Publications related to the GRACE Missions (no abstracts)

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Comparisons of Differential Code Bias (DCB) Estimates and Low-Earth-Orbit (LEO)-Topside Ionosphere Extraction Based on Two Different Topside Ionosphere Processing Methods

Liu, Mingming, Yuan, Yunbin, Ou, Jikun, and Tan, Bingfeng, 2025. Comparisons of Differential Code Bias (DCB) Estimates and Low-Earth-Orbit (LEO)-Topside Ionosphere Extraction Based on Two Different Topside Ionosphere Processing Methods. Remote Sensing, 17(21):3550, doi:10.3390/rs17213550.

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@ARTICLE{2025RemS...17.3550L,
       author = {{Liu}, Mingming and {Yuan}, Yunbin and {Ou}, Jikun and {Tan}, Bingfeng},
        title = "{Comparisons of Differential Code Bias (DCB) Estimates and Low-Earth-Orbit (LEO)-Topside Ionosphere Extraction Based on Two Different Topside Ionosphere Processing Methods}",
      journal = {Remote Sensing},
     keywords = {GPS satellite differential code bias (DCB), LEO receiver DCB, LEO-based topside ionosphere vertical electron content (VEC), SH-topside VEC method, EP-topside VEC method, accuracy},
         year = 2025,
        month = oct,
       volume = {17},
       number = {21},
          eid = {3550},
        pages = {3550},
     abstract = "{What are the main findings? Using GRACE-A data (400 km in 2016), the
        monthly stabilities (STDs) of GPS satellite differential code
        biases (DCBs) and low-earth-orbit (LEO) satellites receiver DCBs
        using the EP (epoch parameter)-topside vertical electron content
        (VEC) method are better than those using the SH (spherical
        harmonic)-topside VEC method. For JASON-2 data (1350 km), the
        STDs of GPS DCBs using the SH-topside VEC method are slightly
        superior to those using the EP-topside VEC method, and LEO DCBs
        using the two methods have similar STD results. However, the
        root mean square (RMS) results for GPS DCBs using the SH-topside
        VEC model relative to the Center for Orbit Determination in
        Europe (CODE) products are slightly superior to those using the
        EP-topside VEC method. Due to the difference in orbital
        altitude, the results and distributions of the GRACE-topside
        VECs differ from those of the JASON-topside VECs, with the
        former being more consistent with the ground-based results,
        indicating that there may be different height structures in the
        LEO-topside VECs. Meanwhile, we applied the IRI-GIM
        (International Reference Ionosphere model─Global Ionosphere Map)
        method to compare the LEO-topside VEC results. The results
        indicate that the accuracy of GRACE-A-topside VECs using the EP-
        topside VEC method is better than that using the SH-topside VEC
        method, whereas for JASON-2, the two methods have similar
        accuracy. The temporal and spatial resolutions of the SH-topside
        VEC model are higher than those of the EP-topside VEC method,
        and the former has a wide range of usability and predictive
        characteristics. Using GRACE-A data (400 km in 2016), the
        monthly stabilities (STDs) of GPS satellite differential code
        biases (DCBs) and low-earth-orbit (LEO) satellites receiver DCBs
        using the EP (epoch parameter)-topside vertical electron content
        (VEC) method are better than those using the SH (spherical
        harmonic)-topside VEC method. For JASON-2 data (1350 km), the
        STDs of GPS DCBs using the SH-topside VEC method are slightly
        superior to those using the EP-topside VEC method, and LEO DCBs
        using the two methods have similar STD results. However, the
        root mean square (RMS) results for GPS DCBs using the SH-topside
        VEC model relative to the Center for Orbit Determination in
        Europe (CODE) products are slightly superior to those using the
        EP-topside VEC method. Due to the difference in orbital
        altitude, the results and distributions of the GRACE-topside
        VECs differ from those of the JASON-topside VECs, with the
        former being more consistent with the ground-based results,
        indicating that there may be different height structures in the
        LEO-topside VECs. Meanwhile, we applied the IRI-GIM
        (International Reference Ionosphere model─Global Ionosphere Map)
        method to compare the LEO-topside VEC results. The results
        indicate that the accuracy of GRACE-A-topside VECs using the EP-
        topside VEC method is better than that using the SH-topside VEC
        method, whereas for JASON-2, the two methods have similar
        accuracy. The temporal and spatial resolutions of the SH-topside
        VEC model are higher than those of the EP-topside VEC method,
        and the former has a wide range of usability and predictive
        characteristics. What is the implication of the main finding? At
        present, there is no research to analyze and compare the effects
        of the two topside VEC processing methods on DCB estimates and
