Method and apparatus for position determination with extended SPS orbit information

• US 9,019,157 B2
• Filed: 08/09/2012
• Issued: 04/28/2015
• Est. Priority Date: 11/10/2006
• Status: Active Grant

• Current Assignee: Qualcomm, Inc.
• Original Assignee: Qualcomm, Inc.
• Inventors: Wengler, Michael James, Sheynblat, Leonid, Moeglein, Mark Leo, Biacs, Zoltan, Gum, Arnold Jason
• Primary Examiner(s): Phan, Dao
• Application Number:
  US13/571,161
• Publication Number:
  US 20130201056A1
• Time in Patent Office: 992 Days
• Field of Search: 342/357.42, 342/357.44, 342/357.64, 342/357.66, 342/357.23, 701/469
• US Class Current: 342/357.42
• CPC Class Codes: G01S 19/05 providing aiding data
• 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

Abstract

A method and system for assisting mobile stations to locate a satellite use an efficient messaging format. A server computes a correction between coarse orbit data of a satellite and precise orbit data of the satellite. A coordinate system is chosen such that variation of the correction is substantially smooth over time. The server further approximates the correction with mathematical functions to reduce the number of bits necessary for transmission to a mobile station. The mobile station, upon receiving the coefficients, evaluates the mathematical functions using the coefficients and a time of applicability (e.g., the current time), converts the evaluated result to a standard coordinate system, and applies the conversion result to the coarse orbit data to obtain the precise orbit data.

Claims

1. A method by a mobile station of locating a satellite, the method comprising:

receiving, by the mobile station, coarse orbit data of the satellite including a coarse estimate of the satellite'"'"'s position;

generating, by the mobile station, a coarse satellite position of the satellite using at least the coarse estimate of the satellite'"'"'s position;

receiving, by the mobile station, coarse orbit correction data of the satellite calculated using the coarse orbit data and predicted orbit data of the satellite, wherein the calculation of the coarse orbit correction data occurs at an entity geographically distinct from the mobile station, and wherein the predicted orbit data is more accurate than the coarse orbit data;

reconstructing, by the mobile station, at least one spatial correction value to the coarse orbit data at least based on the coarse orbit correction data;

converting, by the mobile station, the at least one spatial correction value from a satellite-centered coordinate system to an earth-centered, earth-fixed coordinate system; and

determining, by the mobile station, a corrected position of the satellite using the coarse satellite position of the satellite and the at least one spatial correction value converted to the earth-centered, earth-fixed coordinate system, wherein the corrected position of the satellite is more accurate than the coarse satellite position.

2. The method of claim 1, wherein the coarse orbit data further includes a coarse estimate of clock data of the satellite.

3. The method of claim 2, wherein the predicted orbit data includes a predicted estimate of clock data of the satellite, wherein the predicted estimate of clock data of the satellite is more accurate than the coarse estimate of clock data of the satellite.

4. The method of claim 3, further comprising:

generating by the mobile station a coarse clock bias value of the satellite using at least the coarse estimate of clock data of the satellite;

receiving by the mobile station coarse clock bias correction data of the satellite calculated using the coarse orbit data and the predicted orbit data of the satellite, wherein the calculation of the coarse clock bias correction data occurs at the entity; and

reconstructing by the mobile station at least one temporal correction value to the coarse orbit data at least based on the coarse clock bias correction data.

5. The method of claim 4, further comprising:

determining by the mobile station a corrected clock bias value of the satellite using the coarse clock bias value of the satellite and the at least one temporal correction value, wherein the corrected clock bias value of the satellite is more accurate than the coarse clock bias value.

6. The method of claim 1, wherein the coarse orbit correction data is based on a difference in position between the coarse orbit data and the predicted orbit data.

7. The method of claim 1, wherein the coarse orbit correction data includes at least one coefficient of one or more series of mathematical functions used to approximate the satellite'"'"'s position.

8. The method of claim 7 wherein reconstructing the at least one spatial correction value is based further on evaluating at least one of the one or more series of mathematical functions using the at least one coefficient.

