 Original Article
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Multiconstellation GNSS precise point positioning with multifrequency raw observations and dualfrequency observations of ionosphericfree linear combination
Satellite Navigation volume 1, Article number: 7 (2020)
Abstract
Precise point positioning (PPP) is famous for its capability of highprecision positioning with just one station as long as the receiver can receive global navigation satellite system (GNSS) signals. With the rapid development of BDS and Galileo, the number of available satellites for positioning has increased significantly. In addition, GPS III, GLONASSK, BDS, and Galileo satellites can transmit triplefrequency signals. The potentials of multiconstellation GNSS PPP requires further analysis on a global scale. Therefore, we selected 96 multiGNSS experiment (MGEX) stations with a global distribution and used 1 week’s data to assess the PPP performance. The results show that the PPP based on multifrequency raw observations with spatial and temporal constraints has better performance than PPP using dualfrequency ionosphericfree observations. The main contribution of multiconstellation GNSS PPP is to shorten the convergence time. The convergence time for GPS PPP is approximately 40 min, which can be shortened to less than 20 min in multiGNSS PPP. After convergence, the positioning accuracy of multiGNSS PPP is improved by 0.5 to 1.0 cm compared with GPS or GLONASS PPP. The positioning accuracy of multiGNSS could be further improved in the future with the BDS and Galileo precise products of orbits, clock and phase center offset/variation.
Introduction
Global navigation satellite system (GNSS) users mainly depended on American GPS or Russian GLONASS in the past. However, this has gradually changed with the emergence of Chinese BeiDou navigation satellite system (BDS) and European Galileo system. BDS3 primary system was announced to provide global services on December 27, 2018 (http://en.beidou.gov.cn/). The constellation of BDS includes geostationary earth orbit (GEO) satellites, inclined geosynchronous orbit (IGSO) satellites, and medium earth orbit (MEO) satellites. By November, 2019, it had 5 BDS2 GEO satellites, 7 BDS2 IGSO satellites, 3 BDS2 MEO satellites, and 19 BDS3 satellites in normal operation (https://www.glonassiac.ru/en/BEIDOU/). The European Galileo system is also planned to achieve its full capability around 2020, and it currently has 21 usable MEO satellites (https://www.gsceuropa.eu/systemstatus/ConstellationInformation). As a result, the number of GNSS satellites used for positioning is approaching and will exceed 100, which brings both opportunities and challenges to Precise Point Positioning (PPP).
PPP is most characterized by its high efficiency in GNSS data processing and avoidance of nearby reference stations [1]. As an essential positioning technology, it could be widely used in various areas that require precise position information from GNSS, such as crustal deformation monitoring, intelligent transport, environmental monitoring, and precise agriculture [2,3,4,5]. PPP typically uses dualfrequency observations of the ionosphericfree (IF) linear combination from a GPSonly system [2, 6]. By combining GPS and GLONASS observations, the convergence time of PPP can be significantly shortened [7,8,9]. To further reduce initialization time and improve reliability, quadconstellation PPP based on the IF combination has also been studied with BDS2 and few Galileo satellites [10, 11]. With the significant increase in Galileo satellites, the performance of multiGNSS PPP with the current constellation requires further analysis.
Rather than using observations of the IF combination, PPP based on raw observations is more convenient for multifrequency GNSS data processing. GPS and GLONASS satellites have the capability of transmitting dualfrequency signals, while with their modernization, 13 GPS satellites and 2 GLONASS satellites can currently transmit triplefrequency signals. Different from GPS and GLONASS, all BDS and Galileo satellites can transmit multifrequency signals, e.g. BDS2 B1, B2, B3 and Galileo E1, E5a, E5b, E5, E6. The linear combinations of triplefrequency or multifrequency measurements have more advantages on integer ambiguity resolution and highorder ionosphere delay elimination for GNSS PPP, which have been studied in depth [12,13,14]. It has been proven that using raw observations is more adaptable for multifrequency PPP [15]. The observations at each frequency are assumed to be independent, thus avoiding noise amplification in the linear combinations [16]. However, the combined quadconstellation PPP using raw observations of all available frequencies has not been studied. Therefore, to make best use of multifrequency GNSS measurements, the potentials of multifrequency and multiconstellation GNSS data processing must be fully explored.
