Method of monitoring the integrity of radio-navigation stations in a satellite based augmentation system

Patent metadata

Field	Value
Publication number	US-9316739-B2
Application number	US-201313954642-A
Country	US
Kind code	B2
Filing date	Jul 30, 2013
Priority date	Aug 3, 2012
Publication date	Apr 19, 2016
Grant date	Apr 19, 2016

Abstract

A method of monitoring the integrity of stations for observing radio-navigation signals in a satellite based augmentation system SBAS comprises: defining a geographical zone comprising a plurality of observation stations, calculating, for each observation station of the zone and for each line of sight between the station and a satellite, the discrepancy between the theoretical pseudo-distance D and the measured pseudo-distance D′, calculating the average m of the discrepancies D−D′ over the zone for at least one satellite in visibility of the zone, validating the integrity of at least one observation station of the zone if the discrepancy, for the station and for at least one line of sight between the station and a satellite, is less than or equal to the average that is multiplied by a predetermined exclusion threshold, and excluding this observation station in the converse case.

First claim

The invention claimed is:

1. A method for monitoring the integrity of stations for observing radio-navigation signals in a satellite based augmentation system SBAS comprising:
defining at least one geographical zone comprising a plurality of observation stations,
calculating, for each observation station of the said zone and for each line of sight between the said station and a satellite, the discrepancy between a theoretical pseudo-distance D and a measured pseudo-distance D′,
calculating the average m of the said discrepancies D−D′ over the said zone for at least one satellite in visibility of the said zone,
validating the integrity of at least one observation station of the said zone if the discrepancy between the theoretical pseudo-distance D and the measured pseudo-distance D′, for the said station and for at least one line of sight between the said station and a satellite, is less than or equal to the said average that is multiplied by a predetermined exclusion threshold, and excluding this observation station in the converse case.

2. The method for monitoring the integrity of stations for observing radio-navigation signals according to claim 1 , wherein the said average m is calculated over the set of the satellites in visibility of a said zone.

3. The method for monitoring the integrity of stations for observing radio-navigation signals according to claim 2 , wherein the integrity of the observation stations of the said zone is validated if all the discrepancies between theoretical pseudo-distance D and measured pseudo-distance D′ for all the lines of sight are less than or equal to the said average that is multiplied by a predetermined exclusion threshold.

4. The method for monitoring the integrity of stations for observing radio-navigation signals according to claim 1 , wherein the theoretical pseudo-distance D is calculated on the basis of the knowledge of the positions of the satellites and of the observation stations and the measured pseudo-distance D′ is calculated by the observation stations on the basis of the received radio-navigation signals.

5. The method for monitoring the integrity of stations for observing radio-navigation signals according to claim 1 , wherein the said zone has a fixed size.

6. The method for monitoring the integrity of stations for observing radio-navigation signals according to claim 1 , wherein the said zone is a circle of variable radius centred on a given observation station, termed the reference station.

7. The method for monitoring the integrity of stations for observing radio-navigation signals according to claim 6 , wherein the radius of the said zone is configured so that each zone comprises the same number N of stations.

8. The method for monitoring the integrity of stations for observing radio-navigation signals according to claim 1 , wherein, within a zone, only the integrity of the reference station is validated.

9. The method for monitoring the integrity of stations for observing radio-navigation signals according to claim 1 , in which the exclusion threshold is fixed or dependent on the maximum number of observation stations per zone to be excluded.

10. The method for monitoring the integrity of stations for observing radio-navigation signals according to claim 1 , wherein the exclusion threshold is configured so as to minimize the probability of false alarm and the probability of non-detection over the number of excluded observation stations.

11. The method for monitoring the integrity of stations for observing radio-navigation signals according to claim 1 , in which the said observation stations form part of a collaborative network of stations.

12. A monitoring and processing centre for satellite based augmentation system SBAS comprising means, including a processor, for monitoring the integrity of stations for observing radio-navigation signals, said means being configured for defining at least one geographical zone comprising a plurality of observation stations,
calculating, for each observation station of the said zone and for each line of sight between the said station and a satellite, the discrepancy between a theoretical pseudo-distance D and a measured pseudo-distance D′,
calculating the average m of the said discrepancies D−D′ over the said zone for at least one satellite in visibility of the said zone,
validating the integrity of at least one observation station of the said zone if the discrepancy between the theoretical pseudo-distance D and the measured pseudo-distance D′, for the said station and for at least one line of sight between the said station and a satellite, is less than or equal to the said average that is multiplied by a predetermined exclusion threshold, and excluding this observation station in the converse case.

13. A satellite based augmentation system SBAS comprising a plurality of observation stations whose integrity is not guaranteed and at least one monitoring and processing centre according to claim 12 .

Assignees

• Thales Sa

Inventors

• Bertin De La Hautiere Gonzague
• Dahman Nidhal

Classifications

• G01S19/07 Primary

  providing data for correcting measured positioning data, e.g. DGPS [differential GPS] or ionosphere corrections · CPC title

• G01S19/38 Primary

  Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system · CPC title

• G01S19/02

  Details of the space or ground control segments · CPC title