch angle ψ1 /(°)90.7521590.5384490.7521590.64923
    Orientation O1 /(°)0.000000.000000.000000.00000
    FinalPitch angle ψ2 /(°)90.7522890.5386490.7522890.64938
    Orientation O2 /(°)0.000110.000260.000110.00018
    ψ1-ψ2 /(″)0.4680.7200.4680.540
    O1-O2 /(″)0.3960.9360.3960.648
    Table 4. Stability test results of CFRP truss structure
    Order1st2nd3rd4th
    Test174225293503
    Engineering186220287493
    Table 5. Comparison of characteristic frequencies obtained by process engineering analysis and experimental testing in different ordersunit: Hz
    Kexin Song, Lei Zhang, Xuezhi Jia, Zhiqiang Su. Carbon Fiber Truss Support Technology for JL-1 Light High Resolution Space Camera[J]. Acta Optica Sinica, 2020, 40(21): 2122002
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