To track, collate, and analyze all available GNSS signals, the International GNSS Service (IGS) [17] set up the multiGNSS experiment (MGEX) [18]. IGS analysis centers (ACs) have gradually started to provide MultiGNSS precise orbits and clock and multifrequency differential code bias (DCB) products. These products guarantee highprecision PPP performance. We selected 96 MGEX stations with a global distribution to analyze PPP performance based on multifrequency raw measurements and dualfrequency measurements of the IF combination. The PPP performance with current GNSS constellations was assessed. Considering the large orbit error of BDS GEO satellites, the 5 BDS2 GEO satellites were excluded. Also, because most of the MGEX stations cannot completely track triplefrequency signals of BDS3 satellites, only BDS2 MEO and IGSO satellites are included in the following PPP data processing. The corresponding mathematical model is described in “Mathematical model” section. The experiment network and processing strategies follow in “Experimental network and processing strategy” section. “Results and discussions” section presents the results and comparison analysis, and conclusions are given in “Conclusions” section.
Mathematical model
PPP with multifrequency raw observations
The observation equations for PPP based on raw multifrequency measurements are formulated as follows:
where P and L denote code and carrierphase measurements, respectively, the superscript sys indicates the GPS (G), GLONASS (R), BDS (C), or Galileo (E) system, and i is an index for the satellites belonging to the corresponding system; the subscript 1 is the reference frequency index for each system, e.g., L1 for GPS. k is the frequency index except for the reference frequency, such as L2, L5 for GPS; f_{1} and f_{k} are the frequencies. \(\rho^{i}\) is the nondispersive distance that includes the geometric distance, the satellite and receiver clock corrections, and the tropospheric delays; antenna phase center corrections have been applied to all code and carrier phase measurements to make \(\rho^{i}\) independent of frequency. \(\delta s\) represents the intersystem bias for GLONASS, BDS, and Galileo with respect to GPS, which is zero for GPS observation equations. \(I_{1}^{i}\) is the ionospheric delay on the reference frequency, and N represents the ambiguity parameter. In addition, \(b_{1}^{sys}\), \(b_{k}^{sys}\) and \(b_{1}^{i}\), \(b_{k}^{i}\) are the respective receiver and satellite code hardware delays on frequency 1 and k, and the corresponding phase hardware delays for the receiver and satellite are \(h_{1}^{sys}\), \(h_{k}^{sys}\) and \(h_{1}^{i}\), \(h_{k}^{i}\). \(\varepsilon\) denotes the observation noise.
In general, the precise satellite orbit, clock, and DCB products issued by IGS ACs are applied in PPP. Therefore, the satellite code hardware delay parameters are eliminated in Eq. (1). Considering the singularity between the phase hardware delays and ambiguity parameters, we merge them together. After linearization, the observation equations can be rewritten as
with
where A^{i} represents the coefficient matrix of the vector X, which includes the station coordinate parameters, W is the weighting matrix for the observations, dt is the receiver clock correction, and B^{i} is the coefficient for tropospheric zenith delay parameter T. To remove the singularity between the receiver clock and code hardware delay parameters, we employ the following constraints on Eq. (2):
where the subscript numbers are the frequency indexes for each system. Equation (2) is the basic observation equation for multiconstellation GNSS PPP with multifrequency raw measurements.
To efficiently reduce the convergence time of PPP, we introduce initial ionospheric delay and employ temporal ionospheric constraints. A priori knowledge on ionospheric delay plays an important role in reducing the convergence time of PPP solutions. As an empirical standard model of the ionosphere, the International Reference Ionosphere (IRI)2016 model can provide the vertical total electron content (VTEC) from the ground to a certain altitude for a given location and time [19]. The model is based on experimental evidence using all available ground and space data sources. The precision of VTEC derived from the IRI model is approximately 2 to 10 TEC Units (TECU), which has been deeply analyzed and well validated by various authors [20,21,22]. The initial ionospheric delay derived by IRI2016 is
where z is the zenith distance of the satellite at the receiver, F is the mapping function (as given in http://aiuws.unibe.ch/ionosphere/mslm.pdf) to convert \(VTEC_{IRI}\) derived from IRI to slant TEC (STEC), w is the weight, and \(\sigma_{I}\) denotes the a priori noise of the initial ionospheric delay, which is set as 1.28 m (approximately 8 TECU).
The temporal variation of ionospheric delay for a satellite–station pair can be modelled by a random walk process. Considering their temporal correlation, the lineofsight ionospheric delays are imposed as the temporal constraint:
