False reacquisition mitigation in high sensitivity navigational satellite signal receivers

• US 7,479,924 B2
• Filed: 11/14/2005
• Issued: 01/20/2009
• Est. Priority Date: 11/14/2005
• Status: Active Grant

• Current Assignee: CSR Technology Holdings Inc. (Qualcomm, Inc.)
• Original Assignee: SiRF Technology Holdings Incorporated (Qualcomm, Inc.)
• Inventors: Kudrethaya, Shridhara A., Wang, Chi-Shin, Jia, Zhike
• