Acta Optica Sinica, Volume. 39, Issue 6, 0628003(2019)

Jitter Detection of ZY3-02 Satellite Platform Using Phase-Correlation Registration Based on Symmetrical Energy Distribution

Junfeng Xie1,2, Fan Mo1、*, Huai Wang1, Xiang Li1,2, and Hong Zhu1
Author Affiliations
  • 1 Land Satellite Remote Sensing Application Center, Ministry of Natural Resources, Beijing 100048, China
  • 2 School of Surveying and Geographical Science, Liaoning Technical University, Fuxin, Liaoning 123000, China
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    Figures & Tables(12)
    Schematic of multi-spectral camera imaging on ZY3-02 satellite
    Installation relation among CCDs at different spectral bands in multi-spectral camera
    Schematic of energy peak calculation
    Schematic of jitter detection of satellite platform. (a) b-band camera scanned ground point O at moment t1; (b) a-band camera scanned ground point O at moment t2
    Images of registration error acquired form simulation data. (a) PC; (b) PF; (c) SC; (d) SF; (e) SVD; (f) UP
    Jitter curves detected from on-orbit data using different algorithms
    Experimental scheme
    Parallax images between blue and green spectra. (a) Track 718; (b) track 1379; (c) track 11229; (d) track 11365
    Satellite attitude data verify platform jitter. (a) Track 718; (b) track 1379; (c) track 11229; (d) track 11365
    • Table 1. Jitter frequency and amplitude of different satellite platforms

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      Table 1. Jitter frequency and amplitude of different satellite platforms

      Satellite or sensorLaunch yearFrequencya /HzAmplitudeb /m
      ISS[22-23]19930.01-300.00-
      ETS-VI[13]19940.39-250.00-
      MOC-NA[3]19961-4≈15
      ASTER[4,24-25]19991.5-1.66-7
      QuickBird [4]20011.0, 4.32.5, 0.1
      SPOT 5[4]2002≈0.003≈20
      ALSat-1[26]20020.5-
      Nigeria Sat[26]20030.5-
      UK-DMC[26]20030.6-
      MEX-HRSC[27-28]20030.1-0.2, 1.78
      HiRISE[4,29]2005≈1.6≈1
      Beijing-1[30]20052003
      ALOS[31-32]20066-7, 60-701000, 100
      Kompsat-2[33]20062100.14
      LROC[29,34]200960.1-1.0
      Mapping Satellite-1[35]20100.105, 0.635, 4.0000.2, 0.1, 0.1
      Pleiades-HR[22]201170.9-78.40.14
      ZY3-01[5,10,12,36-37]20120.6-0.72.5-7.5
      Yaogan-26[6]2014100, 200, 3000.1, 0.1, 0.1
      aSatellite attitude jitter frequency may be detected in roll, pitch, or both; the information listed here are from either or both. bThe amplitude has been transformed from on-orbit arcsec or pixel to ground meter (from satellite to ground), which can show the influence of jitter intuitively. Amplitudes not listed in existing records and research are indicated by “-”.
    • Table 2. Statistics of registration error acquired form simulation data

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      Table 2. Statistics of registration error acquired form simulation data

      AlgorithmError /pixel
      MeanRMSE
      PC-0.0070.046
      PF0.0680.088
      SC0.0320.060
      SF0.0690.089
      SVD0.1430.156
      UP-0.0780.085
    • Table 3. Jitter information for experimental data

      View table

      Table 3. Jitter information for experimental data

      Track IDFrequency /HzAmplitude /s
      7180.630.99
      13790.631.12
      112290.650.41
      113650.650.97
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    Junfeng Xie, Fan Mo, Huai Wang, Xiang Li, Hong Zhu. Jitter Detection of ZY3-02 Satellite Platform Using Phase-Correlation Registration Based on Symmetrical Energy Distribution[J]. Acta Optica Sinica, 2019, 39(6): 0628003

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    Paper Information

    Category: Remote Sensing and Sensors

    Received: Nov. 22, 2018

    Accepted: Feb. 26, 2019

    Published Online: Jun. 17, 2019

    The Author Email: Mo Fan (surveymofan@163.com)

    DOI:10.3788/AOS201939.0628003

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