Abstract
Recent research has demonstrated that the undifferenced integer ambiguities can be recovered using products from a network solution. The standard dual-frequency PPP integer ambiguity resolution consists of two aspects: Hatch-Melbourne-Wübbena wide-lane (WL) and ionosphere-free narrow-lane (NL) integer ambiguity resolution. A major issue affecting the performance of dual-frequency PPP applications is the time it takes to fix these two types of integer ambiguities, especially if the WL integer ambiguity resolution suffers from the noisy pseudorange measurements and strong multipath effects. With modernized Global Navigation Satellite Systems, triple-frequency measurements will be available to global users and an extra WL (EWL) model with very long wavelength can be formulated. Then, the easily resolved EWL integer ambiguities can be used to construct linear combinations to accelerate the PPP WL integer ambiguity resolution. Therefore, we propose a new reliable procedure for the modeling and quality control of triple-frequency PPP WL and NL integer ambiguity resolution. First, we analyze a WL integer ambiguity resolution model based on triple-frequency measurements. Then, an optimal pseudorange linear combination which is ionosphere-free and has minimum measurement noise is developed and used as constraint in the WL and the NL integer ambiguity resolution. Based on simulations, we have investigated the inefficiency of dual-frequency WL integer ambiguity resolution and the performance of EWL integer ambiguity resolution. Using almanacs of GPS, Galileo and BeiDou, the performances of the proposed triple-frequency WL and NL models have been evaluated in terms of success rate. Comparing with dual-frequency PPP, numerical results indicate that the proposed triple-frequency models can outperform the dual-frequency PPP WL and NL integer ambiguity resolution. With 1 s sampling rate, generally, only several minutes of data are required for reliable triple-frequency PPP WL and NL integer ambiguity resolution. Under benign observation situations and good geometries, the integer ambiguity can be reliably resolved even within 10 s.
Similar content being viewed by others
References
Collins P (2008) Isolating and estimating undifferenced GPS integer ambiguities. Proceedings of ION-NTM-2008, Institute of navigation, San Diego CA 720–732
Collins P, Bisnath S (2011) Issues in ambiguity resolution for precise point positioning. Proc ION GNSS 2011, Institute of Navigation, Portland OR, Sept 679–687
Feng Y (2008) GNSS three carrier ambiguity resolution using ionosphere-reduced virtual signals. J Geodesy 82(12):847–862
Ge M, Gendt G, Rothacher M, Shi C, Liu J (2008) Resolution of GPS carrier-phase ambiguities in precise point positioning (PPP) with daily observations. J Geodesy 82(7):389–399
Geng J, Bock Y (2013) Triple-frequency GPS precise point positioning with rapid ambiguity resolution. J Geodesy 87(5):449–460
Geng J, Meng X, Dodson A, Teferle F (2010a) Integer ambiguity resolution in precise point positioning: method comparison. J Geodesy 84(9):569–581
Geng J, Teferle F, Meng X, Dodson A (2010b) Towards PPP-RTK: ambiguity resolution in real-time precise point positioning. Adv Space Res 47(10):1664–1673
Geng J, Meng X, Dodson A, Ge M, Teferle F (2010c) Rapid re-convergences to ambiguity-fixed solutions in precise point positioning. J Geodesy 84(12):705–714
Hatch R (1983) The synergism of GPS code and carrier measurements. International geodetic symposium on satellite doppler positioning 2: 1213–1231
Hatch R (2006) A new three-frequency, geometry-free, technique for ambiguity resolution. Proc ION GNSS, Institute of Navigation, Fort Worth, TX, September, pp 309–316
Jan S, Chan W, Walter T, Enge P (2001) Matlab simulation toolset for SBAS availability analysis. Proc ION GPS 2001, Institute of Navigation, Salt Lake City, UT, Sept, pp. 11–14
Kouba J (2009) Guide to using international GNSS service (IGS) products, http://igscb.jpl.nasa.gov/igscb/resource/pubs/UsingIGSProductsVer21.pdf
Laurichesse D (2012) Phase biases estimation for undifferenced ambiguity resolution. PPP–RTK and open standards symposium, March 12–13, Frankfurt
Laurichesse D, Mercier F, Berthias J, Broca P, Cerri L (2009) Integer ambiguity resolution on undifferenced GPS phase measurements and its application to PPP and satellite precise orbit determination. Navigation 56(2):135–149
Laurichesse D, Mercier F, Berthias J (2010) Real-time PPP with undifferenced integer ambiguity resolution, experimental results. Proceedings of ION GNSS 2010, Institute of Navigation, Portland, OR, Sept 2534–2544
Li T, Wang J (2012) Some remarks on GNSS integer ambiguity validation methods. Survey Rev 44(326):230–238
