Prediction refresh method for ephemeris extensions

• US 8,497,801 B2
• Filed: 02/04/2008
• Issued: 07/30/2013
• Est. Priority Date: 02/05/2007
• Status: Expired due to Fees

• Current Assignee: Qualcomm, Inc.
• Original Assignee: Qualcomm, Inc.
• Inventors: Garin, Lionel, Gupta, Pramod, Venkatraman, SaiPradeep
• Primary Examiner(s): Keith, Jack W
• Assistant Examiner(s): GALT, CASSI J
• Application Number:
  US12/025,252
• Publication Number:
  US 20080186228A1
• Time in Patent Office: 2,003 Days
• Field of Search: 342/357.15, 342/357.66
• US Class Current: 342/357.66
• CPC Class Codes: G01S 19/258 relating to the satellite constellation, e.g. almanac, ephemeris data, lists of satellites in view
• CPC Class Codes: G01S 19/27 creating, predicting or correcting ephemeris or almanac data within the receiver
• CPC Class Codes: G01S 19/42 Determining position

Abstract

Systems, methods and devices for using ephemeris data in GNSS receivers and systems are provided. Receivers using synthetic ephemeris data for longer ephemeris availability under poor reception conditions are updated using a variety of techniques that allow for the transfer of accurate information onto degraded synthetic ephemeris information.

Claims

1. A method comprising:

obtaining, by an end user GNSS receiver, a broadcast ephemeris data set associated with a GNSS;

obtaining, by the end user GNSS receiver, a current position;

measuring, by the end user GNSS receiver, a range to a first satellite to obtain a first pseudorange;

calculating, by the end user GNSS receiver, based on a synthetic ephemeris data set for a second satellite, a range to the second satellite to obtain a second pseudorange;

attributing, by the end user GNSS receiver, error in the second pseudorange only to clock error in the synthetic ephemeris data set; and

determining, by the end user GNSS receiver, a clock correction for the synthetic ephemeris data set based, at least in part, on a difference-based relationship associated with the first pseudorange and the second pseudorange.

2. The method of claim 1, wherein determining the clock correction is further based, at least in part, on a position estimate obtained from a non-GNSS source.

3. The method of claim 2, wherein the non-GNSS source comprises a map-matching engine.

4. The method of claim 2, wherein the non-GNSS source comprises a communication network.

10. The method of claim 1, wherein the difference-based relationship includes an ionospheric difference.

11. The method of claim 1, wherein the difference-based relationship includes a tropospheric difference.

12. The method of claim 1, wherein the difference-based relationship includes a geometric range difference.

5. An apparatus comprising:

a receiver section configured to receive GNSS signals; and

a processor configured to;

obtain a broadcast ephemeris data set associated with a GNSS;

obtain a current position;

measure a range to a first satellite to obtain a first pseudorange;

calculate, based on a synthetic ephemeris data set for a second satellite, a range to the second satellite to obtain a second pseudorange;

attribute error in the second pseudorange only to clock error in the synthetic ephermeris data set; and

determine a clock correction for the synthetic ephemeris data set based, at least in part, on a difference-based relationship associated with the first pseudorange and the second pseudorange.

13. The apparatus of claim 5, wherein the difference-based relationship includes an ionospheric difference.

14. The apparatus of claim 5, wherein the difference-based relationship includes a tropospheric difference.

15. The apparatus of claim 5, wherein the difference-based relationship includes a geometric range difference.

6. An apparatus comprising:

means for obtaining a broadcast ephemeris data set associated with a GNSS;

means for obtaining a current position;

means for measuring a range to a first satellite to obtain a first pseudorange;

means for calculating, based on a synthetic ephemeris data set for a second satellite, a range to the second satellite to obtain a second pseudorange;

means for attributing error in the second pseudorange only to a clock error in the synthetic ephemeris data set; and

means for determining a clock correction for the synthetic ephemeris data set based, at least in part, on a difference-based relationship associated with the first pseudorange and the second pseudorange.

7. The apparatus of claim 6, wherein the clock correction is determined further based, at least in part, on a position estimate obtained from a non-GNSS source.

8. The apparatus of claim 7, wherein the non-GNSS source comprises a map-matching engine.

9. The apparatus of claim 7, wherein the non-GNSS source comprises a communication network.

16. The apparatus of claim 6, wherein the difference-based relationship includes an ionospheric difference.

17. The apparatus of claim 6, wherein the difference-based relationship includes a tropospheric difference.

18. The apparatus of claim 6, wherein the difference-based relationship includes a geometric range difference.