Abstract
An observational equation of the GPS carrier phase contains the pair station — satellite specific and epoch independent bias γ s r = ψs(t 0)−ψ r (t 0) +N s r , in which N s r is an integer ambiguity and ψ (t 0), ψr(t 0) are transmitter and receiver initial phases. Through sequential processing of phases we update in each epoch, among other unknowns, the γ s r estimates, provided specific minimal configurations of satellites, stations and already processed epochs are satisfied. All second differences of the phases, e.g. with respect to a given reference satellite and reference receiver, ∇Δγ s r =∇ΔN s r , should be then integers on each L1 and L2 band. These conditions can be solved for all N s r ’s (thus implying new γ s r -values) about current estimates of the γ s r ’s as soon as the integer values are found by means of a proper search procedure.
Cycle slips come into view as outliers of observations produced by rapid changes of particular γ s r values. In that case a new observation sequence is created, for which new γ-parameters are estimated, and then consequently constrained for ambiguities.
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© 1996 Springer-Verlag Berlin Heidelberg
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Pachelski, W. (1996). GPS Phases: Single Epoch Ambiguity and Slip Resolution. In: Beutler, G., Melbourne, W.G., Hein, G.W., Seeber, G. (eds) GPS Trends in Precise Terrestrial, Airborne, and Spaceborne Applications. International Association of Geodesy Symposia, vol 115. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-80133-4_48
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DOI: https://doi.org/10.1007/978-3-642-80133-4_48
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