9. The method of claim 1, wherein the predicted orbit data comprises at least one of the following:

3-D uncertainty values for predicted satellite coordinates, uncertainty of predicted satellite clock corrections, and an indication of predicted outages.

10. The method of claim 1, wherein the coarse orbit correction data is approximated by polynomials of a 7^th order, and wherein reconstructing the at least one spatial correction value is based further on the approximation.

11. The method of claim 1, wherein the coarse orbit data includes almanac data of the satellite, and wherein the predicted orbit data includes a precise representation of a position of the satellite, the predicted orbit data being generated by the entity using real time orbit data.

12. The method of claim 11, wherein the real time orbit data includes ephemeris data having a period of validity approximately 4 hours long, and wherein the predicted orbit data has a period of validity longer than the period of validity of the real time orbit data.

13. A mobile station configured to locate a satellite, the mobile station comprising:

a receiver configured to;

receive coarse orbit data of the satellite including a coarse estimate of the satellite'"'"'s position; and

receive coarse orbit correction data of the satellite calculated using the coarse orbit data and predicted orbit data of the satellite, wherein the calculation of the coarse orbit correction data occurs at an entity geographically distinct from the mobile station, and wherein the predicted orbit data is more accurate than the coarse orbit data; and

a processor configured to;

generate a coarse satellite position of the satellite using at least the coarse estimate of the satellite'"'"'s position;

reconstruct at least one spatial correction value to the coarse orbit data at least based on the coarse orbit correction data;

convert the at least one spatial correction value from a satellite-centered coordinate system to an earth-centered, earth-fixed coordinate system; and

determine a corrected position of the satellite using the coarse satellite position of the satellite and the at least one spatial correction value converted to the earth-centered, earth-fixed coordinate system, wherein the corrected position of the satellite is more accurate than the coarse satellite position.

14. The mobile station of claim 13, wherein the coarse orbit data further includes a coarse estimate of clock data of the satellite.

15. The mobile station of claim 14, wherein the predicted orbit data includes a predicted estimate of clock data of the satellite, wherein the predicted estimate of clock data of the satellite is more accurate than the coarse estimate of clock data of the satellite.

16. The mobile station of claim 15, wherein the receiver is further configured to:

receive coarse clock bias correction data of the satellite calculated using the coarse orbit data and the predicted orbit data of the satellite, wherein the calculation of the coarse clock bias correction data occurs at the entity; and

wherein the processor is further configured to;

generate a coarse clock bias value of the satellite using at least the coarse estimate of clock data of the satellite; and

reconstruct at least one temporal correction value to the coarse orbit data at least based on the coarse clock bias correction data.

17. The mobile station of claim 16, wherein the processor is further configured to:

determine a corrected clock bias value of the satellite using the coarse clock bias value of the satellite and the at least one temporal correction value, wherein the corrected clock bias value of the satellite is more accurate than the coarse clock bias value.

18. The mobile station of claim 13, wherein the coarse orbit correction data is based on a difference in position between the coarse orbit data and the predicted orbit data.

19. The mobile station of claim 13, wherein the coarse orbit correction data includes at least one coefficient of one or more series of mathematical functions used to approximate the satellite'"'"'s position.

20. The mobile station of claim 19 wherein reconstructing the at least one spatial correction value is based further on evaluating at least one of the one or more series of mathematical functions using the at least one coefficient.

21. The mobile station of claim 13, wherein the predicted orbit data comprises at least one of the following:

3-D uncertainty values for predicted satellite coordinates, uncertainty of predicted satellite clock corrections, and an indication of predicted outages.

22. The mobile station of claim 13, wherein the coarse orbit correction data is approximated by polynomials of a 7^th order, and wherein reconstructing the at least one spatial correction value is based further on the approximation.

23. The mobile station of claim 13, wherein the coarse orbit data includes almanac data of the satellite, and wherein the predicted orbit data includes a precise representation of a position of the satellite, the predicted orbit data being generated by the entity using real time orbit data.

24. The mobile station of claim 23, wherein the real time orbit data includes ephemeris data having a period of validity approximately 4 hours long, and wherein the predicted orbit data has a period of validity longer than the period of validity of the real time orbit data.