where t and t − 1 represent the current and previous epochs, respectively, and \(\varepsilon_{t}\) is the assumed variation of ionospheric delay from t − 1 to t, which is set to 0.25 TECU with a 30 s sampling interval.
The ionosphere is modulated by the solar and magnetic activity, which shows significant gradients in the North to South and West to East directions. Therefore, ionosphere spatial constraints can help to further reduce the convergence time. The ionospheric gradient parameters for a satellite are expressed as
where \(I_{1}^{i}\) is the slant ionospheric delay, dL and dB respectively represent the longitude and latitude difference between the ionospheric pierce point and station location; a_{0}, a_{1}, a_{2}, a_{3}, and a_{4} are the coefficients of the two secondorder polynomials, which fit the horizontal gradients of east–westward and south–northward, respectively. The coefficients are simultaneously estimated with the slant ionospheric parameters. \(\sigma_{spatial}^{2}\) is the a priori noise of the ionospheric spatial constraints. The TEC gradients are correlated with the ionospheric activity; a high gradient value of up to 10 TECU/deg was found in the postnoon ionosphere [23], while a 2 TECU/deg gradient was suggested by HernándezPajares [24] under low solar activity.
The a priori ionospheric information and temporal and spatial constraints are seen as pseudo observations. These pseudo observations together with the basic observation of Eq. (2) are lumped into the normal equation and compose the complete mathematical model for multiconstellation GNSS PPP with multifrequency raw measurements. The frequencies used by the raw observations are L1/L2/L5 for GPS, G1/G2 for GLONASS, B1/B2/B3 for BDS2, and E1/E5a/E5b/E5/E6 for Galileo.
PPP with dualfrequency observations of the IF combination
The observation of dualfrequency IF linear combination can efficiently mitigate the firstorder ionospheric delay. The observation equation is written as
where the subscript if denotes the IF combination. Compared with the raw observation model, the observation equation based on IF linear combination is more simplified because it does not require the receiver DCB and ionospheric delay parameters. The two frequencies selected to form the IF combination are L1/L2 for GPS, G1/G2 for GLONASS, B1/B2 for BDS2, and E1/E5a for Galileo.
Experimental network and processing strategy
The globally distributed stations of the MGEX provide offline and realtime data of global and regional navigation satellite systems as well as various satellitebased augmentation systems. Therefore, MGEX is an ideal data source for multiGNSS PPP. Data from 96 MGEX stations with a global distribution were collected, as shown in Fig. 1. All stations can track GPS, GLONASS, BDS2, and Galileo signals. The observation period is GPS week 2057, which is from day of year (DOY) 160 to DOY 166 in 2019. The average number of visible satellites at an epoch varies from 19 to 37 in DOY 160, and 60% of the stations can track more than 30 GNSS satellites on average at an epoch. Because the current constellations of BDS and Galileo have more visible satellites in the Asia–Pacific and Europe regions, there are more observed satellites in the Eastern Hemisphere than in the Western Hemisphere.
Data processing of the experimental network is based on the Positioning And Navigation Data Analysis (PANDA) platform. PANDA is widely used by Wuhan University in China, which is one of the IGS ACs, to generate precise multiGNSS orbit and clock products. The observation time for each station is longer than 18 h. The detailed processing strategies are listed in Table 1. The reference coordinates of the stations are collected from the IGS weekly solution. The positioning errors are the differences between the estimated coordinates and reference coordinates. The convergence refers to the positioning errors reaching a certain level, which is usually defined as 0.1 m for the East (E), North (N), and Up (U) components. We also check the positioning errors of 20 sequential epochs. If the errors of all 20 epochs are within the limit, we consider that the position has converged in this epoch. To analyze the performance of PPP convergence, the daily data are divided into 12 twohour sessions. Seven days’ data at 95 IGS stations are processed in twohour sessions, totalling 7980 reconvergence sessions.
Results and discussions
Carrierphase and code residuals
