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# A sequential and partial ambiguity resolution strategy for improving the initialization performance of medium-baseline relative positioning

- Shoujian Zhang
^{1}, - Lei Zhao
^{1}Email author, - Xintan Li
^{1}and - Bing Cheng
^{1}

**Received:**30 November 2015**Accepted:**11 February 2016**Published:**24 February 2016

The Erratum to this article has been published in Earth, Planets and Space 2016 68:122

## Abstract

Ionosphere products that are relatively precise are available thanks to the efforts of the International GNSS Service (IGS), and it might be possible to obtain a high success rate for the fixed integer ambiguities for medium- or longer-baseline ambiguity resolution (AR) using the ionosphere products as a priori information constraints. In this study, we used the IGS precise ionosphere products as a priori information before forming double-difference (DD) measurement equations using only original observables in a mid-range relative positioning and estimated the ionosphere residuals explicitly after DD. Furthermore, we proposed a sequential and partial ambiguity resolution (SPAR) strategy under the integer least square condition to realize fast and reliable AR. To demonstrate our proposed strategy, we randomly selected seven baselines ranging from 30 to 111 km and undertook positioning in a post-processing mode using real GPS dual-frequency data. According to the results, the SPAR strategy has a faster convergence process compared with batch AR. For instance, the convergence time with >90 % cumulative frequency percentage (probability) for 30, 40, 56, 66, 80, 95, and 111 km baselines was advanced by 55, 50, >75, 85, >110, 65, and >35 epochs, respectively, with a 30-s sample interval. By considering ionospheric correction before DD, we found further improvement in the initialization performance with the use of the SPAR strategy.

## Keywords

- GPS
- Medium-range relative positioning
- Sequential and partial ambiguity resolution
- Convergence time
- Precise ionosphere consideration

## Background

Real-time kinematic (RTK) positioning, which is known for its precision, has been used widely as positioning technology in many fields of engineering and science. The situation is relatively simple for short-baseline (<10 km) RTK under 10 km. The double difference (DD) of satellite observables between rover and base stations mostly eliminates atmospheric delay errors, and the ambiguity resolution process usually employs the least squares ambiguity decorrelation adjustment (LAMBDA) method (Teunissen 1995) that is efficient in delivering reliable fixed integer ambiguities. After comparison of four ambiguity resolution (AR) methods: LAMBDA, geometry-free models for three-carrier ambiguity resolution (TCAR) (Forssell et al. 1997; Vollath et al. 1998), geometry-based TCAR (Teunissen et al. 2002; Feng and Li 2008, 2009), and GIF-TCAR (TCAR based on a geometry-free and ionosphere-free combination) (Wang and Rothacher 2013), Zhang and He (2015) highlighted that the LAMBDA method is optimal in both short- and medium-baseline (10–100 km) cases. Li et al. (2015) developed a reliable AR strategy that efficiently resolves ambiguities sequentially under the integer least square (ILS) condition (Teunissen 1995) for the case of short-range RTK. However, for medium or long baselines (>100 km), large ionospheric delay residuals remain after DD. The conventional method for overcoming this problem is to use ionosphere-free linear combinations (LCs) of the original observables and to accommodate AR using a sequential rounding process of wide-lane (WL) and narrow-lane (NL) ambiguities (Takasu and Yasuda 2010). Unfortunately, the LCs of the original measurements amplify the observable noise and lead to the inevitable addition of positioning error. Therefore, for longer-baseline RTK, it is better to use original observables to limit the propagation of measurement noise. Li et al. (2014) developed efficient procedures for improved float solutions and ambiguity fixing over long-baseline RTK without using ionosphere-free measurements, although the WL AR process remained a rounding process. In fact, simple rounding schemes for WL and NL ambiguities cannot ensure high reliability of fixed integer ambiguities. Teunissen (1999) provided proof that an ILS estimator of the carrier-phase ambiguities is best for maximizing the probability of correct integer estimation. Hence, the AR process should be performed under an ILS condition to ensure the reliability of the fixed integer ambiguities. Nevertheless, validation of the batch AR mode by the LAMBDA method might still fail because of biases in some estimated float ambiguities (Takasu and Yasuda 2010), especially in the case of long baselines. Therefore, the partial AR technique was developed, which resolves a subset of the ambiguities to overcome this condition (Teunissen et al. 1999).

