# GLONASS CDMA L3 ambiguity resolution and positioning

## Abstract

A first assessment of GLONASS CDMA L3 ambiguity resolution and positioning performance is provided. Our analyses are based on GLONASS L3 data from the satellite pair SVNs 755-801, received by two JAVAD receivers at Curtin University, Perth, Australia. In our analyses, four different versions of the two-satellite model are applied: the geometry-free model, the geometry-based model , the height-constrained geometry-based model, and the geometry-fixed model. We study the noise characteristics (carrier-to-noise density, measurement precision), the integer ambiguity resolution performance (success rates and distribution of the ambiguity residuals), and the positioning performance (ambiguity float and ambiguity fixed). The results show that our empirical outcomes are consistent with their formal counterparts and that the GLONASS data have a lower noise level than that of GPS, particularly in case of the code data. This difference is not only seen in the noise levels but also in their onward propagation to the ambiguity time series and ambiguity residuals distribution.

## Keywords

GLONASS CDMA Integer ambiguity resolution GPS PDOP ADOP## Introduction

A first assessment of GLONASS CDMA L3 ambiguity resolution and positioning performance is provided. The navigation signals of the GLONASS system are traditionally transmitted on the basis of the frequency division multiple access (FDMA) technique (ICD-GLONASS 2008). As a consequence of the FDMA technique, inter-frequency biases are present that impede a straightforward integer resolution of the double-differenced (DD) ambiguities (Leick et al. 2015; Hofmann-Wellenhof et al. 2013). To resolve this issue, special calibration procedures have been proposed aimed at realizing GLONASS FDMA integer ambiguity resolution (Takac 2009; Yamada et al. 2010; Reussner and Wanninger 2011; Wanninger 2009). With the advent, however, of the GLONASS code division multiple access (CDMA) signals, double differences of the carrier-phase ambiguities become integer themselves and standard methods of integer ambiguity resolution can directly be applied to realize ambiguity-resolved precise positioning.

In February 2011, following the launch of the first GLONASS-K1 satellite, SVN 801 (R26) (IAC 2016), the Russian satellite system commenced transmitting CDMA signals on L3 (1202.025 MHz) (Urlichich et al. 2010; Thoelert et al. 2011; Oleynik 2012). The current constellation (March 2016) consists of 28 satellites of which 26 are of GLONASS-M series, and two are of GLONASS-K series, subseries GLONASS-K1 (IAC 2016). This constellation has *four* CDMA-transmitting satellites, i.e., SVNs 801 (R26) and 802 (R17) of series K, 755 (R21) and the newly launched 751 of series M, among which SVN 801 is undergoing a flight test (IAC 2016). All the satellites of the GLONASS-K series as well as the last seven satellites of the GLONASS-M series will be capable of transmitting CDMA signals on the L3 frequency (Oleynik 2012; Montenbruck et al. 2015).

It is expected that the last satellites of the GLONASS-M series will be launched by 2017 and that of the GLONASS-K1 series, 11 satellites will be launched through 2020. The GLONASS-K2 satellites will be launched in early 2017 (GPS World 2015). All these satellites will be able to transmit CDMA signals. Providing signals on the frequencies used by the other GNSSs (GPS L5 and L1) is also part of the future plan (Karutin 2012). An overview of these signals was presented in Urlichich et al. (2010, 2011) and Karutin (2012), and Thoelert et al. (2011) assessed the signal quality and the modulation quality of the L3 CDMA civil signal of SVN 801 received by a high-gain antenna.

