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Liu et al. Satell Navig             (2021) 2:6                                           Page 8 of 17





            Performance assessment of tightly combined        Evaluation statistics
            BDS-2/BDS-3 RTK                                   Te performance of BDS-3/BDS-2 RTK positioning was
            In this part, we carry out performance evaluation of   evaluated by ambiguity resolution success rate, Ambigu-
            single-epoch  short-baseline  RTK  positioning  with  cur-  ity Dilution of Precision (ADOP), together with position-
            rent  BDS-2 and  BDS-3  full  constellations.  Te  tightly   ing accuracy.
            combined BDS-3/BDS-2 solution is then compared with   ADOP is a well-known theoretical fgure of merit for
            BDS-3 only and BDS-2 only solutions with observations   inferring the average precision of estimated ambiguities
            from two common signals (B1I and B3I). For the BDS-3   from foat solution, which is expressed as (Teunissen
            only solutions, we also compared the RTK performance   1997):
            of new B1C/B2a navigation signals with that of the legacy            1
            B1I/B3I signals. Four processing schemes (see Table  5)   ADOP =      n  in cycles         (3)
            were  adopted  for  both  the  single-  and  dual-frequency      Q ˆ aˆ a
            solutions. As mentioned above, BDS-2 and BDS-3 can be
                                                              where  n denotes the number of foat ambiguities;  Q ˆ aˆ a

            regarded as one constellation if B1I/B3I observations are   illustrates the determinant of variance–covariance matrix
            used in precise relative positioning, therefore only one   for the estimated ambiguities from foat solution. Smaller
            single-reference satellite was selected for all BDS-2 and   ADOP value implies higher average precision of the esti-
            BDS-3 satellites in the schemes “BDS-2/BDS-3 B1I” and   mated  foat  ambiguities,  while  an  ADOP  value  smaller
            “BDS-2/BDS-3 B1I/B3I”.                            than  0.12  cycles  indicates  that  the  achievable ambigu-
              All the data were processed epoch-by-epoch using the   ity resolution success rate are theoretically higher than
            double-diferenced model with software KinPOS v3.0,   99.9% (Odijk and Teunissen 2008).
            developed by Wuhan University. Because our study was   In addition to the theoretical analysis of the ADOP, we
            on short baselines, the double-diferenced ionospheric   used the success rate to demonstrate the empirical per-
            and tropospheric delays were negligible. Tus, only the   formance of ambiguity resolution, which is defned as the
            Tree-Dimensional (3D) baseline vector and the double-  number of epochs with ambiguities correctly resolved
            diferenced ambiguities were estimated in each epoch.   divided by the total epoch numbers, thereby refects the
            Te estimated ambiguities from foat solution were then   availability of reliable and accurate RTK positioning. Te
            fxed to integers based on the method of Least-squares   ambiguities are regarded as correctly resolved only if the
            AMBiguity Decorrelation Adjustment (LAMBDA)       test ratio is no less than a specifed threshold (2.0 in this
            (Teunissen  1995), among which the popular ratio test   study). Meanwhile, the positioning errors should be less
            with a threshold of 2.0 was adopted for ambiguity valida-  than 5 cm/5 cm/10 cm in the East (E)/North (N)/Up (U)
            tion. Additionally, diferent elevation cut-of angles (10°,   components compared with “true” baseline vector, which
            15°, 20°, 25°, 30°, 35°, and 40°) were set to simulate difer-  is the post-processed baseline fxed solution with BDS-3/
            ent observational conditions and satellite visibilities.  BDS-2 observations over the entire observation period.
              Meanwhile, the following elevation-dependent weight-  Root-Mean-Square (RMS) of the positioning error series
            ing function (Herring et  al.  2018) was used in the sto-  from those correctly resolved solutions was computed
            chastic model:                                    and compared to evaluate the RTK positioning accuracy
                                                              as well.
                               2
                              b
                  2
                         2
                σ (θ) = a +    2                         (2)
                            sin (θ)
                   2
            where σ (θ) denotes the variance of undiferenced obser-  Experimental results
            vation, θ represents the satellite elevation angle. a and b   In this research, the data for both the static and kinematic
            are model coefcients with specifed empirical values.   modes collected in Wuhan were analyzed. Te static data
            Here, both a and b are set to 0.003 m for phase obser-  were collected in the Wuhan University campus, whereas
            vations of BDS-3 B1I/B1C/B2a/B3I and BDS-2 B1I/B3I,   the kinematic data were collected by a car along Liangzi
            while 0.3 m for code observations.                Lake Avenue.



            Table 5  Processing schemes
            Observations           Scheme 1            Scheme 2            Scheme 3             Scheme 4
            Single-frequency       BDS-2 B1I           BDS-3 B1I           BDS-3 B1C            BDS-2/BDS3 B1I
            Dual-frequency         BDS-2 B1I/B3I       BDS-3 B1I/B3I       BDS-3 B1C/B2a        BDS-2/BDS3 B1I/B3I
   136   137   138   139   140   141   142   143   144   145   146