Acta Optica Sinica, Volume. 45, Issue 7, 0706001(2025)

Design and Equivalent Validation of an Omnidirectional Domain Laser Communication Optical Antenna for Low‐Orbit Satellite Networking

Zexiang Li1, Yan An1,2、*, Lichao Hu1, Xiaohua Wang1, Xinhang Li1, Yansong Song1,2, and Keyan Dong1,2
Author Affiliations
  • 1School of Optoelectronic Engineering, Changchun University of Science and Technology, Changchun 130022, Jilin, China
  • 2National and Local Joint Engineering Research Center of Space Optoelectronics Technology, Changchun University of Science and Technology, Changchun 130022, Jilin, China
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    Figures & Tables(26)
    Diagram of relative angles between satellites
    Schematic diagram for two types of panoramic system. (a) Traditional panoramic annular system; (b) proposed two-mirror system
    Schematic diagram of characteristic point acquisition
    Schematic of point-by-point aperture expansion
    Flowchart of feature point calculation
    Freeform surface point cloud diagram. (a) Primary mirror; (b) secondary mirror
    Surface fitting results. (a) Primary mirror; (b) secondary mirror
    Optical design of two panoramic annular systems.
    Optical design of rear mirror assembly
    Complete optical system after stitching. (a) Freeform surface system; (b) aspheric surface system
    MTF comparison. (a) Freeform surface system; (b) aspheric surface system
    Relay system design and spot diagrams. (a) Design result of relay system; (b) spot diagrams
    Collimation-coupling system and wavefront aberration. (a) Collimation-coupling system design result; (b) wavefront aberration
    Overall light path diagram of optical system
    Beam divergence angles of antenna systems with different fields of view. (a) Freeform optical system with 30° field of view; (b) freeform optical system with 70° field of view; (c) aspheric optical system with 30° field of view; (d) aspheric optical system with 70° field of view
    Physical picture of freeform mirror
    Physical setup diagram of experimental equipment
    Communication test layout diagram
    Bit error rate test results. (a) 30° field of view; (b) 70° field of view
    • Table 1. Inter-orbit communication time, angle, and distance

      View table

      Table 1. Inter-orbit communication time, angle, and distance

      TimeRelative angle /(°)Distance /km
      05:330.032664.78
      05:4028.354734.60
      05:5948.399989.70
      06:1232.149808.16
      06:203.616668.52
      06:28-28.918738.18
      06:44-49.985996.80
      07:01-29.697804.00
    • Table 2. Initial XY polynomial coefficients

      View table

      Table 2. Initial XY polynomial coefficients

      CoefficientPrimary mirror valueSecondary mirror value
      x-0.358-0.161
      y-0.609-0.058
      x2-0.127-0.015
      xy-0.0380.015
      y2-0.0990.028
      x30.0830.039
      x2y-0.058-8.293×10-3
      xy22.5×10-34.789×10-3
      y34.699×10-38.715×10-3
      x41.8430.237
      x3y2.234×10-40.011
      x2y2-0.019-9.302×10-3
      xy31.1×10-32.232×10-3
      y4-7.035×10-3-5.711×10-3
    • Table 3. Optical system indicators

      View table

      Table 3. Optical system indicators

      DevicePanoramic antennaRelay systemCollimated coupling system
      Entrance pupil diameter50 mm120 mm120 mm
      F-number/NA1.51.50.14
      Effective focal length75 mm180 mm428.5 mm
      Field of view/object height30°‒70° and -30°‒-70°20°9 μm
      ConfigurationImage space telecentricImage space telecentricCollimated
    • Table 4. Beam divergence angle of different forms of antennas under different fields of view

      View table

      Table 4. Beam divergence angle of different forms of antennas under different fields of view

      FOVBeam divergence angle /μrad
      Freeform surface systemAspheric optical system
      ±30°144326
      ±70°250554
    • Table 5. Telecentric lens indicators

      View table

      Table 5. Telecentric lens indicators

      ParameterValue
      Effective focal length190 mm
      Scanning angle±14°
      Telecentricity<1°
      Transmission>98%
    • Table 6. Scanning system deflection angle and received energy under different fields of view

      View table

      Table 6. Scanning system deflection angle and received energy under different fields of view

      Field of view /(°)3040506070
      Design deflection angle /(°)48.749.850.751.952.5
      Actual deflection angle /(°)48.749.650.551.752.6
      Received energy after introduction of attenuation /dB-13.22-13.81-14.58-15.08-15.48
    • Table 7. Equivalent link calculation results

      View table

      Table 7. Equivalent link calculation results

      Link typeInter-satellite linkIndoor equivalent link
      Laser power37 dBm3 dBm
      Transmission loss-0.96 dB-0.96 dB
      Space loss-73.62 dB@1200 km-1.89 dB@1 m
      Reception loss-0.96 dB-0.96 dB
      Coupling loss-3 dB-3 dB
      Introduction of active losses0 dB-9.73 dB
      Optical power at detector-43.48 dBm-15.48 dBm
      Coding gain3 dB0 dB
      Detection sensitivity-45 dBm@10 Gbit/s 25-20 dBm@10 Gbit/s
      Link margin4.52 dB4.52 dB
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    Zexiang Li, Yan An, Lichao Hu, Xiaohua Wang, Xinhang Li, Yansong Song, Keyan Dong. Design and Equivalent Validation of an Omnidirectional Domain Laser Communication Optical Antenna for Low‐Orbit Satellite Networking[J]. Acta Optica Sinica, 2025, 45(7): 0706001

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    Paper Information

    Category: Fiber Optics and Optical Communications

    Received: Dec. 13, 2024

    Accepted: Dec. 28, 2024

    Published Online: Apr. 22, 2025

    The Author Email: Yan An (anyan_7@126.com)

    DOI:10.3788/AOS241890

    CSTR:32393.14.AOS241890

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