We provide for the first time an analysis of the GLONASS L3 ambiguity resolution and corresponding positioning performance. Our analyses are based on L3 data of the GLONASS satellite pair R21–R26, received by two JAVAD receivers at Curtin University, Perth, Australia. We also compare our results with corresponding results obtained for the GPS L1 observables from the satellite pair G21–G29, having almost the same trajectories as those of R21–R26 for the periods considered in this contribution. We start first with the formulation of the four versions of the two-satellite models used in our analyses. These four versions are the geometry-free model, the geometry-based model, the height-constrained geometry-based model and the geometry-fixed model. We then study the noise characteristics of the GLONASS CDMA data and compare it to their GPS L1 counterparts. We present results on the carrier-to-noise density and on the estimated zenith-referenced measurement precision. Next, double-differenced (DD) ambiguity resolution is taken up. This is done for all four models, both for GLONASS and GPS. In this analysis, we present the empirical results and compare them for consistency with their formal counterparts. Following the ambiguity resolution analyses, the positioning performance is discussed. This is done both for the ambiguity float case as well as for the ambiguity fixed case. Besides, we illustrate a case of a near rank-deficiency and demonstrate that the PDOP and ADOP characteristics can be quite distinct and that one therefore should not confuse a poor PDOP with poor ambiguity resolution capabilities. Finally, a summary and conclusions are provided.

## Two-satellite observational model

As our analyses are based on data from the GLONASS satellites R21 and R26, we first formulate the underlying two-satellite model. In the following, this formulation will be presented for four different models of different strengths, i.e., geometry-free, geometry-based, height-constrained geometry-based, and geometry-fixed model.

### From geometry-free to geometry-fixed

*E*{.} and dispersion

*D*{.}, the corresponding two-satellite double-differenced (DD) system of observation equations reads

*p*and

*φ*being the DD code and phase observable, respectively,

*ρ*the DD receiver-satellite range and

*a*the DD integer ambiguity in cycles. The ambiguity

*a*is linked to the DD phase observable through the signal wavelength

*λ*. With the elevation-dependent weighting functions,

*w*

_{ θ1}and

*w*

_{ θ2}(see 4), for the first and the second satellite with elevation angles

*θ*

_{1}and

*θ*

_{2}, respectively, the final weight becomes \(w = \tfrac{1}{2}[w_{\theta 1}^{ - 1} + w_{\theta 2}^{ - 1} ]^{ - 1}\). The zenith-referenced standard deviations of the undifferenced code and phase observables are denoted as

*σ*

_{ p }and

*σ*

_{ φ }, respectively.

- 1.
Geometry-free model (GFr): This is the model as formulated in (1). As it is parametrized in

*ρ*, it is free from the receiver-satellite geometry; - 2.
Geometry-based model (GB): This model follows from linearizing (1) with respect to the unknown receiver coordinates. The receiver-satellite geometry is then taken into account through the parametrization

with$$\delta \rho \,\, = \,\, - c^{T} \,\delta b$$(2)*δρ*being the receiver-satellite range increment,*c*the 3-vector containing the between-satellite single-differenced (SD) receiver-satellite unit direction vectors, and*δb*= [*δN*,*δE*,*δH*]^{ T }the unknown between-receiver baseline increment vector; - 3.
Height-constrained geometry-based model (H-GB): This model follows if one adds the (weighted) height constraint to the geometry-based model,

$$E\{ \delta h\} = [0,0,1]\delta b;\quad D\{ \delta h\} = \sigma_{h}^{2}$$(3)- 4.
Geometry-fixed model (GFi): In this model the positions of the receiver and the satellite, and thus receiver-satellite range

*ρ*, are assumed known.

- 4.

Note that both the geometry-free and geometry-fixed model are solvable on an epoch-by-epoch basis, i.e., instantaneously. This is, however, not the case for the unconstrained and height-constrained geometry-based models. Two or more epochs are then needed for these models to be solvable.

### Two-satellite positioning

*one*pair of the DD observable (phase and code) over the

*red*period,

*one*pair over the

*blue*period and

*one*pair over the

*green*period. For example, the satellites location indicated with the same markers in Fig. 1 are associated with those instants of which the observables are used in one position solution. Thus, each solution computed is in fact a triple-epoch solution, for which the ambiguities as well as baseline coordinates are assumed constant. As the sampling rate of the epoch-triples is 1 s, the so obtained ambiguity and position time series also has a 1 Hz rate.

## Noise characteristics

In this section, we study the noise characteristics of the GLONASS CDMA data and compare it to their GPS L1 counterparts. We present results on the carrier-to-noise density, the estimated zenith-referenced measurement precision and on the influence of multipath.