The postfit code and carrierphase residuals can help us to detect whether the PPP model has other unmodeled errors. Normally, the residuals are elevationdependent with a normal distribution. Figure 2 shows a scatter plot of the code residuals for GPS, GLONASS, BDS, and Galileo. The residuals are based on all observations of the 96 stations during the observation period. The residuals are illustrated with the elevation of the satellites above the local horizon for the stations. In this figure, one can clearly see the increase in observation noise at low elevations, which is a wellknown phenomenon mainly caused by multipath effects and residual atmospheric delay. The noise amplifications of IF combination for GPS L1/L2, GLONASS G1/G2, BDS2 B1/B2, and Galileo E1/E5a are 2.978, 2.958, 2.898, and 2.588, respectively. Thus, the IF observations show larger residuals compared with the raw observations. Code measurements of Galileo have the minimum noise, where the corresponding root mean squares (RMS) are 7.41 dm and 3.60 dm for the IF and raw observations, respectively. Although the satelliteinduced code biases of the BDS2 MEO and IGSO satellites have been calibrated, the residual BDS2 code bias still contaminates the code measurements; it makes the RMS of BDS2 raw/IF code residuals the largest among the four systems with corresponding RMS values of 16.45 dm and 8.26 dm for IF and raw code measurements, respectively. In addition, due to the influence of GLONASS interfrequency code bias, the residuals of GLONASS are larger than those of GPS and Galileo.
The postfit carrierphase residuals are shown in Fig. 3. Compared with the code residuals, the residuals of carrierphase observations are significantly lower. The carrierphase residuals are obviously decreased with an increase in satellite elevation, and the residuals of IF observations are approximately 2 to 4 times those of the raw observations. The number of BDS2 MEO and IGSO satellites is significantly lower than in other systems; therefore. the samples of BDS carrierphase residuals are less than those of GPS, GLONASS, and Galileo. The RMS values of the raw carrierphase measurements for the four systems are at the same level, ranging from 0.40 to 0.63 cm. The IF carrierphase residuals of BDS and Galileo are slightly larger than those of GPS and GLOANSS. This is possibly because the unprecise orbit, clock and PCO/PCV errors have little influence on the raw observations; while these errors are amplified in the IF combination.
Singlesystem PPP based on raw and IF observations
Compared with BDS2 and Galileo, GPS and GLONASS have better global PPP performance. Therefore, we mainly consider PPP performance on a global scale for GPS and GLONASS. The reference coordinates were collected from the IGS weekly solution at GPS week 2057 on June, 2019.
Figure 4 shows the time series of the positioning accuracy of GPS PPP for the stations; the averaged convergence times for the 96 stations in the E, N, and U components are also plotted. Although GPS PPP based on dualfrequency raw observations must estimate more ionospheric parameters, it introduces a priori information and ionospheric temporal and spatial constraints. Also, because of the lower noise of raw observations, the convergence time is shortened by 2 to 3 min compared with the PPP with IF observations. With the additional L5 and C5 observations, the convergence time is further reduced; the corresponding convergence times for the E, N, and U components are 32, 9, and 34 min, respectively. Normally, GPS PPP can converge to 10 cm within 40 min regardless of whether raw observations or IF observations are used.
After convergence, the positioning accuracy for the stations are shown in Fig. 5. The RMS values for the E, N, and U components are all lower than 10 cm. It can be seen that the stations have comparable accuracy on a global scale. The positioning accuracy of PPP with dualfrequency raw observations is slighter higher than that of PPP based on IF observations. The mean RMS values for the E, N, and U components are respectively 2.47 cm, 1.79 cm, and 3.35 cm for PPP based on IF observations and 2.2 cm, 1.39 cm, and 3.14 cm for PPP based on dualfrequency raw observations, as listed in Table 2. The RMS value for the U component is the highest but is still lower than 4.0 cm on average. After adding GPS L5 signals, the mean RMS value is lower, but the improvement is limited.
The time series of positioning error for GONASS PPP are plotted in Fig. 6. Because only two GLONASS satellites have the capability of transmitting G3 signals, the G3 signal is not included in the data processing. Compared with GPS PPP, GLONASS has fewer available satellites. The positioning error of GLOANSS is larger than that of GPS. The convergence times of GLONASS PPP based on raw observations are 36, 22, and 41 min for the E, N, and U components, respectively, which is longer than that of GPS PPP based on dualfrequency raw observations. The PPP results based on IF observations converged slightly slower than those of PPP based on dualfrequency raw observations. The convergence times of GLONASS PPP with IF observations for the E, N, and U components are 39, 24, and 42 min, respectively. Therefore, GLONASS PPP using dualfrequency raw and IF observations have comparable convergence times on a global scale.
