Submitted:
02 July 2024
Posted:
02 July 2024
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Abstract
Keywords:
1. Introduction
2. Mathematical Model of Long-Distance RTK
3. Experimental Design


4. Numerical Results
4.1. Overview of the Experimental Results
4.1.1. Minimum Required Time to Fix Ambiguity
4.1.2. Maximum R-Ratio in One Minute and One Hour
4.1.3. Convergence Time
4.1.3. Positioning Accuracy
4.2. Ambiguity Validation with the Theoretical Success Rate of Ambiguity Resolution
4.3. Ambiguity Validation with R-Ratio Test
| threshold | dual-frequency | multi-frequency | ||
| case count | proportion (%) | case count | proportion (%) | |
| 1.3 | 137 | 44.6 | 142 | 46.3 |
| 1.4 | 128 | 41.7 | 141 | 45.9 |
| 1.5 | 124 | 40.4 | 135 | 44.0 |
| 1.6 | 122 | 39.7 | 132 | 43.0 |
| 1.7 | 117 | 38.1 | 123 | 40.1 |
| 1.8 | 114 | 37.1 | 123 | 40.1 |
| 1.9 | 111 | 36.2 | 115 | 37.5 |
| 2.0 | 107 | 34.9 | 108 | 35.2 |
5. New Ambiguity Resolution Validation Method
6. Conclusions
- ➢
- The six theoretical success rate bounds currently in use are either excessively large or small compared to the actual value, rendering them impractical for long-distance RTK applications.
- ➢
- The R-ratio test proves to be generally reliable when the threshold is set above 1.7, provided that there is an adequate duration of observations (at least one minute) and a sufficient number of visible satellites (more than 10).
- ➢
- The likelihood of successfully resolving ambiguities using the R-ratio test does not exceed 50%. Furthermore, if a resolution is not achieved in 20 minutes, merely extending the observation time is typically ineffective.
- ➢
- In spite of different time required to exceed various R-ratio thresholds, the success rates for dual- and multi-frequency are quite comparable.
Acknowledgment
Appendix A Detailed Information of Experimental Cases













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| Type | Processing strategy |
| Code noise standard deviation | 0.3m |
| Phase noise standard deviation | 0.003m |
| Weighting scheme | Elevation dependent |
| Frequency | Dual and multiple |
| Positioning mode | Static and kinematic |
| Data interval | 1s |
| Ionosphere correction | Estimate TEC |
| Elevation mask | 15° |
| Satellite ephemeris/clock | Real-time precise Ephemeris |
| Tropospheric dry delay | Model correction |
| Tropospheric wet delay | Estimate ZTD |
| Receiver antenna phase center bias | IGS_14.atx |
| Parameter estimation method | Kalman filtering |
| Solid earth tide correction | Model correction |
| Relative correction | Model correction |
| Wind-up correction | Model correction |
| Ambiguity resolution | Float and integer |
| Outlier detection and rejection | Yes |
| Satellites with single frequency observation | Excluded |
| frequency | threshold | case No. | duration (s) | satellite number |
| dual | 1.3 | 46 | 31 | 14 |
| 93 | 1 | 7 | ||
| 96 | 2 | 8 | ||
| 125 | 1539 | 7 | ||
| 252 | 505 | 8 | ||
| 287 | 2 | 12 | ||
| 1.4 | 46 | 36 | 14 | |
| 96 | 3 | 8 | ||
| 252 | 528 | 8 | ||
| 287 | 28 | 12 | ||
| 1.5 | 96 | 3 | 8 | |
| 252 | 567 | 8 | ||
| 1.6 | 252 | 595 | 8 | |
| multiple | 1.3 | 33 | 4 | 11 |
| 143 | 69 | 11 | ||
| 244 | 1860 | 5 | ||
| 253 | 4 | 11 |
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