### Measurement experiment

Characteristics of the experiment conducted for this study

# antennas | 2 |
---|---|

Antenna type | TRM59800.00 SCIS |

Receiver type | JAVAD TRE_G3TH_8 |

Location | Curtin University, Perth, Australia |

Data type | GLONASS L3, GPS L1 |

Satellites | R21–R26, G21-G29 |

Cutoff angle | 10° |

Date and time | UTC [05:20:00–10:03:00] on DOY 13 of 2016 |

UTC [04:47:00–09:31:00] on DOY 21 of 2016 | |

UTC [03:42:00–08:26:00] on DOY 37 of 2016 |

### Carrier-to-noise density

### Estimated precision (time correlation)

*θ*is the elevation of the satellite in degrees (Euler and Goad 1991). Incorporation of this elevation dependency in the LS-VCE allows one to estimate the zenith-referenced standard deviations of the undifferenced code and phase observables,

*σ*

_{ p }and

*σ*

_{ φ }. The corresponding VCE results are shown in Table 2. Note that the precision of the GLONASS L3 signal is significantly better than its GPS L1 counterpart. This is consistent with what was concluded from the C/N0 graph of Fig. 3. Also note that the table shows results for multipath-corrected standard deviations. The more detailed information on multipath correction is given in the next section. The so-obtained improvement is significant for both the GLONASS and GPS code observables, but most pronounced for GLONASS.

Estimated zenith-referenced standard deviations of the undifferenced original (multipath-corrected) code *σ* _{ p } and phase *σ* _{ φ } observables

Frequency | σ | σ |
---|---|---|

GPS L1 | 0.25 (0.22) | 1 (1) |

GLONASS L3 | 0.11 (0.05) | 2 (1) |

### Multipath

This vector is a zero-mean noise vector in case model (1) is correct, e.g., in case multipath is absent. In the presence of multipath, however, it captures the multipath on code, *m* _{ p }, as well as the multipath on phase *m* _{ φ }.

*m*

_{ p },

*m*

_{ φ }]

^{ T }was determined by computing

*ρ*from the known receiver and satellite positions, while the reference integer

*a*was computed using the very strong multi-epoch geometry-fixed model. Figure 4 displays the so-obtained DD code and phase multipath time series for the GLONASS L3 (R21–R26) and the GPS L1 (G21–G29) signals over the three time periods given in Table 1. Note that in all cases the time series of the three periods on DOYs 13, 21 and 37 indeed completely overlap each other.

As a further confirmation that the time series of the three DOYs 13, 21 and 37 capture the same phenomena, we now consider their day differences. These should then be showing zero-mean noise behavior with a variability that reflects the measurement precision. To do so, we first form the day-differenced DD code and phase multipaths, *dm* _{ p } and *dm* _{ φ }, by subtracting the DD multipath of DOY 37 from those of DOYs 13 and 21. Since the observables are highly dependent on the elevation of the satellites, the day-differenced DD multipaths are then normalized using the weight \(dw = \tfrac{w}{2}\). While *w* captures the DD observable weight of (1), the factor 2 in the denominator takes care of the differencing between the 2 days.

For the results of Table 2, as well as for the results in the sections following, the data of DOYs 13 and 21 have been multipath-corrected on an epoch-by-epoch basis using the multipath time series of DOY 37. This epoch-by-epoch correction ensures that no time correlation enters. The doubling in noise that enters through the correction is accounted for in the analyses that follow.

## Ambiguity resolution

In this section, the ambiguity resolution performance of the GLONASS L3 observables will be assessed and compared with that of the GPS L1 observables. Our assessment will be carried out using four different models: the geometry-free model, the unconstrained and height-constrained geometry-based model, and the geometry-fixed model.

### From geometry-free to geometry-fixed

The data used for our analysis is that of DOY 21 of 2016 over the time period UTC [04:47:00-06:55:00]. The solutions computed are triple-epoch solutions as explained earlier (see Fig. 1). Each of these solutions are obtained with a 1 Hz sampling rate, thus producing a time series of 3500 solutions. As there is only one unknown DD ambiguity in each case, the ambiguity resolution can be done through simple integer rounding. We denote the float ambiguity as \(\hat{a}\), the fixed (integer rounded) ambiguity as *a*ˇ, and the reference ambiguity as *a*. The reference DD ambiguity *a* has been obtained, as mentioned earlier, through the multi-epoch solution of the geometry-fixed model.

