Detection and correction of carrier phase inconsistency during the tracking of a radio navigation signal

1. A method for tracking the carrier phase of a signal received from a satellite by a mobile carrier device by means of a carrier phase tracking loop, said signal being acquired by a navigation system of the mobile carrier device which comprises a localization receiver ( 10 ) by radio navigation, a local oscillator and an autonomous unit ( 20 ), the receiver ( 10 ) being adapted for acquiring and tracking the phase of the carrier of the signal from the satellite, the method comprising the following steps:

generating, by the local oscillator, a replica signal of the received signal,

determining (E 1 ) a closed-loop control error of the carrier phase loop from the received signal and from a local signal, wherein said closed-loop control error is determined between two sampling instants and is represented by a first phase deviation;

determining (E 2 ) an acceleration variation of the mobile carrier device between the two sampling instants by means of the autonomous unit ( 20 );

projecting (E 3 ) the acceleration variation on a satellite-receiver view axis for obtaining a second phase deviation;

comparing (E 4 ) the first and second deviations in order to detect an error on the measurement of the carrier phase tracked by said carrier phase loop, said comparison including determining an inconsistency term representing an inconsistency of the first phase deviation with the second phase deviation;

updating the replica signal using one of the first and second phase deviations, depending on a value of the inconsistency term;

integrating the inconsistency term over a sliding period so as to produce an integrated term, then

comparing the integrated term with a threshold, and

updating the replica signal using the second phase deviation if the integrated term is greater than the threshold.

2. The method according to claim 1 , wherein the acceleration variation of the mobile carrier device is determined by means of an inertial unit ( 21 ) of the navigation system.

3. The method according to claim 1 , comprising a step for producing integrated dopplers from the generated replica signal, and a step (E 6 ) for determining a navigation solution from said integrated dopplers.

4. The method according to claim 3 , wherein if the inconsistency term is greater than the threshold, the method comprises a step (E 5 ′) for correcting the integrated dopplers, the correction consisting of adding a term k·λ/2 to said integrated dopplers wherein k is an integer such that the absolute value of the integrated inconsistency term is less than the threshold, and wherein λ is the wavelength associated with the carrier frequency of the received signal.

5. The method according to claim 4 , comprising a step (E 6 ) for determining a navigation solution from the corrected integrated dopplers.

6. The method according to claim 1 , wherein the threshold is λ/4, wherein λ is a wavelength associated with the carrier frequency of the received signal.