IP Library Granted Patent US 8,072,377
Granted Patent B2
US 8,072,377 · App. 12/294,839 · Granted Dec 6, 2011

Method of managing additional filters in a satellite navigaiton system

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Quick Facts
Patent No.
US 8,072,377
App. No.
12/294,839
Granted
Dec 6, 2011
Kind
B2
Abstract

A method of managing additional filters in a navigation system fitted to a vehicle, the system acting, during a journey of the vehicle, to deliver at least one position of the vehicle by using a main filter for merging data coming from a constellation of visible satellites present above a vehicle horizon, each additional filter excluding data coming from one of the satellites in order to obtain a corrected position in the event of failure of the excluded satellite. The steps including from a position of the vehicle, determining a theoretical constellation of satellites present above the horizon; and for each satellite present in the theoretical constellation, creating and maintaining an additional filter excluding that satellite.

Claims (7)

1. A method of managing additional filters in a navigation system fitted to a vehicle, the system acting, during a journey of the vehicle, to deliver at least one position of the vehicle by using a main filter for merging data coming from a constellation of visible satellites present above a vehicle horizon, each additional filter excluding data coming from one of the satellites in order to obtain a corrected position in the event of failure of the excluded satellite, the method being comprising the steps of:

from a position of the vehicle, determining a theoretical constellation of satellites present above the horizon; and

for each satellite present in the theoretical constellation, creating and maintaining an additional filter excluding the satellite.

2. A method according to claim 1 , including the step, for each satellite present in the theoretical constellation, of including said satellites in the existing additional filters as soon as said satellite appears in the theoretical constellation.

3. A method according to claim 1 , in which the position used for determining the theoretical constellation is provided by the main filter.

4. A method according to claim 1 , in which, when a satellite disappears from the theoretical constellation at some instant on a journey, the method comprises the step of waiting for a predetermined duration before eliminating the additional filter excluding said satellite.

5. A method according to claim 4 , in which, when a satellite that has disappeared reappears in the theoretical constellation, the method includes the step of waiting for the filters to converge prior to creating an additional filter excluding said satellite and reincorporating said satellite in the existing additional filters.

Assignments (1)
CHANGE OF NAME Recorded May 6, 2018
From: SAGEM DÉFENSE SÉCURITÉ
To: SAFRAN ELECTRONICS & DEFENSE
Reel/Frame 046082/0606 →