Figure 6 shows, for the receiver pair CUT3-CUCC, the time series of *a*ˆ − *a* and *a*ˇ − *a* for both the GLONASS satellite pair R21–R26 (left column) and the GPS satellite pair G21-G29 (right column). Float solutions are shown in *gray*, correctly fixed solutions in *green*, and incorrectly fixed solutions in *red*. These time series are given, from top to bottom, for the geometry-free model, the geometry-based model, the height-constrained geometry-based models using *σ* _{ h } = 0.2 m and *σ* _{ h } = 0.15 m, respectively, and the geometry-fixed model.

*a*ˇ −

*a*∈ {−2, −1, 1, 2}.

The ambiguity resolution performance improves if we switch to the stronger (unconstrained) geometry-based model (second row in Fig. 6). The incorrectly fixed GPS ambiguities do, however, still vary over a much larger range than their GLONASS counterparts. The performance improves further if we include a weighted height constraint (3rd and 4th row in Fig. 6). Now GLONASS and GPS have the same range of incorrectly fixed ambiguities, although the number of incorrectly fixed GLONASS solutions is of course still smaller than that of GPS. Finally, with the strongest model of all, being the geometry-fixed model (bottom row in Fig. 6), both GLONASS and GPS have all ambiguities correctly fixed. Thus, despite the larger noise level of the GPS ambiguities (compare the variability in the GLONASS and GPS float time series), all fixed ambiguities are now correct.

### Distribution of the ambiguity residuals

*a*ˆ −

*a*and

*a*ˇ −

*a*, respectively (Fig. 6). We now consider the ambiguity residual, i.e., the difference between the float and corresponding fixed solution, \(\check{\varepsilon}=\,\)

*a*ˆ −

*a*ˇ. The ambiguity residuals form the basis for ambiguity validation (Verhagen and Teunissen 2013). Figure 7 displays the histograms of the DD ambiguity residuals for the five different models considered. The domain of the histograms is [−0.5, +0.5]. Note that the shape of the histograms changes when one goes from the weaker model (geometry-free) to the stronger model (geometry-fixed). Hence, the ambiguity residuals are not normally distributed, i.e., they are not normally distributed even if the data are.

*x*∈ [−0.5, 0.5]. This distribution has also been shown (red curve) for the five cases in Fig. 7. It demonstrates the consistency between the empirical and formal distributions. The distribution (6) has two limiting cases. The distribution tends to the uniform distribution when \(\sigma_{{\hat{a}}}\) gets larger and it tends to the impulse function when \(\sigma_{{\hat{a}}}\) gets smaller. This behavior is indeed clearly present in Fig. 7 when one goes from the rather weak geometry-free model toward the much stronger geometry-fixed model.

### The ambiguity success rates

*j*th solution. As the results of Table 3 show, the empirical values are in good agreement with the formal ones. Also, the stronger the model is (from top to bottom), the larger the success rates become. Similarly, we see an increase in success rate with wavelength.

GLONASS L3, GPS L1, and GPS L2 ambiguity success rates, empirical and (formal), for the geometry-free (GFr) model, the geometry-based (GB) model, the height-constrained geometry-based (H-GB) model, and the geometry-fixed (GFi) model

Model | GLONASS L3 | GPS L1 | GPS L2 |
---|---|---|---|

GFr | 0.60 (0.55) | 0.12 (0.11) | 0.25 (0.20) |

GB | 0.77 (0.75) | 0.20 (0.19) | 0.34 (0.32) |

H-GB (σ | 0.92 (0.92) | 0.76 (0.75) | 0.87 (0.87) |

H-GB (σ | 0.96 (0.96) | 0.87 (0.87) | 0.95 (0.95) |

GFi | 1.00 (1.00) | 1.00 (1.00) | 1.00 (1.00) |

## Positioning performance

In this section, we assess the GLONASS L3 observables performance in positioning. All results belong to the triple-epoch geometry-based model without any height constraint.