The corresponding positioning accuracy of GLONASS PPP after convergence for the stations is illustrated in Fig. 7 and Table 3. Generally, the U component has the longest convergence time and lowest accuracy compared with the E and N components. The positioning accuracy of GLOANSS PPP is lower than that of GPS, and the RMS value of GLONASS PPP based on raw observations is slightly lower than that of PPP using dualfrequency IF observations. The averaged RMS values for the stations at E, N, and U are 2.69, 1.81, and 3.82 cm for PPP based on raw observations, and 2.72, 2.09, and 4.03 cm for PPP with IF observations. Therefore, the GLONASS PPP results based on raw observations can be converged to 10 cm within 45 min for the E, N, and U components, and the positioning accuracy after convergence is lower than 3 cm in the E and N components and lower than 4 cm in the U component.
Multiconstellation GNSS PPP
Figure 8 plots the results of multiGNSS PPP based on IF observations and raw observations. Compared with the singleGNSS PPP, multiGNSS PPP can efficiently shorten the convergence time to less than 15 min for the E and N components, while the convergence time for the U component is approximately 3 to 10 min longer than the E and N components. Moreover, the convergence time of PPP based on dualfrequency raw observations is 1 to 2 min shorter than that of PPP based on IF observations. Moreover, after introducing multifrequency observations, the convergence time is slightly reduced again. It can be clearly seen that the positioning errors are smaller after convergence compared with those of singleGNSS PPP. In summary, combining the observations from multiconstellation GNSS observations can significantly reduce PPP convergence time.
The positioning accuracy for the stations is illustrated in Fig. 9. The mean RMS values of the E, N, and U components for different solutions are listed in Table 4. The 3D RMS values of the stations are below 8 cm. The multiGNSS PPP based on raw observations has a higher accuracy compared with that of multiGNSS using dualfrequency IF observations. For some stations, the 3D RMS value of the PPP results based on dualfrequency raw observations is larger than that of the PPP based on IF observations. The mean RMS values of the E, N, and U components for PPP based on dualfrequency raw observations are 2.01, 1.35, and 2.82 cm, respectively. They are lower than those of the dualfrequency IF PPP, which are 2.09, 1.50, and 2.94 cm, respectively. By introducing multifrequency signals, the mean RMS values of the multifrequency PPP are improved to 1.25, 1.06, and 2.37 cm, respectively. Currently, the PCO values at the receiver ends for BDS and Galileo satellites are unknown in data processing, so we use the values of GPS PCO as substitutes. Although it may not be precise, the multiGNSS can improve the positioning accuracy after reducing the weights of BDS and Galileo observations. Therefore, the additional observations from multiGNSS and multifrequency not only improve accuracy but also reduce convergence time.
Conclusions
GNSS satellites are increasingly becoming available for providing global PPP services, and MGEX stations can receive more than 40 GNSS satellites at an epoch. Based on the globally distributed MGEX stations, we assessed the performance of multiGNSS PPP based on raw and IF observations. The results showed that the code measurements of Galileo have the lowest residuals compared with those of GPS and BDS. Currently, because there are no available PCO and PCV values for the Galileo and BDS satellites, the GPS PCO/PCV values were used as substitutes. Due to the relatively large orbit, clock and PCO/PCV errors of BDS and Galileo satellites, the phase residuals of dualfrequency IF combination of Galileo and BDS are larger than those of GPS and GLONASS. By reducing the weights of the BDS and Galileo observations, multifrequency and multiconstellation GNSS PPP based on raw observations achieved better performance than singleGNSS PPP. The fusion of multiconstellation and multifrequency GNSS observations can significantly shorten convergence time, which was reduced from approximately 40 min for GPS PPP to less than 20 min for multiGNSS PPP. After convergence, the positioning accuracy of multiGNSS PPP was improved by 0.5 to 1.0 cm compared with GPS or GLONASS PPP. The positioning accuracy of MultiGNSS could be further improved with the precise BDS and Galileo orbits, clock and PCO/PCV products in the future.
Availability of data and materials
The GNSS datasets used during the current study are available from the Crustal Dynamics Data Information System (CDDIS) repository, ftp://ftp.cddis.eosdis.nasa.gov/pub/gnss/data/. The GNSS precise orbit and clock products issued by Wuhan University are available from the Institut Géographique National (IGN) repository, ftp://igs.ign.fr/pub/igs/products/mgex/. The GNSS multifrequency DCB products generated by Chinese Academy of Sciences (CAS) are available from the Institut Géographique National (IGN) repository, ftp://igs.ign.fr/pub/igs/products/mgex/dcb. The IRI2016 source code is available from http://irimodel.org/IRI2016/.
Abbreviations
 GNSS:

