Applications of two-way satellite time and frequency transfer in the BeiDou navigation satellite system<xref rid="fn2" ref-type="Recommend" xml:lang="en"><sup>?</sup></xref>

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SCIENCE CHINA Physics, Mechanics & Astronomy, Volume 59, Issue 10: 109511(2016) https://doi.org/10.1007/s11433-016-0185-6

Applications of two-way satellite time and frequency transfer in the BeiDou navigation satellite system?

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  • ReceivedMay 10, 2016
  • AcceptedJun 15, 2016
  • PublishedAug 22, 2016
PACS numbers

Abstract

A two-way satellite time and frequency transfer (TWSTFT) device equipped in the BeiDou navigation satellite system (BDS) can calculate clock error between satellite and ground master clock. TWSTFT is a real-time method with high accuracy because most system errors such as orbital error, station position error, and tropospheric and ionospheric delay error can be eliminated by calculating the two-way pseudorange difference. Another method, the multi-satellite precision orbit determination (MPOD) method, can be applied to estimate satellite clock errors. By comparison with MPOD clock estimations, this paper discusses the applications of the BDS TWSTFT clock observations in satellite clock measurement, satellite clock prediction, navigation system time monitor, and satellite clock performance assessment in orbit. The results show that with TWSTFT clock observations, the accuracy of satellite clock prediction is higher than MPOD. Five continuous weeks of comparisons with three international GNSS Service (IGS) analysis centers (ACs) show that the reference time difference between BeiDou time (BDT) and golbal positoning system (GPS) time (GPST) realized IGS ACs is in the tens of nanoseconds. Applying the TWSTFT clock error observations may obtain more accurate satellite clock performance evaluation in the 104 s interval because the accuracy of the MPOD clock estimation is not sufficiently high. By comparing the BDS and GPS satellite clock performance, we found that the BDS clock stability at the 103 s interval is approximately 10?12, which is similar to the GPS IIR.


Funded by

The National Natural Sciences Foundation of China(41574029)


Acknowledgment

This work was supported by the National Natural Sciences Foundation of China (Grant No. 41574029) and Youth Innovation Promotion Association CAS (Grant No. 2016242). We would like to thank the Beijing Global Information Application and Development Center for providing the TWSTFT observations of the BDS. We also thank IGS for providing the BDS satellite clock products. The authors gratefully acknowledge the support of all individuals and institutions that have supported this work.


References

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  • Figure 1

    (Color online) Diagram of TWSTFT measure.

  • Figure 2

    (Color online) TWSTFT and MPOD clock comparison time series. (a) Shows the GEO satellite clock comparisons; (b) shows the IGSO; (c) shows MEO. Different colors represent different satellites listed in the right legends.

  • Figure 3

    (Color online) TWSTFT and MPOD clock linear fitting RMS and a1 time series. The left subplots show the TWSTFT residual and the MPOD clock fitting residual in blue and red, respectively. The right subplots show the linear fitting parameter (a1) time series. The blue points represent TWSTFT fitting results, and red points represent MPOD results.

  • Figure 4

    (Color online) Satellite clock prediction error time series for TWSTFT and MPOD. The blue represents TWSTFT clock prediction error, the red MPOD clock predictions error. (a)-(c) Represent C01 (GEO), C08 (IGSO), C11 (MEO) satellite clock prediction error respectively.

  • Figure 5

    (Color online) Comparisons of TWSTFT and three AC MPOD clocks. The three rows represent three ACs, (a) the comparison between TWSTFT and CODE MPOD clock; (b) the comparison between TWSTFT and GFZ; (c) the comparison between TWSTFT and WHU. Different colors represent different satellites listed in the right legends.

  • Figure 6

    (Color online) Satellite performance evaluations in orbit. The blue and red curves represent Allan variances calculated by TWSTFT and by GFZ MPOD clock data, respectively. (a)-(c) Represent C01 (GEO), C08 (IGSO), C11 (MEO).

  • Figure 7

    (Color online) Comparison of GPS and BDS satellite performance evaluations in orbit. The black points represent BDS Allan variance, and the other colors represent GPS. The same color represents the same GPS block type.

  • Table 1   Error sources for TWSTFT and MPOD clock errors

    Error source

    TWSTFT

    MPOD

    System error

    residual ionospheric delay

    device bias

    orbital correlated error

    White noise

    0.707pseudorange noise

    BDS ionospheric free combination

    B1/B2: 2.90phase noise

    B1/B3: 3.53phase noise

    Satellite reference position

    B3 send phase center

    LC combination phase center

    Ground reference time

    BDT: ground atomic time

    the GPST realized at each AC (see ref. [5])

  • Table 2   TWSTFT and MPOD clock comparison: MEAN and STD

    SATID

    Mean (ns)

    STD (ns)

    SATID

    Mean (ns)

    STD (ns)

    01

    13.181

    1.591

    08

    16.585

    0.472

    02

    –13.801

    1.328

    09

    6.220

    0.360

    03

    0.928

    1.252

    10

    –1.083

    0.528

    04

    –0.421

    0.864

    11

    0.441

    0.385

    05

    –9.354

    1.589

    12

    –10.542

    0.270

    06

    17.422

    0.314

    14

    –23.356

    0.360

    07

    17.844

    0.533

  • Table 3   Satellite clock error fitting residual comparison

    SATID

    GFZ (ns)

    TWSTFT (ns)

    SATID

    GFZ (ns)

    TWSTFT (ns)

    C01

    0.108

    0.126

    C08

    0.304

    0.321

    C02

    0.116

    0.128

    C09

    0.079

    0.128

    C03

    0.068

    0.111

    C10

    0.134

    0.176

    C04

    0.176

    0.176

    C11

    0.154

    0.218

    C05

    0.086

    0.138

    C12

    0.075

    0.152

    C06

    0.153

    0.175

    C14

    0.053

    0.156

    C07

    0.093

    0.129

    Mean (all satellites): GFZ: 0.126 TWSTFT: 0.166

  • Table 4   Satellite clock prediction error for TWSTFT and MPOD

    SATID

    TWSTFT (ns)

    MPOD (ns)

    SATID

    TWSTFT (ns)

    MPOD (ns)

    01

    0.556

    1.072

    08

    1.505

    1.636

    02

    0.462

    1.239

    09

    0.435

    0.708

    03

    0.369

    0.764

    10

    0.682

    0.888

    04

    0.726

    1.553

    11

    0.620

    0.816

    05

    0.787

    1.475

    12

    0.450

    0.762

    06

    1.268

    1.280

    14

    0.613

    0.734

    07

    0.582

    0.874

    mean

    0.697

    1.062

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