Method and apparatus for position determination with extended SPS orbit information

• US 8,319,684 B2
• Filed: 02/05/2009
• Issued: 11/27/2012
• 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 F., Gum, Arnold Jason
• Primary Examiner(s): Keith, Jack W
• Assistant Examiner(s): GALT, CASSI J
• Application Number:
  US12/366,546
• Publication Number:
  US 20090315772A1
• Time in Patent Office: 1,391 Days
• Field of Search: 342/357.13, 342/357.15, 342/357.42, 342/357.66
• US Class Current: 342/357.66
• 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 of a mobile station, comprising:

estimating predicted orbit data of a second satellite at least in part by applying correction information received at the mobile station to previous orbit data for the second satellite stored at the mobile station, wherein the correction information is represented by one or more coefficients of one or more polynomials;

combining real-time orbit data of a first satellite and the predicted orbit data of the second satellite at least in part to determine an estimated location for the mobile station;

switching from the real-time orbit data of the first satellite to predicted orbit data of the first satellite in response to the real-time orbit data of the first satellite becoming unavailable;

interpolating the real-time data of the first satellite and the predicted orbit data of the first satellite to smooth a transition between the real-time data and the predicted orbit data; and

using the predicted orbit data of the first satellite at least in part to determine the estimated location for the mobile station.

2. The method of claim 1, further comprising receiving said correction information from a server.

3. The method of claim 1, wherein the previous orbit data for the second satellite comprises coarse orbit data.

4. The method of claim 1, further comprising:

using the real-time orbit data of the first satellite in an earlier time period to correct an error of a clock bias in the predicted orbit data of the first satellite in a later time period.

5. The method of claim 1, further comprising:

switching from the predicted orbit data of the second satellite to real-time orbit data of the second satellite in response to the real-time orbit data of the second satellite becoming available; and

using the real-time orbit data of the second satellite at least in part to determine the estimated location for the mobile station.

6. The method of claim 1, further comprising:

monitoring an age of the real-time orbit data of the first satellite, the age indicated by a time to Time of Ephemeris (TOE); and

switching from the real-time orbit data of the first satellite to the predicted orbit data of the first satellite in response to the age of the real-time orbit data exceeding a predetermined threshold.

7. A system of a mobile station, comprising:

a processor to estimate predicted orbit data of a second satellite at least in part by applying correction information received at the mobile station to previous orbit data for the second satellite stored in a memory of the mobile station, wherein the correction information is represented by one or more coefficients of one or more polynomials; and

a combining unit to combine real-time orbit data of a first satellite with the predicted orbit data of the second satellite at least in part to determine an estimated location for the mobile station, the combining unit further to switch from the real-time orbit data of the first satellite to predicted orbit data of the first satellite in response to the real-time orbit data of the first satellite becoming unavailable, to interpolate the real-time data of the first satellite and the predicted orbit data of the first satellite to smooth a transition between the real-time data and the predicted orbit data, and to use the predicted orbit data of the first satellite at least in part to determine the estimated location for the mobile station.

8. The system of claim 7, the combining unit to use real-time orbit data of a third satellite in place of the predicted orbit data of the second satellite to determine the estimated location of the mobile station at least in part in response to the real-time orbit data of the third satellite becoming available.

9. A mobile station, comprising:

means for estimating predicted orbit data of a second satellite at least in part by applying correction information received at the mobile station to previous orbit data for the second satellite stored at the mobile station, wherein the correction information is represented by one or more coefficients of one or more polynomials;

means for combining real-time orbit data of a first satellite and the predicted orbit data of the second satellite at least in part to determine an estimated location for the mobile station;

means for switching from the real-time orbit data of the first satellite to predicted orbit data of the first satellite in response to the real-time orbit data of the first satellite becoming unavailable;

means for interpolating the real-time data of the first satellite and the predicted orbit data of the first satellite to smooth a transition between the real-time data and the predicted orbit data; and

means for using the predicted orbit data of the first satellite at least in part to determine the estimated location for the mobile station.

10. The mobile station of claim 9, further comprising:

means for switching from the predicted orbit data of the second satellite to real-time orbit data of the second satellite at least in part in response to the real-time orbit data of the second satellite becoming available; and

means for using the real-time orbit data of the second satellite at least in part to determine the estimated location for the mobile station.

11. An article, comprising:

a non-transient machine-readable medium having stored thereon instructions executable by a processor of a mobile station to;

estimate predicted orbit data of a second satellite at least in part by applying correction information received at the mobile station to previous orbit data of the second satellite stored at the mobile station, wherein the correction information is represented by one or more coefficients of one or more polynomials;

combine real-time orbit data of a first satellite and the predicted orbit data of the second satellite at least in part to determine an estimated location for the mobile station;

switch from the real-time orbit data of the first satellite to predicted orbit data of the first satellite in response to the real-time orbit data of the first satellite becoming unavailable;

interpolate the real-time data of the first satellite and the predicted orbit data of the first satellite to smooth a transition between the real-time data and the predicted orbit data; and

determine the estimated location for the mobile station at least in part by using the predicted orbit data of the first satellite.

12. The article of claim 11, wherein the non-transient machine-readable medium has stored thereon further instructions executable by the processor to correct an error of a clock bias in the predicted orbit data of the first satellite in a later time period using the real-time orbit data of the first satellite in an earlier time period.