Frequency error tracking in satellite positioning system receivers

• US 7,061,425 B2
• Filed: 11/12/2004
• Issued: 06/13/2006
• Est. Priority Date: 11/12/2004
• Status: Active Grant

• Current Assignee: Google Technology Holdings LLC (Alphabet Inc.)
• Original Assignee: Motorola, Inc. (Motorola Solutions, Inc.)
• Inventors: Nory, Ravikiran, King, Thomas M., Geier, George J., Yuan, Xiang
• Primary Examiner(s): Phan, Dao
• Application Number:
  US10/986,697
• Publication Number:
  US 20060103573A1
• Time in Patent Office: 578 Days
• Field of Search: 342/357.02, 342/357.06, 342/357.15, 342/357.12, 701/213, 701/215
• US Class Current: 342/357.68
• CPC Class Codes: G01S 19/29 carrier including Doppler, related G01S19/246 takes precedence

Abstract

A method in a satellite positioning system (SPS) receiver 100 including acquiring a plurality of at least two SPS signals, estimating frequency error for each of the plurality of SPS signals, and compensating for the frequency error of each of the plurality of SPS signal based on the estimated frequency errors for all of the plurality of SPS signals.

Claims

1. A method in a satellite positioning system (SPS) receiver, the method comprising:

acquiring a plurality of at least two SPS signals;

estimating frequency error for each of the plurality of SPS signals;

compensating for the frequency error of each of the plurality of SPS signals based on the estimated frequency errors for all of the plurality of SPS signals.

2. The method of claim 1, estimating the frequency error of the plurality of SPS signals based on an evaluation of the plurality of SPS signals over a time period greater than a data bit period of the SPS signals.

3. The method of claim 1, estimating the frequency error of the plurality of SPS signals based only on frequency information.

4. The method of claim 1, estimating the frequency error of the plurality of SPS signals based only on frequency information, without tracking phase information, obtained from each of the plurality of SPS signals for a time period greater than a data bit period of the SPS signals.

5. The method of claim 1,

correlating each of the plurality of SPS signals for multiple time periods, each of the time periods less than a data bit period of the of SPS signals,

estimating the frequency error of each of the plurality of SPS signals based on the multiple correlations of each of the plurality of SPS signals for a time period greater than a data bit period of the plurality of SPS signals.

6. A method in a satellite positioning system (SPS) receiver, the method comprising:

acquiring a plurality of at least two SPS signals;

estimating frequency error for each of the plurality of SPS signals;

compensating for any frequency error of each of the plurality of SPS signals based on a reference frequency error of the SPS receiver,

the reference frequency error of the SPS receiver based on the estimated frequency errors of the plurality of SPS signals.

7. The method of claim 6, determining the reference frequency error of the SPS receiver based on a weighting of the estimated frequency errors of the plurality of SPS signals.

8. The method of claim 6, determining the reference frequency error of the SPS receiver based on a weighting of the estimated frequency errors of the plurality of SPS signals, wherein the weighting of the estimated frequency errors of the plurality of SIPS signals is based on an elevation of the sources of the plurality of SPS signals.

9. The method of claim 6, compensating for frequency error of each of the plurality of SPS signals based on one of an estimated acceleration error of the SPS receiver, an estimated rate of change of a reference frequency of the SPS receiver, and an estimated velocity error of the SPS receiver.

10. A method in a satellite positioning system (SPS) receiver, the method comprising:

estimating frequency error for a plurality of at least two SPS signals at a first rate;

generating frequency tracking information for each of the plurality SPS signals at a second rate;

compensating for the estimated frequency error of each of the plurality of SPS signals based on the frequency tracking information generated at the second rate.

11. The method of claim 10, generating the frequency tracking information for each of the plurality of SPS signals at the second rate less than the first rate.

12. The method of claim 10, generating the frequency tracking information for each of the plurality of SPS signals includes one of generating a tracking bandwidth for each of the plurality of SPS signals, generating tracking gain for each of the plurality of SPS signals.

13. A method in a satellite positioning system (SPS) receiver, the method comprising:

detecting a change in a condition monitored by the SPS receiver;

generating frequency tracking information for a plurality of SPS signals based on the detected change in the condition monitored;

tracking frequency for the plurality of SPS signals based on frequency tracking information generated for the plurality of SPS signals.

14. The method of claim 13, detecting the change in the condition based on a change in magnitude between frequency measurements for the plurality of SPS signals and estimated frequencies values for the plurality of SPS signals.

15. The method of claim 13, wherein generating the frequency tracking information for each of the plurality of SPS signals includes one of tracking bandwidth for each of the plurality of SPS signals, and generating tracking gain for each of the plurality of SPS signals.

16. The method of claim 13, wherein generating the frequency tracking information for each of the plurality of SPS signals includes tracking bandwidth for each of the plurality of SPS signals.

17. The method of claim 15, tracking the bandwidth based on increasing the bandwidth towards a maximum value at a first rate and decreasing the bandwidth towards a minimum value at a second rate.