### Two-satellite positioning: float solution

*b*ˆ, having mean

*E*(

*b*ˆ) =

*b*, is given as

*b*ˆ and constant

*r*

^{2}chosen such that a certain confidence level is reached (e.g., 95 %). The confidence ellipsoid of the fixed solution is obtained by replacing

*b*ˆ and \(Q_{{\hat{b}\hat{b}}}\) by

*b*ˇ and \(Q_{{\mathop b\limits^{ \vee } \mathop b\limits^{ \vee } }}\), respectively.

### Two-satellite positioning: fixed solution

*blue*and

*red*curves), while the East component would be much more precisely estimable (see

*green*curve).

## Interaction of positioning and ambiguity resolution

*blue*curve). This dramatic increase in PDOP must be due to a very poor relative receiver-satellite geometry. To explain the situation, we first show under which condition the multi-epoch geometry-based model becomes rank defect.

### Almost rank defect positioning geometry

*k*-epoch design matrix is formed by stacking the SD receiver-satellite unit vectors \(- c^{T} (i)\,{\text{for}}\quad i = 1,{ \ldots },k\) (see 2). Such a design matrix is rank defect if a vector \(d \in {\mathbb{R}}^{3}\) can be found such that

*c*(

*i*), the condition (11) means that at each epoch the two line-of-sight vectors make the

*same angle*with the direction vector

*d*. Geometrically this means that the rank deficiency occurs when the receiver-satellite unit line-of-sight vectors lie, at each epoch, on a cone having

*d*as its symmetry axis (Fig. 14). The symmetry axis of the cone, i.e., the vector

*d*, is then the direction in which the baseline solution becomes indeterminate. It is precisely this situation that explains the dramatic increase in PDOP values of Fig. 13.

*red*and

*green*) cone having direction

*d*(see 11), indicated as a

*purple*circle, as its symmetry axis. Although the blue satellite locations of R21 and R26 lie on a different cone, this (blue) cone has again the same symmetry axis

*d*. Hence, the geometry as shown in Fig. 15 is one in which the design matrix of the geometry-based model becomes (near) rank defect such that the baseline component in the direction of vector

*d*becomes very poorly estimable. It is the very poor precision of this component that drives the PDOP to such large values.

### Poor PDOP, good ADOP

Although the PDOP is often used as a quick diagnostic to infer whether the receiver-satellite geometry is favorable for positioning, one should be aware of the fact that the PDOP does not reveal whether or not one can expect ambiguity resolution to be successful (Teunissen et al. 2014). For that one needs the ADOP (Ambiguity Dilution of Precision). The ADOP is an easy-to-compute scalar diagnostic that measures the intrinsic model strength for successful ambiguity resolution. It is defined as the square-root of the determinant of the ambiguity variance matrix raised to the power of one over the ambiguity dimension (Teunissen 1997). The ADOP has several important properties. First, it is invariant against the choice of ambiguity parametrization. Second, it is a measure of the volume of the ambiguity confidence ellipsoid. And third, the ADOP equals the geometric mean of the standard deviations of the ambiguities, in case the ambiguities are completely decorrelated. Hence, in the one-dimensional case it simply reduces to the ambiguity standard deviation itself.

*σ*

_{ h }the a priori standard deviation of the height constraint, and \(\sigma_{{\hat{h}}}^{2}\) the variance of the unconstrained estimator of the height component. It can be seen that the ratio \(\sigma_{h}^{2} /\sigma_{{\hat{h}}}^{2}\) governs the benefit brought by the height constraint. One has the most benefit when

*σ*

_{ h }

^{2}= 0 and the least benefit when

*σ*

_{ h }

^{2}= ∞.

