DEVICE FOR PROCESSING NAVIGATION DATA OF A SATELLITE NAVIGATION SYSTEM FOR DELIVERING INTEGRITY AREA MAPS

• US 20090234581A1
• Filed: 11/06/2006
• Published: 09/17/2009
• Est. Priority Date: 11/07/2005
• Status: Abandoned Application

• Current Assignee: Alcatel-Lucent SA (Nokia Corporation)
• Original Assignee: Alcatel-Lucent SA (Nokia Corporation)
• Inventors: Flament, Didier, Levy, Jean Christophe
• Application Number:
  US12/092,858
• Publication Number:
  US 20090234581A1
• Time in Patent Office: Days
• US Class Current: 701/214
• CPC Class Codes: G01S 19/08 providing integrity information, e.g. health of satellites or quality of ephemeris data

Abstract

A device (PD) is dedicated to processing navigation data related to satellites in a satellite navigation system in orbit around a heavenly body. This device (PD) comprises processing means (PM) tasked with comparing integrity data (ID), which represents reliability values of corrections to errors in the orbital positioning and/or synchronization of the satellites, to at least one selected set of N selected threshold values, N being an integer greater than or equal to one, in such a way as to deliver at least one group of cartographic data representative of at most N+1 geographic areas defined with respect to said heavenly body and in which said integrity data is less than the N threshold values of the selected set, greater than the N threshold values of the selected set Si, or between two threshold values of the selected set.

Claims

1. A device (PD) for processing navigation data related to satellites in a satellite navigation system orbiting around a heavenly body, characterized in that it comprises processing means (PM) configured to compare integrity data (ID) representative of reliability values for corrections of errors in the orbital positioning and/or synchronization of said satellites, to at least one selected set of N selected threshold values, N being an integer greater than or equal to one, in such a way as to deliver at least one group of cartographic data representative of at most N+1 geographic areas defined with respect to said heavenly body and in which said integrity data is less than said N threshold values of said selected set, greater than said N threshold values of said selected set Si, or between two threshold values of said selected set.

2. A device according to claim 1, characterized in that said processing means (PM) are configured to compare integrity data (ID) to at least two selected sets (Si) of Ni selected threshold values, Ni being integers greater than or equal to one, in such a way as to deliver at least two groups (Gi) of cartographic data that each represent at most Ni+1 geographic areas (Aj) defined with respect to said heavenly body and in which said integrity data is less than said Ni threshold values of the selected set (Si), greater than said Ni threshold values of the selected set (Si), or between two threshold values of the selected set (Si).

3. A device according to claim 1, characterized in that said threshold values are representative of integrity margins with respect to a reference value, which is itself defined with respect to a user of said satellite navigation system having the worst reliability value of corrections of errors in satellite orbital positioning and/or synchronization.

4. A device according to claim 1, characterized in that said processing means (PM) are configured to determine each group of cartographic data (G1) from the most recent integrity data (ID), in such a way as to enable almost real-time functioning.

5. A device according to claim 1, characterized in that it comprises calculation means (CM;

CSM) configured to determine said integrity data (ID) from at least i) first data (D1) representing information contained within navigation messages broadcast by said satellites, ii) second data (D2) representing estimated positions for said satellites, and iii) third data (D3) representing estimated time differences between the clocks of said satellites compared to a master clock.

6. A device according to claim 5, characterized in that said calculation means (CM;

CSM) are configured to determine said integrity data (ID) from the first (D1), second (D2), and third (D3) reference data, and from fourth data (D4) representing a selected architecture for said satellite navigation system, in such a way as to enable a predicted functioning and/or to determine the influence of breakdowns and/or maintenance activity on devices in said satellite navigation system.

7. A device according to claim 5, characterized in that said processing means (PM) are incorporated into said calculation means (CM).

8. A device according to claim 1, characterized in that comprises display means (DM) for drawing geographic areas (Aj), defined by said determined cartographic data, with respect to corresponding regions in the surface of said heavenly body.

9. The usage of the navigation data processing device (PD) according to claim 1, for integrity services of satellite navigation systems selected from a group comprising at least GALILEO, GPS, EGNOS and WAAS, as well as their variants and equivalents.