25. An apparatus for locating a satellite, the apparatus comprising:

means for receiving coarse orbit data of the satellite including a coarse estimate of the satellite'"'"'s position;

means for generating a coarse satellite position of the satellite using at least the coarse estimate of the satellite'"'"'s position;

means for receiving coarse orbit correction data of the satellite calculated using the coarse orbit data and predicted orbit data of the satellite, wherein the calculation of the coarse orbit correction data occurs at an entity geographically distinct from the mobile station, and wherein the predicted orbit data is more accurate than the coarse orbit data;

means for reconstructing at least one spatial correction value to the coarse orbit data at least based on the coarse orbit correction data;

means for converting the at least one spatial correction value from a satellite-centered coordinate system to an earth-centered, earth-fixed coordinate system; and

means for determining a corrected position of the satellite using the coarse satellite position of the satellite and the at least one spatial correction value converted to the earth-centered, earth-fixed coordinate system, wherein the corrected position of the satellite is more accurate than the coarse satellite position.

26. The apparatus of claim 25, wherein the coarse orbit data further includes a coarse estimate of clock data of the satellite.

27. The apparatus of claim 26, wherein the predicted orbit data includes a predicted estimate of clock data of the satellite, wherein the predicted estimate of clock data of the satellite is more accurate than the coarse estimate of clock data of the satellite.

28. The apparatus of claim 27, further comprising:

means for generating a coarse clock bias value of the satellite using at least the coarse estimate of clock data of the satellite;

means for receiving coarse clock bias correction data of the satellite calculated using the coarse orbit data and the predicted orbit data of the satellite, wherein the calculation of the coarse clock bias correction data occurs at the entity; and

means for reconstructing at least one temporal correction value to the coarse orbit data at least based on the coarse clock bias correction data.

29. The apparatus of claim 28, further comprising:

means for determining a corrected clock bias value of the satellite using the coarse clock bias value of the satellite and the at least one temporal correction value, wherein the corrected clock bias value of the satellite is more accurate than the coarse clock bias value.

30. A non-transitory computer program product configured to enable a processor to locate a satellite, the computer program product comprising instructions to cause the processor to:

receive coarse orbit data of the satellite including a coarse estimate of the satellite'"'"'s position;

receive coarse orbit correction data of the satellite calculated using the coarse orbit data and predicted orbit data of the satellite, wherein the calculation of the coarse orbit correction data occurs at an entity geographically distinct from the mobile station, and wherein the predicted orbit data is more accurate than the coarse orbit data; and

generate a coarse satellite position of the satellite using at least the coarse estimate of the satellite'"'"'s position;

reconstruct at least one spatial correction value to the coarse orbit data at least based on the coarse orbit correction data;

convert the at least one spatial correction value from a satellite-centered coordinate system to an earth-centered, earth-fixed coordinate system; and

determine a corrected position of the satellite using the coarse satellite position of the satellite and the at least one spatial correction value converted to the earth-centered, earth-fixed coordinate system, wherein the corrected position of the satellite is more accurate than the coarse satellite position.

31. The non-transitory computer program product of claim 30, wherein the coarse orbit data further includes a coarse estimate of clock data of the satellite.

32. The non-transitory computer program product of claim 31, wherein the predicted orbit data includes a predicted estimate of clock data of the satellite, wherein the predicted estimate of clock data of the satellite is more accurate than the coarse estimate of clock data of the satellite.

33. The non-transitory computer program product of claim 32, wherein the instructions further cause the processor to:

receive coarse clock bias correction data of the satellite calculated using the coarse orbit data and the predicted orbit data of the satellite, wherein the calculation of the coarse clock bias correction data occurs at the entity;

generate a coarse clock bias value of the satellite using at least the coarse estimate of clock data of the satellite; and

reconstruct at least one temporal correction value to the coarse orbit data at least based on the coarse clock bias correction data.

34. The non-transitory computer program product of claim 33, wherein the instructions further cause the processor to:

determine a corrected clock bias value of the satellite using the coarse clock bias value of the satellite and the at least one temporal correction value, wherein the corrected clock bias value of the satellite is more accurate than the coarse clock bias value.