• Acta Optica Sinica
  • Vol. 38, Issue 1, 0128003 (2018)
Shisong Wu1、2, Heyong Zhang1, Tingfeng Wang1、2、*, Jin Guo1、2, Chunhui Yan1、2, and Tao Lü1、2
Author Affiliations
  • 1 State Key Laboratory of Laser Interaction with Mater, Changchun Institute of Optics, Fine Mechanics and Physics, Chinese Academy of Sciences, Changchun, Jilin 130033, China
  • 2 University of Chinese Academy of Sciences, Beijing 100049, China
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    DOI: 10.3788/AOS201838.0128003 Cite this Article Set citation alerts
    Shisong Wu, Heyong Zhang, Tingfeng Wang, Jin Guo, Chunhui Yan, Tao Lü. Study on Matched Filtering Process Based on Long-Range Pulsed Laser Heterodyne Detection[J]. Acta Optica Sinica, 2018, 38(1): 0128003 Copy Citation Text show less
    Schematic of the heterodyne detection system
    Fig. 1. Schematic of the heterodyne detection system
    Schematic of the I&Q detector
    Fig. 2. Schematic of the I&Q detector
    Processing flow chart of the matched filtering algorithm
    Fig. 3. Processing flow chart of the matched filtering algorithm
    Waveform distortion induced by the matched filtering process. (a) Envelope of the OPM signal; (b) envelope of self-convolution of the OPM signal
    Fig. 4. Waveform distortion induced by the matched filtering process. (a) Envelope of the OPM signal; (b) envelope of self-convolution of the OPM signal
    Matched filtering process of medium-range missile. (a) REC signal; (b) power spectrum density of REC signal; (c) OPM signal and REC signal; (d) matched filtered output signal with carrier frequency; (e) envelope of the matched filtered output signal; (f) power spectrum density of the matched filtered output signal
    Fig. 5. Matched filtering process of medium-range missile. (a) REC signal; (b) power spectrum density of REC signal; (c) OPM signal and REC signal; (d) matched filtered output signal with carrier frequency; (e) envelope of the matched filtered output signal; (f) power spectrum density of the matched filtered output signal
    Matched filtering process of ISS. (a) REC signal; (b) power spectrum density of REC signal; (c) OPM signal and REC signal; (d) matched filtered output signal with carrier frequency; (e) envelope of the matched filtered output signal; (f) power spectrum density of the matched filtered output signal
    Fig. 6. Matched filtering process of ISS. (a) REC signal; (b) power spectrum density of REC signal; (c) OPM signal and REC signal; (d) matched filtered output signal with carrier frequency; (e) envelope of the matched filtered output signal; (f) power spectrum density of the matched filtered output signal
    Monte Carlo simulation. (a) Range error of medium-range missile; (b) range rate error of medium-range missile; (c) range error of ISS; (d) range rate error of ISS
    Fig. 7. Monte Carlo simulation. (a) Range error of medium-range missile; (b) range rate error of medium-range missile; (c) range error of ISS; (d) range rate error of ISS
    CNR versus target range
    Fig. 8. CNR versus target range
    CNR versus radar cross section of target
    Fig. 9. CNR versus radar cross section of target
    Power spectral density of echo signal with different sampling rates. (a) 100 MHz; (b) 400 MHz; (c) 700 MHz; (d) 1 GHz; (e) 10 GHz; (f) 20 GHz
    Fig. 10. Power spectral density of echo signal with different sampling rates. (a) 100 MHz; (b) 400 MHz; (c) 700 MHz; (d) 1 GHz; (e) 10 GHz; (f) 20 GHz
    Envelope of the matched-filtered signal with different sampling rates. (a) 100 MHz; (b) 400 MHz; (c) 700 MHz; (d) 1 GHz; (e) 10 GHz; (f) 20 GHz
    Fig. 11. Envelope of the matched-filtered signal with different sampling rates. (a) 100 MHz; (b) 400 MHz; (c) 700 MHz; (d) 1 GHz; (e) 10 GHz; (f) 20 GHz
    ItemParameterValue
    Energy /pulse10 J@10R(18)-13CO2
    Pulse recurrence frequency10 Hz
    Pulse width2.5 μs
    Wavelength λ11.15 μm
    Aperture diameter60 cm
    TransmitterOptical transmission55%
    Heterodyne efficiency60%
    Quantum efficiency35%
    Frequency fidelitySingle transverse and longitudinal mode
    ResonatorUnstable, 4 cm×4 cm, M=1.25, L=2.5 m
    LO power~0.5 mW @shot noise limited operation
    DetectorHgCdTe (77 K)
    ReceiverBandwidth>100 MHz
    Pre-amplifier gain>40 dB
    Table 1. Heterodyne detection system parameters
    ParameterValue
    Energy /pulse Et10 J@10R(20)-13CO2
    Atmosphere transmission T0.8
    Transmission system efficiency Kt0.75
    Receiving system efficiency Kr0.7
    Aperture D0.6 m
    Target reflectivity ρ0.2
    Target Area δ10-100 m2
    Pulse duration Δt2.5 μs
    Target range R10-1000 km
    Divergence angle θt0.1 mrad
    Table 2. Heterodyne detection system parameters
    TargetTarget area δ /m2Target range R /kmVelocity /Ma
    Medium-range missile510-30010
    ISS100380-150022-23
    Table 3. Parameters of two types of target
    Shisong Wu, Heyong Zhang, Tingfeng Wang, Jin Guo, Chunhui Yan, Tao Lü. Study on Matched Filtering Process Based on Long-Range Pulsed Laser Heterodyne Detection[J]. Acta Optica Sinica, 2018, 38(1): 0128003
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