Ionosphere products that are relatively precise are available owing to the efforts of the International GNSS Service (IGS), and it might be possible to obtain a high success rate for the fixed integer ambiguities for medium- or longer-baseline AR using the ionosphere products as a priori information constraints. Considering the problems mentioned above, we used the IGS precise ionosphere products as a priori information before forming the DD measurement equations using only original observables in a mid-range RTK and estimated the ionosphere residuals explicitly after DD. Furthermore, we propose a sequential and partial ambiguity resolution (SPAR) strategy under the ILS condition to realize fast and reliable AR. In the following, we offer a detailed description of the proposed SPAR strategy. We compare the initialization performances of the SPAR and batch AR strategies and investigate the influence of a priori ionosphere information on the efficiency of the SPAR strategy.

## Sequential and partial ambiguity resolution (SPAR) strategy

For medium- or longer-baseline RTK, because of the biases in some float ambiguities, batch AR by the LAMBDA method might still not pass the validation step. Therefore, the partial AR technique, which resolves a subset of the ambiguities, is implemented to obtain a high success rate (Teunissen et al. 1999; Zinas et al. 2013; Wang and Feng 2013). The success rate and ratio test are different indicators with which to assess the reliability of the fixed ambiguities (Euler and Schaffrin 1990; Teunissen 1998; Hassibi and Boyd 1998; Teunissen and Verhagen 2008; Wang and Feng 2013). The selection of the ambiguity subset, however, is not unique, and it could be based on the float ambiguity variance, elevation angle, and LCs (Mowlam and Collier 2004). Parkins (2011) described an algorithm for resolving a subset of ambiguities with validation from previous epochs in single-epoch RTK positioning (Wang and Feng 2013). Takasu and Yasuda (2010) employed a very simple criterion involving the satellite elevation angle for long-baseline RTK. Li et al. (2015) chose a subset that comprised all the extra-WL or WL ambiguities in a multi-frequency case, because the extra-WL or WL ambiguities suffer relatively low effects from noise and they can be easily resolved reliably. They also indicated the possibility of resolving the ambiguities sequentially when the corresponding success rate is very close to the batch AR mode and they proposed a multi-carrier fast partial ambiguity resolution strategy that they tested with short baselines.

For longer baselines, WL ambiguity resolution will be affected inevitably by the biases in the measurements. Thus, a subset that contains all the WL float ambiguities without distinction might not be the best choice, and consequently, there is a need to optimize the subset. Here, we propose an optimization method that works in an iterative scheme to fix the float ambiguities with low variance. The ratio test (Euler and Schaffrin 1990) is used here for ambiguity validation. The ratio test in fact calculates the closeness of the float ambiguity \(\hat{B}\) to its nearest integer \(\bar{B}\) compared to the second nearest integer \(\bar{B}^{{\prime }}\), and it reads as:

After transformation, the ambiguity types are \(\hat{B}_{\text{WL}}\) and \(\hat{B}_{1}\) instead of the previous \(\hat{B}_{1}\) and \(\hat{B}_{2}\). This transformation is fundamental in our proposed strategy for introducing the WL ambiguity type.

*Step 1* Resolve the WL ambiguities first using the LAMBDA method; the validation technique used here is the popular ratio test with a critical threshold value of 3. Actually, this is the partial AR idea that resolves a subset of the entire float ambiguities. As the biases in the measurements have the least effect on the resolution of WL ambiguities, a subset that comprises all the WL float ambiguities is reasonable (Li et al. 2015). However, for a longer baseline, WL AR could be disturbed by measurement noise, meaning that it is not possible to select all the float WL ambiguities without distinction. When the validation test fails, our optimizing method deletes the float WL ambiguity with the maximum variance (which is considered the one disturbing the WL AR process) from \(\hat{B}_{\text{WL}}\), and then repeats the resolution and test until the validation test is passed, which provides the integer solution \(\bar{B}_{\text{WL}}\).

