Volume 45 Issue 2
Apr.  2025
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TAN Jiaheng, YONG Qiang, XU Wei. Design and Experiment of Optical Transmission Device for Laser Communication between Rotating Components on Satellite (in Chinese). Chinese Journal of Space Science, 2025, 45(2): 629-640 doi: 10.11728/cjss2025.02.2024-0160
Citation: TAN Jiaheng, YONG Qiang, XU Wei. Design and Experiment of Optical Transmission Device for Laser Communication between Rotating Components on Satellite (in Chinese). Chinese Journal of Space Science, 2025, 45(2): 629-640 doi: 10.11728/cjss2025.02.2024-0160
shu

Design and Experiment of Optical Transmission Device for Laser Communication between Rotating Components on Satellite

doi: 10.11728/cjss2025.02.2024-0160 cstr: 32142.14.cjss.2024-0160
  • 1.

    Changchun Institute of Optics, Fine Mechanics and Physics, Chinese Academy of Sciences, Changchun 130033

  • 2.

    University of Chinese Academy of Sciences, Beijing 100049

  • Received Date: 2024-11-13
  • Rev Recd Date: 2024-12-29
    • Available Online: 2025-02-20
    Abstract
  • Aiming to address the demand for high-capacity and high-reliability data transmission between a rotating imaging ultra-wide-field space camera and the satellite platform, a space optical transmission device based on laser communication was designed, and the high-precision optical testing and alignment scheme was studied. The device’s reliability was enhanced by installing the primary and backup collimators at both the transmitter and the receiver, with mutual backup achieved through the design of multiple optical channels. At the same time, a high-precision alignment scheme to ensure accurate measurement and alignment of the collimator’s optical axis was proposed. Finally, the modal analysis of the space optical transmission device was carried out by using the finite element analysis software MSC.PATRAN and the vibration test of the installed space optical transmission device was completed. The results show that the first-order frequency of the transmitter of the space optical transmission device is 264.25 Hz, and the first-order frequency of the receiver is 434.35 Hz. After the vibration test, the maximum optical power penalty between the transceiver collimator is 1.94 dB, and the spatial angle change of each prism reference surface normal is within 5". It shows that the space optical transmission device can overcome the influence of a complex mechanical environment during the satellite launch, has high alignment precision and reliability, and meets the requirements of laser communication data transmission between satellite-borne rotating components.

     

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