Li T, Wang J (2013) Analysis of the upper bounds for the integer ambiguity validation statistics. GPS Solut. doi:10.1007/s10291-013-0312-1
Li B, Feng Y, Shen Y (2010) Three carrier ambiguity resolution: distance-independent performance demonstrated using semi-generated triple frequency GPS signals. GPS Solut 14(2):177–184
Melbourne W (1985) The case for ranging in GPS based geodetic systems. Proceedings of first international symposium on precise positioning with global positioning system, Rockville, 15–19 April, 373–386
Takasu T, Yasuda A (2009) Development of the low-cost RTK-GPS receiver with an open source program package RTKLIB. Proceedings of the international symposium on GPS/GNSS, 4–6 Nov, Jeju, Korea
Teunissen P (1995) The least-squares ambiguity decorrelation adjustment: a method for fast GPS integer estimation. J Geodesy 70(1–2):65–82
Teunissen P (1998) Success probability of integer GPS ambiguity rounding and bootstrapping. J Geodesy 72(10):606–612
Teunissen P (2003) Integer aperture GNSS ambiguity resolution. Artif Satell 38(3):79–88
Verhagen S (2005) The GNSS integer ambiguities: estimation and validation. Ph.D. thesis, Publications on Geodesy 58 Netherland Geodetic Commission, Delft
Teunissen P, Verhagen, S (2008) GNSS ambiguity resolution: when and how to fix or not to fix? In: VI Hotine-Marussi symposium on theoretical and computational geodesy: challenge and role of modern geodesy, Wuhan, China, 29th May–2nd June 2006, Series: International Association of Geodesy Symposia, 132: 143–148
Verhagen S, Teunissen P (2012) The ratio test for future GNSS ambiguity resolution. GPS Solutions 1–14. doi:10.1007/s10291-012-0299-z
Verhagen S, Li B, Teunissen P (2013) Ps-LAMBDA: ambiguity success rate evaluation software for interferometric applications. Comput Geosci 54:361–376
Wang J, Stewart M, Tsakiri M (1998) A discrimination test procedure for ambiguity resolution on-the-fly. J Geodesy 72(11):644–653
Wang J, Stewart M, Tsakiri M (2000) A comparative study of the integer ambiguity validation procedures. Earth, Planets Space 52(10):813–817
Wu J, Wu S, Hajj G, Bertiger W, Lichten S (1993) Effects of antenna orientation on GPS carrier phase. Manuscripta Geodaetica 18:91–98
Wübbena G (1985) Software developments for geodetic positioning with GPS using TI-4100 code and carrier measurements. Proceedings of first international symposium on precise positioning with global positioning system, Rockville, 15–19 April, 403–412
Zumberge J, Heflin M, Jefferson D, Watkins M, Webb F (1997) Precise point positioning for the efficient and robust analysis of GPS data from large networks. J Geophys Res 102(B3):5005–5017
Acknowledgments
The authors would like to acknowledge three anonymous reviewers for their valuable comments on this manuscript. Chinese Scholarship Council (CSC) is acknowledged for supporting the first author’s Ph.D. studies at the University of New South Wales, Sydney, Australia.
Author information
Authors and Affiliations
Corresponding author
Appendices
Appendix 1
Ignoring the UPDs in (11), the ambiguity term can be expressed as \(x\lambda_{1} N_{1} + y\lambda_{2} N_{2} + z\lambda_{5} N_{5}\). Since our intention is to form the ambiguity term with both WL integer ambiguities and EWL integer ambiguities, we have:
Therefore, when the term \((x\lambda_{1} + y\lambda_{2} + z\lambda_{5} )\) equals to 0, the third condition and the objective model can be generated accordingly.
Appendix 2
With the conditions of (15a) and (15b), coefficients x and y can be expressed as \(x = t_{1} + m_{1} z\) and \(y = t_{2} + m_{2} z\), with \(t_{1} = \frac{{f_{1}^{2} }}{{f_{1}^{2} - f_{2}^{2} }}\), \(t_{2} = \frac{{ - f_{2}^{2} }}{{f_{1}^{2} - f_{2}^{2} }}\), \(m_{1} = \frac{{ - f_{1}^{2} (f_{5}^{2} - f_{2}^{2} )}}{{f_{5}^{2} (f_{1}^{2} - f_{2}^{2} )}}\), \(m_{2} = \frac{{ - f_{2}^{2} (f_{1}^{2} - f_{5}^{2} )}}{{f_{5}^{2} (f_{1}^{2} - f_{2}^{2} )}}\). The minimization of the third condition (15c) becomes:
Solving the above quadratic equation, we have:
The minimization function can be obtained by setting the first term of (21) as 0 and x, y and z can be generated. Then it is observed that (21) is smaller than \(t_{1}^{2} + t_{2}^{2} a^{2}\), which is the measurement noise variance of dual-frequency ionosphere-free model (9). In a similar manner, it can be proven that (21) is smaller than the measurement noises of ionosphere-free L1 and L5 model and L2 and L5 model.
Rights and permissions
About this article
Cite this article
Li, T., Wang, J. & Laurichesse, D. Modeling and quality control for reliable precise point positioning integer ambiguity resolution with GNSS modernization. GPS Solut 18, 429–442 (2014). https://doi.org/10.1007/s10291-013-0342-8
Received:
Accepted:
Published:
Issue Date:
DOI: https://doi.org/10.1007/s10291-013-0342-8