• Acta Optica Sinica
  • Vol. 44, Issue 6, 0606003 (2024)
Chongmiao Jiao1、2、3, Yan He1、*, Shanjiang Hu1, Chunhe Hou1, Yongqiang Chen1、2, and Weibiao Chen1、**
Author Affiliations
  • 1Key Laboratory of Space Laser Communication and Detection Technology, Shanghai Institute of Optics and Fine Mechanics, Chinese Academy of Sciences, Shanghai 201800, China
  • 2Center of Materials Science and Optoelectronics Engineering, University of Chinese Academy of Sciences, Beijing 100049, China
  • 3Hangzhou Institute for Advanced Studies, University of Chinese Academy of Sciences, Hangzhou , 310024, Zhejiang , China
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    DOI: 10.3788/AOS231506 Cite this Article Set citation alerts
    Chongmiao Jiao, Yan He, Shanjiang Hu, Chunhe Hou, Yongqiang Chen, Weibiao Chen. Orbit Forecasting, Tracking, and Pointing System Based on High-Altitude Aircraft Laser Communication[J]. Acta Optica Sinica, 2024, 44(6): 0606003 Copy Citation Text show less
    Optical center to target pointing angle
    Fig. 1. Optical center to target pointing angle
    Structure of laser communication tracking pointing system for underwater platforms
    Fig. 2. Structure of laser communication tracking pointing system for underwater platforms
    Flowchart of laser communication tracking pointing system for underwater platforms
    Fig. 3. Flowchart of laser communication tracking pointing system for underwater platforms
    Time dependence of acceleration and deceleration versus angle
    Fig. 4. Time dependence of acceleration and deceleration versus angle
    Errors of simulated orbit position and actual orbit position. (a) Errors between forecasted value and actual value for X, Y, Z axes; (b) absolute position error
    Fig. 5. Errors of simulated orbit position and actual orbit position. (a) Errors between forecasted value and actual value for X, Y, Z axes; (b) absolute position error
    Errors between actual navigational parameter prediction results and aircraft actual orbit, and pointing errors. (a) Errors between forecasted value and actual value for X, Y, Z axes; (b) absolute position error; (c) pointing vector errors in the local coordinate system; (d) optical pointing angle error
    Fig. 6. Errors between actual navigational parameter prediction results and aircraft actual orbit, and pointing errors. (a) Errors between forecasted value and actual value for X, Y, Z axes; (b) absolute position error; (c) pointing vector errors in the local coordinate system; (d) optical pointing angle error
    Actual pointing errors versus theoretical pointing errors in pitch and roll directions. (a) Actual pointing error in pitch direction; (b) actual pointing error in roll direction
    Fig. 7. Actual pointing errors versus theoretical pointing errors in pitch and roll directions. (a) Actual pointing error in pitch direction; (b) actual pointing error in roll direction
    No. of experimentsNavigating parameters received timeUplink data received timeLink establishment time /s
    101:31:50.40401:31:51.8391.435
    204:51:43.76804:51:45.4451.677
    305:39:29.65605:39:31.1491.493
    Table 1. Uplink establishment time
    Angle /(°)Speed /(r/min)Time /ms
    0.1100/1000/200022.68
    1.0100/1000/200031.02
    3.0100/1000/200037.60
    5.0100/1000/200042.46
    10.0100/1000/200050.40
    Table 2. Actual motor rotation time
    Chongmiao Jiao, Yan He, Shanjiang Hu, Chunhe Hou, Yongqiang Chen, Weibiao Chen. Orbit Forecasting, Tracking, and Pointing System Based on High-Altitude Aircraft Laser Communication[J]. Acta Optica Sinica, 2024, 44(6): 0606003
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