GNSS Carrier-Phase Multipath Modeling and Correction: A Review and Prospect of Data Processing Methods
Abstract
:1. Introduction
2. Multipath Error Principle and Mitigation Methods
2.1. Generation Principle of Multipath Errors
2.2. Multipath Error Mitigation Methods
3. Research Status of the Multipath Error Data Processing Algorithm
3.1. Multipath Error Mitigation Methods Based on the Stochastic Model
3.2. Multipath Error Mitigation Method Based on the Function Model
3.2.1. Multipath Error Mitigation Method Based on the Coordinate Domain
3.2.2. Multipath Error Mitigation Method Based on the Observation Domain
- According to the first phase of GNSS navigation ephemeris data, the average angular velocity of different satellites is calculated and the time offset of the repeat period of different satellites is obtained.
- According to the GNSS baseline observation data of the first phase, errors such as satellite clock error, receiver clock error, satellite orbit error, tropospheric delay, and ionospheric delay are eliminated by constructing a double-difference observation equation. The double-difference ambiguity is fixed using the LAMBDA algorithm.
- Double-difference residuals are converted to single-difference residuals based on the “zero-mean assumption”; wavelet analysis, EMD, or other filters are used to process the signal, and low-frequency components of single-difference residuals are extracted.
- Using the obtained satellite repetition cycle time offset, the satellite single-difference residual time series is time-corrected based on GPST to obtain the single-difference residual low-frequency component correction model for the next repetition cycle. Finally, the SF model of the observation domain for multipath error mitigation in the next period is obtained.
- According to the GNSS baseline observation data of the second phase, the satellite single-difference observation equation is constructed, and the corresponding satellite multipath error correction value in the sidereal filtering multipath model is extracted based on the GPST timestamp. The single-difference observation equation weakened by the multipath error is reconstructed into a satellite double-difference observation equation.
- The Kalman filter is used to estimate the floating-point solution of the ambiguity, and the LAMBDA algorithm is used to fix the double-difference ambiguity. The double-difference ambiguity is substituted into the solution equation to obtain a fixed-point solution for the baseline solution, which mitigated the multipath error.
- Single-difference residual low-frequency components are extracted using the filtering method from the first-period observation data.
- For different satellite constellations, different hemisphere geometric models are established. Based on the minimum elevation, maximum elevation, azimuth angle, minimum grid latitude, and minimum grid longitude, the hemispherical geometric model of GPS/BDS IGSO/BDS MEO satellites is established; based on the minimum elevation, maximum elevation, minimum azimuth, maximum azimuth, minimum latitude interval, and minimum longitude interval, the semi-celestial geometric model of the BDS GEO satellite is established.
- Based on the instantaneous elevation and azimuth of the satellite, the low-frequency components of the instantaneous single-difference residual of the satellite are divided into the corresponding grids of the hemispherical geometric model (HGM)/GEO hemispherical geometric model (GEOHGM).
- The mean value of the low-frequency component of the satellite single-difference residual in each grid is calculated, that is, the parameter fitting of the semi-celestial spherical grid. Finally the MHM/MHMGEO corresponding to HGM/HGMGEO is obtained.
- The second-phase GNSS baseline monitoring data are used to construct a single-difference observation equation. The grid parameters of the MHM model are obtained based on the satellite azimuth and elevation of the current epoch and the multipath error correction of the single-difference observation equation is conducted.
- The single-difference observation equation that was weakened by multipath errors was reconstructed into a satellite double-difference observation equation. The LAMBDA algorithm is used to fix the double-difference ambiguity and the double-difference ambiguity is substituted into the solution equation to obtain a fixed-point solution for the baseline solution.
