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

Abstract

The invention relates to a method for tracking the carrier phase of a signal received from a satellite by a carrier using a carrier loop of the carrier phase, said signal being acquired by a navigation system of the carrier, said navigation system including a receiver for location by radio navigation, and a self-contained unit, wherein the receiver is suitable for acquiring and tracking the phase of the carrier of the signal from the satellite.

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, an inertial unit, a local oscillator and a 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 the 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 ), by the inertial unit, 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 consisting of determining an inconsistency term representing an inconsistency of the first deviation with the second deviation; and   producing integrated dopplers from the replica signal;   correcting the integrated dopplers or not depending on a value of the inconsistency term; and   determining a navigation solution from said integrated dopplers.   
     
     
         2 . The method according to  claim 1 , further comprising integrating the inconsistency term over a sliding period so as to produce an integrated inconsistency term, comparing the integrated inconsistency term with a threshold, and wherein correcting the integrated dopplers is carried out only if the integrated inconsistency term is greater than the threshold. 
     
     
         3 . The method according to  claim 2 , wherein correcting the integrated dopplers comprises 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. 
     
     
         4 . 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.