global navigation satellite system
 BDS:

BeiDou navigation satellite system
 GEO:

geostationary earth orbit
 IGSO:

inclined geosynchronous orbit
 MEO:

medium earth orbit
 PPP:

precise point positioning
 IGS:

International GNSS Service
 MGEX:

multiGNSS experiment
 ACs:

analysis centers
 DCB:

differential code bias
 IF:

ionosphericfree
 PCV:

phase center variation
 PCO:

phase center offset
 TEC:

total electron content
 VTEC:

vertical total electron content
 STEC:

slant total electron content
 TECU:

total electron content unit
 IRI:

International Reference Ionosphere
 DOY:

day of year
 PANDA:

positioning and navigation data analysis
 E:

east
 N:

north
 U:

up
 RMS:

root mean squares
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Acknowledgements
Thanks to IGSMGEX, Wuhan University for providing the GNSS data, Galileo precise orbits, and clock products. Special thanks to the China Scholarship Council (CSC) and University of Nottingham. Under the foundation of CSC, the first author was given the opportunity to study at the University of Nottingham, UK for two years from Nov. 2017 to Nov. 2019. We thank all reviewers for their valuable, constructive, and prompt comments.
Funding
China Scholarship Council (CSC). Under the foundation of CSC, the first author was given the opportunity to study at the University of Nottingham, UK to complete this research with Prof. Meng and Prof. Jiang.
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XA developed the platform, processed and analyzed the results, and drafted the paper. XM proposed ideas, analyzed the results, and revised and proofread the paper. WJ analyzed the results and revised and proofread the paper. All authors read and approved the final version of the manuscript.
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An, X., Meng, X. & Jiang, W. Multiconstellation GNSS precise point positioning with multifrequency raw observations and dualfrequency observations of ionosphericfree linear combination. Satell Navig 1, 7 (2020). https://doi.org/10.1186/s430200200009x
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DOI: https://doi.org/10.1186/s430200200009x