*σ*

_{ h }

^{2}is chosen much larger than \(\sigma_{{\hat{h}}}^{2}\), then the bracketed term of (12) becomes small. This means that if the receiver-satellite geometry is so strong that \(\sigma_{{\hat{h}}}^{2}\) is small, constraining the height with a variance

*σ*

_{ h }

^{2}much larger than \(\sigma_{{\hat{h}}}^{2}\) would have a negligible impact on ambiguity resolution. On the other hand, however, ambiguity resolution can benefit considerably from a weighted height constraint if \(\sigma_{{\hat{h}}}^{2}\) is large. The larger \(\sigma_{{\hat{h}}}^{2}\) is, the softer the weighted height constraint can be to still have an impact on ambiguity resolution. Thus, in case of a large PDOP, soft constraining of the height can still result in a very significant improvement of ambiguity resolution. The following examples shown in Fig. 16 make this clear.

The first row of Fig. 16 shows the PDOP time series (and a zoom-in) of the triple-epoch, two-satellite geometry-based model of the GLONASS satellites R21–R26 for the period UTC [04:47:00-08:10:00] of DOY 21 in 2016. The second row of Fig. 16 shows in the left column the unconstrained DD ambiguity float and fixed time series, *a*ˆ − *a* (in gray) and *a*ˇ − *a* (in green and red), and in the right column the corresponding time series of the unconstrained ambiguity standard deviation. Similar time series are also shown in the third to bottom row of Fig. 16, but now as a result of imposing a weighted height constraint with increasing weight.

The results in the third row show that a soft height constraint of only *σ* _{ h } = 2 m already has a significant impact on ambiguity resolution at the time instances for which the PDOPs are large. At these instances, the formal float ambiguity standard deviation has become much smaller, the variability in the float time series has reduced dramatically, and the ambiguity fixed solutions are now all correct. When we further increase the weight of the height-constraint, the results of the fourth to sixth row of Fig. 16 show that the ambiguity resolution improvements flow over to neighboring time instances such that finally in case of the bottom row now almost all of the 5000 ambiguity fixed solutions are correct.

## Summary and conclusions

We provided an initial assessment of GLONASS CDMA L3 double-differenced integer ambiguity resolution and corresponding positioning performance. Our analyses are based on GLONASS L3 data from the satellite pair R21–R26 and on GPS L1 data from the satellite pair G21–G29. We studied the noise characteristics (carrier-to-noise density, measurement precision), the integer ambiguity resolution performance (success rates and distribution of the ambiguity residuals) and the corresponding ambiguity float and ambiguity fixed positioning performance. The results show that the GLONASS data have a significantly lower noise level than that of GPS, particularly in case of the code data. This difference is not only seen in the noise levels but also in their onward propagation to ambiguity time series and ambiguity residuals distribution. We also compared all our empirical results with their formal counterparts, thereby showing the consistency between data and models. The four different versions of the two-satellite model that were applied are as following: the geometry-free model, the geometry-based model, the height-constrained geometry-based model, and the geometry-fixed model. Finally, we demonstrated that PDOP and ADOP characteristics can be quite distinct and that one therefore should not confuse a poor PDOP with poor ambiguity resolution capabilities.

## Notes

### Acknowledgments

Part of this work has been done in the context of the Positioning Program Project 1.19 “Multi-GNSS PPP-RTK Network” of the Cooperative Research Centre for Spatial Information (CRC-SI). The second author is the recipient of an Australian Research Council (ARC) Federation Fellowship (Project Number FF0883188).

