2019
DOI: 10.1049/iet-rsn.2019.0084
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CS detection and correction techniques for RTK positioning using single‐frequency GNSS receivers: trends and comparison

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Cited by 3 publications
(6 citation statements)
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“…The carrier phase is represented by a featureless cosine wave. When a weekly jump occurs, the whole-week counter no longer counts, creating ambiguity that affects the actual value of the carrier phase (Karaim et al 2014;Zainab Farooq et al 2019). In addition, LT4A satellites receive most of their navigation signals from the other side of the Earth, which propagate over long distances and may be obscured by the Earth, making them more prone to signal interruptions.…”
Section: Data Quality Analysis Cycle Slip Detection and Measurement N...mentioning
confidence: 99%
“…The carrier phase is represented by a featureless cosine wave. When a weekly jump occurs, the whole-week counter no longer counts, creating ambiguity that affects the actual value of the carrier phase (Karaim et al 2014;Zainab Farooq et al 2019). In addition, LT4A satellites receive most of their navigation signals from the other side of the Earth, which propagate over long distances and may be obscured by the Earth, making them more prone to signal interruptions.…”
Section: Data Quality Analysis Cycle Slip Detection and Measurement N...mentioning
confidence: 99%
“…As seen, the minimum and maximum number of GPS satellites varies from 6 to 11 over the course of an entire day. CS detection takes place once ambiguities are resolved, and, corresponding to the satellite availability, the measurement redundancy varies as (7,9,11,13,15,17). From the procedure to assess the reliability of the position fix given in Table 1, the thresholds for detection and identification stages are determined.…”
Section: Choice Of Parametersmentioning
confidence: 99%
“…As soon as the measurement joins the LS adjustment, the MDB reduces for all satellites. The number of visible satellites remains constant till epoch 658, and it changes to (8,9,7,9) for epoch (659,660,661,662); hence the peak is observed at epoch 661. This is clear from Figure 10, which shows the number of visible satellites for the rover for Dataset 2.…”
Section: Analysis Of External Reliabilitymentioning
confidence: 99%
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