Acta Optica Sinica, Volume. 39, Issue 10, 1006003(2019)

Visible-Light Communication and Performance Analysis Based on Medium- and Short-Distance Inter-Satellite Links

Quanrun Chen1,2、*, Xiang Yu1, Wennan Cui1, and Tao Zhang1,3、**
Author Affiliations
  • 1Shanghai Institute of Technical Physics, Chinese Academy of Sciences, Shanghai 200083, China
  • 2University of Chinese Academy of Sciences, Beijing 100049, China
  • 3ShanghaiTech University, Shanghai 201210, China
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    Figures & Tables(19)
    Schematic of outdoor VLC system
    Influences of different factors on background light power. (a) Bandwidth of filter; (b) receiving FOV
    Common formation flying types[18]. (a) Trailing; (b) cluster; (c) constellation
    Geometric relationship of formation flying model
    Design flow chart of orbital elements of formation flying satellite
    Two-satellite formation flying model based on STK
    Schematic of inter-satellite VLC link
    Solar angles of formation flying satellites. (a) F-1; (b) F-2
    Variations of solar angles of formation flying satellites within one year. (a) F-1; (b) F-2
    Distributions of background light powers in critical cases. (a) 5.92° solar angle incidence; (b) illuminance distribution of detector
    Background light powers at different solar angles
    BER as a function of SNR under different modulation schemes
    Performance analysis in deep space scenes. (a) Transmitting power as a function of transmission distance under different BERs; (b) BER as a function of transmitting power at different transmitting and receiving angles when transmission distance is 20 km
    Schematic of SIMO-VLC system for inter-satellite link
    BER as a function of transmitting power under different diversity detection schemes
    BER as a function of transmission distance under EGC merging algorithm
    • Table 1. Orbital elements of two-satellite formation flying model

      View table

      Table 1. Orbital elements of two-satellite formation flying model

      Objectα /kme /10-4i /(°)w /(°)Ω /(°)f /(°)
      Leader6978.14097.79240234.0660
      F-16978.147.177697.7924179.9890234.066180.017
      F-26978.147.177697.792459.7659234.066300.169
    • Table 2. Key parameters of inter-satellite link

      View table

      Table 2. Key parameters of inter-satellite link

      ISLDmax/kmDmin/kmDmean/kmθmin/(°)
      Leader to F-110.755.338.505.92
      Leader to F-210.745.338.5351.65
      F-1 to F-217.378.6813.3928.43
    • Table 3. Simulation parameters of inter-satellite VLC link

      View table

      Table 3. Simulation parameters of inter-satellite VLC link

      ParameterValue
      Peak wavelength of LED λ /nm650
      Half power angle of LED /(°)1
      Bandwidth /MHz300
      Modulation scheme8-PPM
      Photodiode responsivity /(A·W-1)0.53
      Field of view at receiver /(°)5
      Refractive index of a lens at a PD1.5
      Gain of an optical filter Ts(ψ) /dB1
      Detector physical area of a PD /(A·m-2)0.62
      Noise equivalent power of receiver /(pW·Hz-1/2)0.02
      Input current noise density Ia /(pA·Hz-1/2)3.7
      Absolute temperature /K298
      Load resistance /kΩ10
      Other propagation losses /dB2
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    Quanrun Chen, Xiang Yu, Wennan Cui, Tao Zhang. Visible-Light Communication and Performance Analysis Based on Medium- and Short-Distance Inter-Satellite Links[J]. Acta Optica Sinica, 2019, 39(10): 1006003

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    Paper Information

    Category: Fiber Optics and Optical Communications

    Received: May. 22, 2019

    Accepted: Jun. 21, 2019

    Published Online: Oct. 9, 2019

    The Author Email: Chen Quanrun (qrchen_work@126.com), Zhang Tao (haozzh@sina.com)

    DOI:10.3788/AOS201939.1006003

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