Method for integrity monitoring in position determination

• US 5,910,789 A
• Filed: 08/28/1997
• Issued: 06/08/1999
• Est. Priority Date: 12/20/1994
• Status: Expired due to Term

• Current Assignee: GECO AS
• Original Assignee: GECO AS
• Inventors: Vigen, Erik
• Primary Examiner(s): Issing, Gregory C.
• Application Number:
  US08/849,257
• Time in Patent Office: 649 Days
• Field of Search: 342/357, 701/214, 701/215
• US Class Current: 342/357.45
• CPC Class Codes: G01S 19/08 providing integrity information, e.g. health of satellites or quality of ephemeris data
• CPC Class Codes: G01S 19/20 Integrity monitoring, fault detection or fault isolation of space segment
• CPC Class Codes: G01S 19/23 Testing, monitoring, correcting or calibrating of receiver elements
• CPC Class Codes: G01S 5/0036 of measured values, i.e. measurement on mobile and position calculation on base station
• CPC Class Codes: G01S 5/0063 of measured values, i.e. measurement on base station and position calculation on mobile

Abstract

In a method for integrity monitoring in position determination by means of the Global Positioning System (GPS), especially by means of differential GPS (DGPS) or multi-station DGPS, wherein there is employed a monitor station (M) with a first GPS receiver, provided at a location with a known geographical position, GPS-based position measurement results are transferred on a communication line from the monitor station (M) to a user location (F) the integrity of whose geographical position has to be monitored by means of a second GPS receiver provided at the location (F). A space vector between the location of the monitor station (M) and the location (F) is determined by means of the position measurement results for the location (F) and the monitor station (M), whereupon the degree of agreement is determined between the position for the location (F), the space vector and the known position of the monitor station (M), the degree of agreement being required to correspond to a maximum error in the position for the user location (F).

Claims

1. A method of integrity monitoring in position determination by means of Global Positioning System (GPS), wherein there is employed a monitor station (M) with a first GPS receiver, provided at a location with a known geographical position, and a user location (F) with a second GPS receiver, the integrity of whose geographical position has to be monitored,

characterised by transferring first GPS-based position measurement results obtained at the monitor station (M) on a communication line from the monitor station (M) to the user location (F);

determining a space vector between the location of the monitor station (M) and the user location (F) by means of second GPS-based position measurement results obtained at the user location (F) and said first GPS-based position measurement results obtained at the monitor station (M); and

determining the degree of agreement among a GPS-based position measurement of the user location (F), the space vector and the known position of the monitor station (M), the degree of agreement being compared against a maximum error in the position for the user location (F) against which protection is desired.

2. A method according to claim 1, characterized in that said degree of agreement is determined by means of solid geometric or geodetic calculations.

3. A method according to claim 2, characterized in that the position of the user location (F) is determined by means of GPS signals and differential correction signals transferred from one or more reference stations (R) in a known position or known positions.

4. A method according to claim 3, characterized in that the differential corrections from the reference station or reference stations (R) are received by a receiver provided for this purpose at the user location (F).

5. A method according to claim 4, characterized in that there is provided an additional GPS receiver at the user location (F), with an associated additional antenna, thus duplicating the GPS receiver equipment at the user location (F) in order to be able to eliminate the effect of equipment error.

6. A method according to claim 5, characterized in that the position of the additional GPS receiver is determined relative to the position of the second GPS receiver, the second and the additional GPS receivers'"'"' antennae being arranged in such a manner that they receive different interference conditions due to multiple-path propagation.

7. A method according to claim 6, characterized in that the distance between the antennae of the two GPS receivers at the user location (F) is selected in order to enable position errors which are due to multiple-path propagation of the GPS signals to be identified, a corresponding space vector being calculated between the additional GPS receiver and the second GPS receiver.

8. A method according to claim 1, wherein the position determination is performed by means of differential GPS, characterized in that any ionospheric refraction of the GPS signals is corrected by employing GPS receivers which work on two frequencies, both in the monitor station (M) and in the user location (F).

9. A method according to claim 1, wherein the position determination is performed by means of DGPS, characterized in that any ionospheric refraction of the GPS signals is identified by arranging the monitor station (M) and the reference station or reference stations (R) in respective arcs which intersect each other in such a manner that the user location (F) is located in the segment between the said circular arcs.

10. A method according to claim 1, wherein the position determination has to be performed in another datum than that to which GPS refers, characterized in that a datum transformation is verified by means of integrity monitoring, any error in the position thus also being determined in the second datum.