3.2.3. Summary
4. Application Scenarios of the Multipath Error Mitigation Algorithm
4.1. GNSS Deformation Monitoring
4.2. Precise Positioning of Urban Areas
5. Conclusions
- Extend the current multipath error correction modeling method to the multi-frequency data of multi-GNSS systems, including GPS, BDS, Galileo, GLONASS, and other systems. Zou et al. [115] extended the MHM method and proposed a MHGM (multi-point hemispherical grid model, MHGM) method suitable for multi-GNSS systems. This approach enabled the fusion of observation data from different GNSS systems for MHGM modeling, demonstrating a significant attenuation effect on the multipath errors of GNSS signals. At present, the fusion processing of multi-system and multi-frequency GNSS data has emerged as the future trend in satellite positioning [116]. Research into multipath error processing methods suitable for multi-system and multi-frequency GNSS data constitutes a focal point for future investigations.
- Enhance the effectiveness of multipath mitigation methods in practical applications. In order to improve the positioning accuracy and operating efficiency in actual engineering practice, research on multipath error mitigation should be developed to achieve real-time application, intelligence [117], and engineering application, and the actual application scenarios should be extended to single-point positioning, dynamic scenes, and more complex environments with severe occlusions.
- Integrate deep learning and machine learning technology into multipath error mitigation. Xu and Tao [118] used a combination of deep learning network long short-term memory network (LSTM) and EMD to predict and weaken the impact of multipath effects. Tao et al. [119] constructed a time–frequency mask and convolutional neural network (TFM–CNN) model, which had a remarkable effect on separating the multiple paths of GNSS observation sequences in real-time deformation monitoring. Gong et al. [120] used the K-means clustering algorithm from machine learning to distinguish direct signals and reflected signals in urban environments to achieve the purpose of improving positioning accuracy. By processing GNSS data through deep learning and machine learning technology, the strengths of these approaches are leveraged to improve the capability of handling GNSS data and enhance the accuracy and reliability of GNSS positioning results.
Author Contributions
Funding
Data Availability Statement
Acknowledgments
Conflicts of Interest
References
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Type | Method | Year | Scholar |
---|---|---|---|
Antenna method | Choke ring technology | 1998 | Filippov [18] |
Compression wheel antenna technology | 2001 | Krantz [20] | |
Dual-polarized antenna technique | 2010 | Groves [22] | |
Cross-plate reflection planes | 2013 | Maqsood [23] | |
Single orthogonal dual-polarized GNSS antenna | 2017 | Zhang [24] | |
Receiver method | Narrow spatial correlator technique | 1992 | Dieredonck [27] |
Multipath elimination delay-locked loop technology | 2002 | Nee [25] | |
Group-delay multiple amplitude phase-locked loop technology | 2013 | Chen [26] | |
New ranging code tracking loop | 2022 | Qiu [28] |
Model Type | Contributions | Year | Scholar |
---|---|---|---|
C/N0 | Construction of the SIGMA-Δ model based on C/N0 | 1999 | Brunner [29] |
dual-frequency C/N0 | 2019 | Zhang [35] | |
SNR | Validation of the effectiveness of the SNR method to | 2003 | Zhang [30] |
refine a stochastic model for GPS | 2003 | Liu [31] | |
Elevation | Refined stochastic model for multi-GNSS | 2020 | Xi [36] |
real-time adaptive weighting model | 2018 | Zhang [34] |