        LEO-topside VEC extraction. It is essential to obtain more
        accurate global navigation satellite system (GNSS)/LEO DCBs and
        LEO-topside VEC parameters, particularly in future scenarios
        with an increase in LEO satellites, which can serve next-
        generation GNSS and LEO positioning. For GNSS/LEO DCB estimates,
        different evaluation criteria yield different results. The STD
        results are related to the heights of LEO receivers, whereas the
        RMS results are not. The accuracies of the LEO-topside VEC
        results are related to the heights of LEO orbits. Meanwhile, the
        temporal and spatial resolutions of the SH-topside VEC model are
        higher than those of the EP-topside VECs, and the former have a
        wide range of usability and predictive characteristics. At
        present, there is no research to analyze and compare the effects
        of the two topside VEC processing methods on DCB estimates and
        LEO-topside VEC extraction. It is essential to obtain more
        accurate global navigation satellite system (GNSS)/LEO DCBs and
        LEO-topside VEC parameters, particularly in future scenarios
        with an increase in LEO satellites, which can serve next-
        generation GNSS and LEO positioning. For GNSS/LEO DCB estimates,
        different evaluation criteria yield different results. The STD
        results are related to the heights of LEO receivers, whereas the
        RMS results are not. The accuracies of the LEO-topside VEC
        results are related to the heights of LEO orbits. Meanwhile, the
        temporal and spatial resolutions of the SH-topside VEC model are
        higher than those of the EP-topside VECs, and the former have a
        wide range of usability and predictive characteristics. Global
        navigation satellite system (GNSS) differential code bias (DCB)
        and topside ionosphere vertical electron content (VEC) can be
        estimated using onboard data from low-earth-orbit (LEO)
        satellites. These satellites provide the potential to make up
        for the lack of ground-based stations in the oceanic and polar
        regions and establish a high-precision global ionosphere model.
        In order to study the influences of different LEO-topside VEC
        processing methods on estimates, we creatively analyzed and
        compared the results and accuracy of the DCBs and LEO-topside
        VEC estimates using two topside VEC solutions{\textemdash}the
        SH-topside VEC (spherical harmonic-topside vertical electron
        content) and EP-topside VEC (epoch parameter-topside vertical
        electron content) methods. Some conclusions are drawn as
        follows. (1) Using GRACE-A data (400 km in 2016), the monthly
        stabilities (STDs) of GPS satellite DCBs and LEO receiver DCBs
        using the EP-topside VEC method are better than those using the
        SH-topside VEC method. For JASON-2 data (1350 km), the STD
        results of GPS DCBs using the SH-topside VEC method are slightly
        superior to those using the EP-topside VEC method, and LEO DCBs
        using the two methods have similar STD results. However, the
        root mean square (RMS) results for GPS DCBs using the SH-topside
        VEC model relative to the Center for Orbit Determination in
        Europe (CODE) products are slightly superior to those using the
        EP-topside VEC method. (2) The peak ranges of the actual GRACE-
        A-topside VEC results using the SH-topside VEC and EP-topside
        VEC methods are within 42 and 35 TECU, respectively, while the
        peak ranges of the JASON-2-topside VEC results are both within 6
        TECU. Additionally, only the SH-topside VEC model results are
        displayed due to the EP-topside VEC method not modeling VEC. Due
        to the difference in orbital altitude, the results and
        distributions of the GRACE-topside VECs differ from those of the
        JASON-topside VECs, with the former being more consistent with
        the ground-based results, indicating that there may be different
        height structures in the LEO-topside VECs. In addition, we
        applied the IRI-GIM (International Reference Ionosphere
        model─Global Ionosphere Map) method to compare the LEO-based
        topside VEC results, which indicate that the accuracy of GRACE-
        A-topside VEC using the EP-topside VEC method is better than
        that using the SH-topside VEC method, whereas for JASON-2, the
        two methods have similar accuracy. Meanwhile, we note that the
        temporal and spatial resolutions of the SH-topside VEC method
        are higher than those of the EP-topside VEC method, and the
        former has a wide range of usability and predictive
        characteristics. The latter seems to correspond to the single-
        epoch VEC mean of the former to some extent.}",
          doi = {10.3390/rs17213550},
       adsurl = {https://ui.adsabs.harvard.edu/abs/2025RemS...17.3550L},
      adsnote = {Provided by the SAO/NASA Astrophysics Data System}
}

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