Infrared and Laser Engineering, Volume. 52, Issue 12, 20230336(2023)

Laser communication flat back servo pendulum mirror support structure optimization design

Xiaoming Li1,2, Minghang Guo1,2, Yingze Liu1,2, Jialong Yao2, Libiao Wang2, Yunchong Dong1,2, and Xilai Chen1,2
Author Affiliations
  • 1College of mechanical and Electronic Engineering, Changchun University of Science and Technology, Changchun 130022, China
  • 2National and Local Joint Engineering Research Center of Space and Optoelectronics Technology, Changchun University of Science and Technology, Changchun 130022, China
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    Figures & Tables(21)
    General layout of single pendulum mirror servo turntable
    Plane shape of pendulum mirror
    Pendulum mirror-shaped cloud map of standard Earth gravity
    Schematic diagram of flexible hinge structure. (a) Schematic diagram of hinge 1; (b) Schematic diagram of hinge 2
    Schematic diagram of the main parameters of the flexible hinge structure
    First-order modal cloud of the pendulum mirror assembly
    Pendulum mirror 5 ℃ temperature rise (fall) and standard earth gravity effect of the mirror surface surface shape cloud map
    Physical drawing of the pendulum mirror assembly and the whole machine assembly diagram
    System for pendulum mirror assembly inspection
    Results of pendulum mirror assembly surface shape testing at different temperatures
    Sweep sine response curve under Z vibration
    • Table 1. Material properties of reflector components

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      Table 1. Material properties of reflector components

      PartMaterialE/GPa ρ/g·cm−3α/℃ k/W∙(M∙K)−3ν
      MirrorZerodur912.530.051.640.24
      SupportTC41094.448.97.80.31
    • Table 2. Parameter level table of the position of the bonding point of the pendulum mirror

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      Table 2. Parameter level table of the position of the bonding point of the pendulum mirror

      LevelFactors
      α/(°) L1/mm L2/mm
      11062014
      21072115
      31082216
      41092317
    • Table 3. Orthogonal test scheme of the position of the bonding point of the pendulum mirror

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      Table 3. Orthogonal test scheme of the position of the bonding point of the pendulum mirror

      No.α/(°) L1/mm L2/mm V/nm
      110620140.861
      210621150.804
      310622160.877
      410623171.067
      510720150.851
      610721140.660
      710722171.070
      810723160.863
      910820160.895
      1010821170.905
      1110822141.059
      1210823151.053
      1310920171.117
      1410921161.033
      1510922141.198
      1610923151.289
    • Table 4. Range analysis of factors of the position of the bonding point of the pendulum mirror

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      Table 4. Range analysis of factors of the position of the bonding point of the pendulum mirror

      FactorsABC
      α/(°) L1/mm L2/mm
      N1 0.9020.9310.945
      N2 0.8610.8510.999
      N3 0.9781.0510.917
      N4 1.1591.0681.039
      R0.2980.2170.122
    • Table 5. Parameter level of flexible support structure

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      Table 5. Parameter level of flexible support structure

      LevelFactors
      a/mm h/mm b/mm r/mm s/mm t/mm
      1122.416.522.48
      2132.8172.52.89
      3143.217.533.210
      4153.6183.53.611
      516418.54412
    • Table 6. Orthogonal test scheme of flexible support structure

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      Table 6. Orthogonal test scheme of flexible support structure

      No.a/mm h/mm b/mm r/mm s/mm t/mm P/nm
      1122.416.522.4824.03
      2122.8172.52.8933.04
      3123.217.533.21044.58
      4123.6183.53.61159.03
      512418.5441270.99
      6132.41733.61241.27
      7132.817.53.54838.35
      8133.21842.4922.70
      9133.618.522.81033.63
      1013416.52.53.21147.07
      11142.417.542.81120.58
      12142.81823.21230.08
      13143.218.52.53.6825.17
      14143.616.534944.48
      15144173.52.41024.02
      16152.4182.541029.49
      17152.818.532.41116.25
      18153.216.53.52.81222.05
      19153.61743.2816.60
      2015417.523.6930.25
      21162.418.543.2912.01
      22162.816.523.61020.19
      23163.2172.541132.46
      24163.617.532.41214.84
      25164183.52.8810.09
    • Table 7. Range analysis of factors of flexible support structure

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      Table 7. Range analysis of factors of flexible support structure

      FactorsABCDEF
      a/mm h/mm b/mm r/mm s/mm t/mm
      N1 46.3325.4831.6427.7020.3722.85
      N2 36.6027.5829.4833.4523.8828.57
      N3 28.8729.2729.7232.2830.0730.38
      N4 22.9333.7230.2830.7135.1835.08
      N5 17.9236.4831.6128.5843.1535.85
      R28.41112.165.7522.7813
    • Table 8. Results of modal analysis of pendulum mirror assembly

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      Table 8. Results of modal analysis of pendulum mirror assembly

      OrderFz/Hz Mode of vibration
      1446.66Pendulum mirror translates along the x-axis
      21137.7Pendulum mirror translates along the y-axis
      31248.2Pendulum mirror translates along the z-axis
      41282.7Pendulum mirror rotates around x-axis
      51361.1Pendulum mirror rotates around z-axis
      62134.1Pendulum mirror rotates around y-axis
    • Table 9. Analysis results of 5 ℃ temperature rise (fall) and standard earth gravity under the pendulum mirror surface shape accuracy (Unit: nm)

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      Table 9. Analysis results of 5 ℃ temperature rise (fall) and standard earth gravity under the pendulum mirror surface shape accuracy (Unit: nm)

      Load case directionTemperature riseTemperature reduction
      PVRMSPVRMS
      Xλ/16.34 λ/92.13 λ/16.75 λ/95.13
      Yλ/17.23 λ/94.97 λ/17.47 λ/95.43
      Zλ/16.55 λ/83.28 λ/19.88 λ/101
    • Table 10. Results of pendulum mirror assembly face shape test (Unit: nm)

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      Table 10. Results of pendulum mirror assembly face shape test (Unit: nm)

      Temperature/°CPVRMS
      15λ/5.41 λ/45.34
      20λ/5.49 λ/45.71
      25λ/5.10 λ/43.28
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    Xiaoming Li, Minghang Guo, Yingze Liu, Jialong Yao, Libiao Wang, Yunchong Dong, Xilai Chen. Laser communication flat back servo pendulum mirror support structure optimization design[J]. Infrared and Laser Engineering, 2023, 52(12): 20230336

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    Paper Information

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    Received: Jun. 7, 2023

    Accepted: --

    Published Online: Feb. 23, 2024

    The Author Email:

    DOI:10.3788/IRLA20230336

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