Fault detection and exclusion used in a global positioning system GPS receiver

• US 5,841,399 A
• Filed: 04/10/1997
• Issued: 11/24/1998
• Est. Priority Date: 06/28/1996
• Status: Expired due to Term

• Current Assignee: Alliedsignal Inc. (Honeywell International Inc.)
• Original Assignee: Alliedsignal Inc. (Honeywell International Inc.)
• Inventors: Yu, Jimmy Y.
• Primary Examiner(s): Blum, Theodore M.
• Application Number:
  US08/838,571
• Time in Patent Office: 593 Days
• Field of Search: 342/357, 701/213
• US Class Current: 342/357.29
• CPC Class Codes: G01S 19/20 Integrity monitoring, fault detection or fault isolation of space segment

Abstract

A fault exclusion (FE) system for a global positioning system (GPS) receiver which upon detection of a faulty satellite, for example, by a fault detection (FD) system, such as a receiver autonomous integrity monitoring (RAIM) system. The FE system computes the test statistics for all satellites and ranks the satellites in descending order of their test statistics. The FE system excludes data from the satellites one at a time starting with the satellites at the top of the list. Should a subsequent satellite anomaly be detected, the FE system excludes satellites based on the test statistics computed for the previous satellite anomaly condition. The FE system proceeds down the list until the fault detection condition is cleared or the list is exhausted without affecting the availability of the FD system.

Claims

1. A fault detection and exclusion system for detecting satellite anomalies in a global positioning system (GPS) and excluding the data from the satellite with the anomaly from the navigation solution, the system comprising:

means for detecting a first and a second satellite anomaly;

means for computing the test statistics for a predetermined number of satellites at least when said first satellite anomaly is detected; and

means for excluding data from one of the satellites, when said second satellite anomaly is detected, as a function of the test statistics calculated for said first satellite anomaly condition.

2. The fault detection and exclusion system as recited in claim 1, wherein said excluding means includes means for ranking the satellites in descending order as a function of the computed test statistic.

3. The fault detection and exclusion system as recited in claim 2, further including means for excluding satellites in order of descending test statistics until the satellite anomaly is no longer detected or the list is exhausted.

4. The fault detection and exclusion system as recited in claim 2, further including means for checking for satellite anomalies after each of said satellites is excluded.

5. The fault detection and exclusion system as recited in claim 1, wherein said detecting means includes a receiver autonomous integrity monitoring (RAIM) system.

6. A fault exclusion system for use with a detection system which detects satellite anomalies for GPS receiver for excluding data from a satellite providing incorrect navigational data, the system comprising:

means for computing the test statistics for a predetermined number of satellites; and

means for excluding data from satellites during a later satellite anomaly condition as a function of the test statistic computed for a previous satellite anomaly condition.

7. The fault exclusion system as recited in claim 6, further including means for ranking the satellites in descending order according to the computed test statistics.

8. The fault exclusion system as recited in claim 7, wherein said excluding means is responsive to said ranking means for excluding satellites in descending order test statistics until said satellite anomaly is no longer detected.

9. The fault exclusion system as recited in claim 7, further including means for comparing said test statistics with a predetermined threshold and maintaining a list of satellites whose test statistics are less than said predetermined threshold.

10. The fault exclusion system as recited in claim 6, further including means for enabling said fault exclusion system only when said fault detection system has detected a satellite anomaly.

11. The fault exclusion system as recited in claim 7, wherein said fault exclusion system is only enabled when a predetermined number of satellites are available.

12. The fault exclusion system as recited in claim 11, wherein said predetermined number of satellites is at least six.

13. The fault exclusion system as recited in claim 9, wherein said fault exclusion system is enabled only when five satellites and an altitude input are available.

14. A method for excluding data from a GPS satellite after a satellite anomaly has been detected, the method comprising the steps of:

(a) computing the test statistics of each of the satellites;

(b) excluding data from a satellite as a function of the test statistics; and

(c) excluding data from a satellite upon detection of a subsequent satellite anomaly based on the test statistics computed for a previously detected satellite anomaly.

15. The method as recited in claim 14, wherein said test statistics are ranked in a list in descending order and said satellites are excluded one at a time starting from the top of the list until a satellite anomaly is no longer detected.

16. The method as recited in claim 15, further including the step of:

comparing the test statistics with a predetermined threshold and identifying those test statistics below said predetermined threshold.

17. A method for excluding data from a GPS satellite, comprising the steps of:

(a) receiving a signal from a plurality of GPS satellites;

(b) computing a first test statistic for said satellites;

(c) detecting a first anomaly condition based on said first test statistic;

(d) excluding one of said plurality of GPS satellites from a first navigation solution when said first anomaly condition is detected;

(e) computing a second test statistic for said GPS satellites wherein said second test statistic does not include a test statistic for said one GPS satellite excluded from said first navigation solution

(f) detecting a second anomaly condition based on said second test statistic; and

(g) determining a satellite to be excluded from a second navigation solution by evaluating said second test statistic and said test statistic for said one GPS satellite excluded from said first navigation solution.