Method and apparatus for geolocation determination

• US 7,692,577 B2
• Filed: 08/29/2008
• Issued: 04/06/2010
• Est. Priority Date: 04/18/2006
• Status: Active Grant

• Current Assignee: REDEX S.A.
• Original Assignee: Andrew Corporation (CommScope Holding Company, Inc.)
• Inventors: Nicholson, Peter, Harper, Neil
• Primary Examiner(s): Tarcza, Thomas H
• Assistant Examiner(s): Nguyen, Nga X
• Application Number:
  US12/201,279
• Publication Number:
  US 20090079623A1
• Time in Patent Office: 585 Days
• Field of Search: 34235701-35717
• US Class Current: 342/357.58
• CPC Class Codes: G01S 19/20 Integrity monitoring, fault detection or fault isolation of space segment
• CPC Class Codes: G01S 19/252 Employing an initial estimate of location in generating assistance data

Abstract

The disclosure relates to method and apparatus for geolocation determination. In one embodiment, the disclosure relates to a method for detecting an erroneous satellite measurement by a receiver, including the steps of (a) determining an approximate location of the receiver; (b) for each of a plurality of satellites from which the receiver receives a signal: (i) determining a range difference between an expected range between the receiver and the satellite and a measured range between the receiver and the satellite; (ii) determining a median value of the range differences; (iii) determining an offset value between the range difference and the median value; (iv) comparing the offset value with a predetermined threshold to thereby detect an erroneous satellite measurement.

Claims

1. A method for detecting an erroneous satellite measurement from a signal sent by a satellite and received by a receiver, comprising the steps of:

(a) determining an approximate location of the receiver;

(b) determining an elevation for each of a plurality of satellites from which the receiver receives a signal; and

(c) for each one of the plurality of satellites;

(i) determining an uncertainty value as a function of the satellite elevation;

(ii) determining an expected range between the receiver and the satellite;

(iii) measuring a range between the receiver and the satellite;

(iv) determining a range difference between the expected range and the measured range;

(v) determining a median value of the range differences;

(vi) determining an offset value between the range difference and the median value; and

(vii) comparing the offset value with a value that is the sum of the uncertainty value and a predetermined threshold to thereby detect an erroneous satellite measurement.

2. The method of claim 1 wherein the satellites are part of a Global Navigation Satellite System (“

GNSS”

).

3. The method of claim 2 wherein the satellites are part of the Beidou satellite system.

4. The method of claim 3 wherein the expected range is determined as a function of the location of the satellites.

5. The method of claim 2 wherein the GNSS is selected from the group consisting of:

Global Positioning System (“

GPS”

), Galileo, GLONASS, and Quasi-Zenith Satellite System (“

QZSS”

).

6. The method of claim 5 wherein the step of determining an approximate location of the receiver is independent of signals transmitted by the satellites and received by the receiver.

7. The method of claim 6 wherein the receiver receives signals from a cellular communication network.

8. The method of claim 7 wherein the approximate location of the receiver is a function of an area of a cell in the cellular communication network.

9. The method of claim 8 wherein the expected range is determined as a function of the approximate location of the receiver.

10. The method of claim 9 wherein the step of determining an elevation of the satellites is a function of ephemeris information received from at least one of the plurality of satellites and the approximate location of the user.

11. The method of claim 10 wherein the step of determining an expected range between the satellite and the receiver includes determining a predicted code phase.

12. The method of claim 11 wherein the step of measuring a range between the receiver and the satellite includes determining a measured code phase that is a function of a clock signal for the satellite from a signal transmitted by the satellite and received by the receiver.

13. The method of claim 12 wherein the local clock signal and the satellite clock signal are not synchronized.

14. The method of claim 13 wherein the predetermined threshold is a code phase value greater than or equal to four.

15. The method of claim 13 wherein the predetermined threshold is a code phase value greater than or equal to two.

16. The method of claim 13 wherein the predetermined threshold is a code phase value greater than or equal to one.

17. A method for detecting an erroneous satellite measurement from a signal sent by a Global Navigation Satellite System (“

GNSS”

) satellite and received by a receiver, where the receiver is receiving signals from a cellular communication network, comprising the steps of;

(a) determining an approximate location of the receiver as a function of an area of a cell in the cellular communication network;

(b) determining an elevation for each of a plurality of satellites from which the receiver receives a signal as a function of ephemeris information received from at least one of the plurality of satellites;

(c) for each one of the plurality of satellites;

(i) determining an uncertainty value as a function of the satellite elevation and the approximate location of the receiver;

(ii) determining an expected range between the receiver and the satellite as a function of the ephemeris information and the approximate location of the receiver;

(iii) measuring a range between the receiver and the satellite from a signal transmitted by the satellite and received by the receiver

(iv) determining a range difference between the expected range and the measured range;

(v) determining a median value of the range differences;

(vi) determining an offset value between the range difference and the median value; and

(vii) comparing the offset value with a value that is the sum of the uncertainty value and a predetermined threshold to thereby detect an erroneous satellite measurement.