*Step 2*Update \(\hat{X}\), \(\hat{B}_{1}\), and their variance–covariance matrix together with the fixed solution \(\bar{B}_{\text{WL}}\). In this step, the remaining float ambiguities on the L1 frequency and other parameters are not distinguished. The formula for the update is as below (Teunissen 1995):

*Step 3* Resolve the remaining ambiguities on the L1 frequency using the LAMBDA method and repeat the entire process from Step 1 to obtain the remaining integer ambiguities \(\bar{B}_{1}\).

*Step 4*Obtain the fixed solution of the remaining unknowns using the formulas below:

*Step 5* Change back. Conduct the inverse transformation of (3).

The fundamental concepts of this strategy involve resolving the WL ambiguities and the ambiguities on the L1 frequency sequentially, and optimizing the selected ambiguity subset circularly based on the estimated ambiguity variance, as long as the validation test fails.

## Experiment demonstration

Information of selected baselines in EUREF

Approximate length (km) | Base station ID | Rover station ID |
---|---|---|

31 | EIJS | WARE |

40 | DOUR | REDU |

56 | GOPE | CTAB |

66 | CRAK | MARJ |

80 | BRUX | DOUR |

95 | CLIB | CPAR |

111 | CPAR | KUNZ |

Comparison of initialization performance for the two strategies and comparison of initialization performance for two ionosphere correction models applied in SPAR strategy

Baseline length (km) | Convergence time (epoch) with cumulative frequency percentage ≥90 % | Convergence time (epoch) with cumulative frequency percentage ≥90 % for SPAR strategy | ||
---|---|---|---|---|

Batch AR | SPAR | Broadcast model | IONEX TEC model | |

31 | 110 | 55 | 55 | 55 |

40 | 130 | 80 | 60 | 60 |

56 | >240 | 165 | 175 | 160 |

66 | 230 | 145 | 110 | 110 |

80 | >240 | 130 | 75 | 75 |

95 | 130 | 65 | 60 | 60 |

111 | >240 | 205 | 190 | 170 |

## Conclusions

In this work, we proposed a SPAR strategy for a dual-frequency case with estimation of atmosphere residuals for medium- and longer-baseline relative positioning. The fundamental concepts of this strategy involve resolving the WL ambiguities and the ambiguities on the L1 frequency sequentially, and optimizing the selected ambiguity subset circularly based on the estimated ambiguity variance, as long as the validation test fails. Tested using real GPS dual-frequency data of seven mid-range baselines in a post-processing mode, our strategy was shown always to be faster than the batch AR mode. The convergence time with >90 % cumulative frequency percentage in our samples for randomly chosen 30, 40, 56, 66, 80, 95, and 111 km baselines was advanced by 55, 50, >75, 85, >110, 65, and >35 epochs, respectively, with a 30-s sample interval. We undertook ionosphere corrections for each baseline before considering the DD of the satellite observables with the intention of reducing the ionospheric delay errors further. The results showed that after considering ionosphere correction, our proposed strategy worked faster; however, differences between the ionosphere models applied with our strategy were not obvious, which means it is acceptable to use the broadcast model with our SPAR strategy in such mid-range circumstances. Further investigation is necessary to do to test our proposed strategy in different positioning modes.

## Notes

## Declarations

### Authors’ contributions

All the authors contributed to the design of the proposed algorithm. SZ came up with the idea of partial optimization in the algorithm. XL and BC participated in the experimental analysis. LZ carried out the experiments and drafted the manuscript. All authors read and approved the final manuscript.

### Acknowledgements

This work is supported by Grants from the National Natural Science Foundation of China (Nos. 41304027 and 41274033) and the National Basic Research Program of China (973 Program) (Grant No. 2013CB733301). The authors are also very grateful to the open source software RTKLIB and EPN for providing GPS dual-frequency data.

### Competing interests

The authors declare that they have no competing interests.

**Open Access**This article is distributed under the terms of the Creative Commons Attribution 4.0 International License (http://creativecommons.org/licenses/by/4.0/), which permits unrestricted use, distribution, and reproduction in any medium, provided you give appropriate credit to the original author(s) and the source, provide a link to the Creative Commons license, and indicate if changes were made.

## Authors’ Affiliations

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