## References

- Euler HJ, Goad CC (1991) On optimal filtering of GPS dual frequency observations without using orbit information. Bulletin Geodesique 65(2):130–143CrossRefGoogle Scholar
- GPS World (2015) Final GLONASS-M satellite passes tests. Available from: http://gpsworld.com/final-glonass-m-satellite-passes-tests/. Accessed 2 Feb, 2016
- GPSD (2013) Navstar GPS space segment/navigation user segment interface, Revision F (IS-GPS-200H:24-Sep-2013), global positioning system directorateGoogle Scholar
- Hofmann-Wellenhof B, Lichtenegger H, Collins J (2013) Global positioning system: theory and practice. Springer Science & Business MediaGoogle Scholar
- IAC (2016) GLONASS constellation status. Available from: https://www.glonass-iac.ru/en/GLONASS/, accessed 2 February 2016
- ICD-GLONASS (2008) Global Navigation Satellite System GLONASS Interface Control Document, version 5.1, MoscowGoogle Scholar
- Karutin S (2012) GLONASS signals and augmentations. In: Proceeding of ION GNSS 2012, Institute of Navigation, Nashville, TN, 17–21 September, pp 3878–3911Google Scholar
- Leick A, Rapoport L, Tatarnikov D (2015) GPS satellite surveying. Wiley, New YorkCrossRefGoogle Scholar
- Montenbruck O, Schmid R, Mercier F, Steigenberger P, Noll C, Fatkulin R, Kogure S, Ganeshan AS (2015) GNSS satellite geometry and attitude models. Adv Space Res 56(6):1015–1029CrossRefGoogle Scholar
- Nadarajah N, Khodabandeh A, Teunissen PJG (2015) Assessing the IRNSS L5-signal in combination with GPS, Galileo, and QZSS L5/E5a-signals for positioning and navigation. GPS Solutions 20(2):289–297. doi: 10.1007/s10291-015-0450-8 CrossRefGoogle Scholar
- Oleynik E (2012) GLONASS Status and Modernization. United Nations/Latvia Workshop on the Applications of Global Navigation Satellite Systems, RigaGoogle Scholar
- Reussner N, Wanninger L (2011) GLONASS interfrequency biases and their effects on RTK and PPP carrier-phase ambiguity resolution. In: Proceedings of ION GNSS 2011, Institute of Navigation, Portland, OR, 20–23 September, pp 712–716Google Scholar
- Takac F (2009) GLONASS inter-frequency biases and ambiguity resolution. Inside GNSS 4(2):24–28Google Scholar
- Teunissen PJG (1990) GPS op afstand bekeken In: een halve eeuw in de goede richting. Lustrumboek Snellius 1985-1990, DUM Delft pp 215–233Google Scholar
- Teunissen PJG (1997) A canonical theory for short GPS baselines. Part I: The baseline precision. Journal of Geodesy 71(6):320–336CrossRefGoogle Scholar
- Teunissen PJG (1998) Success probability of integer GPS ambiguity rounding and bootstrapping. J Geodesy 72(10):606–612CrossRefGoogle Scholar
- Teunissen PJG (2002) The parameter distributions of the integer GPS model. J Geodesy 76(1):41–48CrossRefGoogle Scholar
- Teunissen PJG, Amiri-Simkooei AR (2008) Least-squares variance component estimation. J Geodesy 82(2):65–82CrossRefGoogle Scholar
- Teunissen PJG, Odolinski R, Odijk D (2014) Instantaneous BeiDou + GPS RTK positioning with high cut-off elevation angles. J Geodesy 88(4):335–350CrossRefGoogle Scholar
- Thoelert S, Erker S, Furthner J, Meurer M, Gao GX, Heng L, Walter T, Enge P (2011) First signal in space analysis of GLONASS K-1. In: Proceedings of ITM 2011, Institute of Navigation, Portland, OR, 19–23 September, pp. 3076–3082Google Scholar
- Urlichich Y, Subbotin V, Stupak G, Dvorkin V, Povaliaev A, Karutin S (2010) GLONASS Developing Strategy. In: Proceedings of the 23rd ITM 2010, ION, pp 1566–1571Google Scholar
- Urlichich Y, Subbotin V, Stupak G, Dvorkin V, Povaliaev A, Karutin S (2011) A new data processing strategy for combined GPS/GLONASS carrier phase-based positioning. In: Proceedings of ION GNSS 2011, Institute of Navigation, Portland, OR, 20-23 September, pp 3125–3128Google Scholar
- Verhagen S, Teunissen P (2013) The ratio test for future GNSS ambiguity resolution. GPS Solutions 17(4):535–548CrossRefGoogle Scholar
- Wanninger L (2009) Carrier-phase inter-frequency biases of GLONASS receivers. J Geodesy 86(2):139–148CrossRefGoogle Scholar
- Yamada Y, Takasu T, Kubo N, Yasuda A (2010) Evaluation and calibration of receiver inter- channel biases for RTK-GPS/GLONASS. In: Proceedings of ION GNSS 2010, Institute of Navigation, Portland, OR, 21–24 September, pp 1580–1587Google Scholar

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