18. The method of claim 17 wherein the satellites are part of the Beidou satellite system.

19. The method of claim 17 wherein the GNSS is selected from the group consisting of:

Global Positioning System (“

GPS”

), Galileo, GLONASS, and Quasi-Zenith Satellite System (“

QZSS”

).

20. The method of claim 17 wherein the step of determining an approximate location of the receiver is independent of signals transmitted by the satellites and received by the receiver.

21. The method of claim 17 wherein the local clock signal and the satellite clock signal are not synchronized.

22. An apparatus for detecting an erroneous satellite measurement from a signal sent by a satellite and received by a receiver, comprising:

means for determining an approximate location of said receiver;

circuitry for determining an elevation for each of a plurality of satellites from which said receiver receives a signal;

circuitry for determining an uncertainty value as a function of the satellite elevation for each respective one of said plural satellites;

circuitry for determining an expected range between said receiver and each respective one of said plural satellites;

circuitry for measuring a range between said receiver and each respective one of said plural satellites;

circuitry for determining a range difference between the expected range and the measured range for each respective one of said plural satellites;

circuitry for determining a median value of the range differences;

circuitry for determining an offset value between the median value and the range difference for each respective one of said plural satellites; and

circuitry for comparing the offset value with a value that is the sum of the uncertainty value and a predetermined threshold to thereby detect an erroneous satellite measurement.

23. The apparatus of claim 22 wherein said plural satellites are part of a Global Navigation Satellite System (“

GNSS”

).

24. The apparatus of claim 23 wherein said plural satellites are part of the Beidou satellite system.

25. The apparatus of claim 23 wherein the GNSS is selected from the group consisting of:

Global Positioning System (“

GPS”

), Galileo, GLONASS, and Quasi-Zenith Satellite System (“

QZSS”

).

26. The apparatus of claim 25 wherein said means for determining an approximate location of the receiver operates independently of signals transmitted by said plural satellites and received by said receiver.

27. The apparatus of claim 26 wherein said receiver receives signals from a cellular communication network.

28. The apparatus of claim 27 wherein the approximate location of said receiver is determined by an area of a cell in said cellular communication network.

29. The apparatus of claim 28 wherein the expected range is determined as a function of the approximate location of said receiver.

30. The apparatus of claim 29 wherein said circuitry for determining an elevation of the satellites operates on ephemeris information received from at least one of the plurality of satellites and the approximate location of the user.

31. The apparatus of claim 30 wherein said circuitry for determining an expected range between said receiver and each respective one of said plural satellites includes determining a predicted code phase.

32. The apparatus of claim 31 wherein said circuitry for measuring a range between said receiver and each respective one of said plural satellites includes circuitry for determining a measured code phase that is a function of a clock signal for a respective one of said plural satellites from a signal transmitted by said respective one satellite and received by said receiver.

33. The apparatus of claim 32 wherein a local clock signal at said receiver and a satellite clock signal for said respective one satellite are not synchronized.

34. The apparatus of claim 33 wherein the predetermined threshold is a code phase value greater than or equal to four.

35. The apparatus of claim 33 wherein the predetermined threshold is a code phase value greater than or equal to two.

36. The apparatus of claim 33 wherein the predetermined threshold is a code phase value greater than or equal to one.

37. An apparatus for detecting an erroneous satellite measurement from a signal sent by a Global Navigation Satellite System (“

GNSS”

) satellite and received by a receiver, where the receiver is receiving signals from a cellular communication network, comprising;

circuitry for determining an approximate location of said receiver as an area of a cell in the cellular communication network;

circuitry for determining an elevation for each of a plurality of satellites from which said receiver receives a signal as a function of ephemeris information received from at least one of said plural satellites;

circuitry for determining an uncertainty value as a function of the satellite elevation for each respective one of said plural satellites and the approximate location of said receiver;

circuitry for determining an expected range between said receiver and each respective one of said plural satellites as a function of the ephemeris information and the approximate location of said receiver;

circuitry for measuring a range between said receiver and each respective one of said plural satellites from a signal transmitted by a respective one of said plural satellites and received by said receiver;

circuitry for determining a range difference between the expected range and the measured range;

circuitry for determining a median value of the range differences;

circuitry for determining an offset value between the median value and the range difference for each respective one of said plural satellites; and

circuitry for comparing the offset value with a value that is the sum of the uncertainty value and a predetermined threshold to thereby detect an erroneous satellite measurement.

38. The apparatus of claim 37 wherein said plural satellites are part of the Beidou satellite system.

39. The apparatus of claim 37 wherein the GNSS is selected from the group consisting of:

Global Positioning System (“

GPS”

), Galileo, GLONASS, and Quasi-Zenith Satellite System (“

QZSS”

).

40. The apparatus of claim 37 wherein said circuitry for determining an approximate location of said receiver operates independently of signals transmitted by said plural satellites and received by said receiver.

41. The apparatus of claim 37 wherein a local clock signal at said receiver and a satellite clock signal for one of said plural satellites are not synchronized.