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P. 180

Zhang et al. Satell Navig            (2021) 2:11                                         Page 4 of 10





            where                                             Results
                                                              Te present section starts with a description of the
                               ˜
                d r,j (i) = d r,j (1) + d r,j (i)        (9)  experimental data and processing strategies, then pro-
                                                              ceeds with the results and analysis, and ends with some
                 ˜
            with d r,j (i) = d r,j (i) − d r,j (1).           concluding remarks.
                            ˜
              Note that if the d r,j (i) is ignored, the (rank-defcient)
            design matrix of Eq. (8) turns out to be the same as that   Experiment setup
                                    ˜
            of Eq. (2). In the following d r,j (i) is assumed as a time-  Te data for this analysis were collected at four stations
            varying parameter. But  there will be  a rank  defciency   with dual-frequency observations and a 30-s sampling
            between  dt r (i) ,  d r,j (i) and  a  parameters. Te receiver   interval. Te detailed information is given in Table  1.
                                    s
                                    r,j
            code biases at the frst epoch are chosen as datum to   Note that stations ALIC and MTDN have thermometers
                                                       ˜
            eliminate the rank defciency, thus the estimated  d r,j (i)   to gauge the air temperatures, and the receivers at sta-
            are the variations of receiver code bias with respect to   tions  NOT1  and  MEDI  were  both  connected  to  a  high
            the frst epoch, see Eq. (9). As for other parameters, the   performance external frequency standard (H-maser).
            procedures described in the preceding subsection are   Our data processing strategies are as follows. Firstly,
            closely  followed  to  overcome  the  rank  defciency  prob-  the original as well as the modifed PPP were conducted,
            lem, thereby yielding
                                                              solving for  the parameters  by means  of Kalman flter.
                                  ˜
                   s       s               s                  Te estimated parameters included the ZTDs (a random
                                                ˜
                �p (i) = m τ r (i) + dt r (i) + µ j ˜ι (i) + d r,j (i)
                   r,j     r               r                  walk process with a variance rate of 1 ×  10   m /s), the
                                                                                                  −7
                                                                                                      2
                   s       s               s     s      (10)
                                  ˜
                �φ (i) = m τ r (i) + dt r (i) − µ j ˜ι (i) + ˜ a  biased receiver clocks (time-varying), the biased slant
                   r,j     r               r     r,j
                                                              ionosphere delay (time-varying), the biased ambigui-
            with                                              ties (time-constant), and the biased receiver code biases
                                                              (time-varying for the modifed PPP). Te elevation cut-
                 ˜
                dt r (i) = dt r (i) + d r,IF (1)              of angle was set as 10°, and the P1-C1 satellite DCB
                 s
                       s
                ˜ ι (i) = ι (i) + d r,GF (1) − d s
                 r     r              GF                      corrections provided by the IGS were applied to the C1
                             s



                 ˜ a s r,j  = a s r,j  + d IF  − d r,IF (1) − µ j d s GF  − d r,GF (1)   observations. Te IGS fnal orbit and clock products were
                                                        (11)  employed to correct for the satellite orbital and clock
            where a tilde marks the biased, but estimable param-  errors. Te other critical corrections to raw observa-
            eters. Note the diference to the estimable parameters in   tions were also considered, including the solid Earth tide,
            Eqs. (5) and (6).                                 the phase wind-up efects, and the satellite and receiver
              Equation  (10) is a full-rank system, representing the   phase center ofsets and variations.
            full-rank functional model constructed for the modifed   Second, Te variations of the code observations were
                                                       ˜
            PPP. Note that, the estimable receiver code biases d r,j (i)   estimated on each frequency epoch by epoch. Te results
            only appear in the observation equations at the second   would allow us to verify the ability of the modifed PPP to
            epoch and beyond, i.e., i ≥ 2 , for those at the frst epoch   directly measure the temporal variability of the receiver
            get  lumped  with  the parameters  given  in  Eq.  (11).  Te   code biases for each observable type.
            estimability  of  d r,j (i)  implies  that  any  temporal  varia-  Tird, the time-varying receiver code biases are not
                          ˜
            tions in receiver code biases shall fully enter into d r,j (i) ,   considered in Global Ionosphere Maps (GIMs) provided
                                                      ˜
            and thus have no negative impacts on the estimation of   by  the  IGS,  and  the  GF  carrier  phase  observables are
            remaining parameters.                             almost unafected by measurements noise and multipath.
                                                              Te Diference of Slant Total Electron Content (DSTEC)
                                                              obtained from the GF carrier phase observations is thus
                                                              chosen as the reference to evaluate the performance of
            Table 1  The information on the collected GPS data used in this study
            Station    Receiver       Antenna type   Temperature data  Frequency   Period      Latitude, longitude
                                                                    standard
            ALIC       LEICA GR25     LEIAR25.R3     ✓              Internal     DOY 002, 2017  − 23.67°, 133.89°
            MTDN       TRIMBLE NETR9  TRM59800.00    ✓              Internal     DOY 005, 2018  − 22.13°, 131.49°
            NOT1       LEICA GR30     LEIAR20                       H-maser      DOY 001, 2018  36.88°, 14.99°
            MEDI       LEICA GR10     LEIAR20                       H-maser      DOY 009, 2018  44.52°, 11.65°
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