| 摘要 |
Method for determining a confidence indicator relating to the trajectory followed by a moving objectThe method consists in estimating the position of the moving object on the basis of the reception of navigation signals emitted by a constellation of satellites, the navigation signals being modulated by a code and the receiver (4) comprising a local replica of the code. The determination of the confidence indicator consists in estimating a speed of displacement of the receiver (4) over an identified trajectory segment (R1, R2), deducing therefrom a Doppler delay function corresponding to the motion of the receiver (4), in correcting the auto-correlation function of the GNSS navigation signal received from each satellite of the constellation by means of the delay function, in comparing the corrected auto-correlation function (Ct, Cf) with a theoretical auto-correlation function by applying a quadratic criterion corresponding to the confidence indicator.Fig. 4 |