Orbit Type | Repeat Period | |
---|---|---|
GPS | MEO | 1 day |
BDS | GEO | 1 day |
IGGSO | 1 day | |
MEO | 7 days | |
GLONASS | MEO | 8 days |
Galileo | MEO | 10 days |
Method | Scenario | System | Year | Scholar |
---|---|---|---|---|
Multipath spherical harmonic model | Baseline positioning | GPS | 1991 | Cohen [78] |
MPS | PPP | GNSS | 2015 | Fuhrmann [79] |
MHM | Baseline positioning | GNSS | 2016 | Dong [80] |
T-MHM | Baseline positioning, PPP | GNSS | 2019 | Wang [82] |
M-MHM | PPP | GNSS | 2019 | Zheng [84] |
MHGM | Baseline positioning | GPS | 2020 | Wang [85] |
AT-MHM | Baseline positioning, PPP | GNSS | 2020 | Wang [83] |
Type | Method | Experimental Scene | System | Year | Scholar |
---|---|---|---|---|---|
Coordinate domain | CVVF | Baseline positioning | GPS | 2005 | Zheng [42] |
EMD | Baseline positioning | GPS | 2006 | Dai [43] | |
Wavelet signal-layer automatic identification | Baseline positioning | GPS | 2008 | Zhong [50] | |
EEMD | Baseline positioning | GPS | 2012 | Xue [44] | |
PCA-EMD-ICA-R | Baseline positioning | GPS | 2014 | Dai [51] | |
SSA | Baseline positioning | GPS | 2015 | Lu [49] | |
CEEMD | Baseline positioning | GPS | 2018 | Luo [45] | |
GED | Baseline positioning | BDS | 2018 | Chen [47] | |
EMD-RLS | Baseline positioning | BDS | 2019 | Yan [48] | |
EWT | Baseline positioning | GPS | 2020 | Luo [52] | |
Wavelet analysis | Baseline positioning | GPS | 2021 | Zhang [53] | |
Least-squares harmonic estimation | Baseline positioning | GNSS | 2022 | Cao [54] | |
AF-ICA | Baseline positioning | GNSS | 2022 | Yuan [55] | |
CEEMDAN-WT | Baseline positioning | GPS, BDS | 2022 | Tong [46] | |
Observation domain | Wavelet analysis | Baseline positioning | GPS | 2005 | Satirapod [62] |
Wavelet detrending technique | Baseline positioning | GPS | 2009 | El-Ghazouly [63] | |
SF based on single differences | Baseline positioning | GNSS | 2010 | Zhong [57] | |
Three-level wavelet packet-based denoising method | Baseline positioning | GPS | 2017 | Lau [66] | |
KF-RTSS | Baseline positioning | BDS | 2018 | Zhang [65] | |
MHM_V | Baseline positioning | GPS | 2021 | Zhang [86] | |
MHM based on EEMD | Baseline positioning | GNSS | 2022 | Tang [87] | |
SF based on EC wavelet packet transform | Baseline positioning | GNSS | 2022 | Su [67] | |
SF-based sym6 wavelet decomposition | Baseline positioning | BDS | 2022 | Yang [73] | |
Window-matching method based on SF | Baseline positioning | GPS, BDS | 2022 | Zhan [61] | |
RWM | Baseline positioning | Galileo | 2023 | Hu [75] | |
LSC | Baseline positioning, PPP | GPS, Galileo | 2023 | Tian [76] |
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Zhang, Q.; Zhang, L.; Sun, A.; Meng, X.; Zhao, D.; Hancock, C. GNSS Carrier-Phase Multipath Modeling and Correction: A Review and Prospect of Data Processing Methods. Remote Sens. 2024, 16, 189. https://doi.org/10.3390/rs16010189
Zhang Q, Zhang L, Sun A, Meng X, Zhao D, Hancock C. GNSS Carrier-Phase Multipath Modeling and Correction: A Review and Prospect of Data Processing Methods. Remote Sensing. 2024; 16(1):189. https://doi.org/10.3390/rs16010189
Chicago/Turabian StyleZhang, Qiuzhao, Longqiang Zhang, Ao Sun, Xiaolin Meng, Dongsheng Zhao, and Craig Hancock. 2024. "GNSS Carrier-Phase Multipath Modeling and Correction: A Review and Prospect of Data Processing Methods" Remote Sensing 16, no. 1: 189. https://doi.org/10.3390/rs16010189
APA StyleZhang, Q., Zhang, L., Sun, A., Meng, X., Zhao, D., & Hancock, C. (2024). GNSS Carrier-Phase Multipath Modeling and Correction: A Review and Prospect of Data Processing Methods. Remote Sensing, 16(1), 189. https://doi.org/10.3390/rs16010189