• Acta Photonica Sinica
  • Vol. 54, Issue 2, 0254108 (2025)
Shihao SU1, Long MA1,*, Xinyi ZHAO1, Yongbin SHAO1..., Xutao YIN1 and Ming XIN2|Show fewer author(s)
Author Affiliations
  • 1Sino-European Institute of Aviation Engineering, Civil Aviation University of China, Tianjin 300300, China
  • 2School of Electrical and Information Engineering, Tianjin University, Tianjin 300072, China
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    DOI: 10.3788/gzxb20255402.0254108 Cite this Article
    Shihao SU, Long MA, Xinyi ZHAO, Yongbin SHAO, Xutao YIN, Ming XIN. Design Method for Satellite-borne Single Arm Locking Controller Based on Bilayer Synchronized Optimization Strategy[J]. Acta Photonica Sinica, 2025, 54(2): 0254108 Copy Citation Text show less
    Schematic diagram of the arm locking structure
    Fig. 1. Schematic diagram of the arm locking structure
    Arm locking circuit structure
    Fig. 2. Arm locking circuit structure
    Step response of the Padé approximation for different orders of the delay segment
    Fig. 3. Step response of the Padé approximation for different orders of the delay segment
    The variation of the arm lengths
    Fig. 4. The variation of the arm lengths
    Schematic of bilayer optimization strategy
    Fig. 5. Schematic of bilayer optimization strategy
    Boxplots of evaluation indicator for different pairs of zero poles
    Fig. 6. Boxplots of evaluation indicator for different pairs of zero poles
    Close-loop transfer function bode plot
    Fig. 7. Close-loop transfer function bode plot
    Structure of single arm locking simulation
    Fig. 8. Structure of single arm locking simulation
    Time domain noise signal
    Fig. 9. Time domain noise signal
    Technical noise amplification in frequency domain
    Fig. 10. Technical noise amplification in frequency domain
    Laser frequency noise suppression in frequency domain
    Fig. 11. Laser frequency noise suppression in frequency domain
    Single arm locking system simulation results
    Fig. 12. Single arm locking system simulation results
    All noise frequency domain analysis
    Fig. 13. All noise frequency domain analysis
    Simulation parametersValueSimulation parametersValue
    One-way delay time τ10 sRamp signal start time20 s
    Gain2/Gain1100Sample interval0.001 s
    Ramp signal slope0.001Simulation time40 000 s
    Table 1. Simulation parameters of the single arm system
    NoiseEquivalent displacement noise
    Laser frequency noise3.19×10-4 m/Hz1/2∙[1+(2.8 mHz/f41/2
    Clock noise1.49/f pm/Hz1/2
    Readout noise3.16×10-4 pm/Hz1/2∙[1+(2.8 mHz/f41/2
    Shot noise7.3 pm/Hz1/2
    Table 2. Noise type and equivalent displacement noise
    Shihao SU, Long MA, Xinyi ZHAO, Yongbin SHAO, Xutao YIN, Ming XIN. Design Method for Satellite-borne Single Arm Locking Controller Based on Bilayer Synchronized Optimization Strategy[J]. Acta Photonica Sinica, 2025, 54(2): 0254108
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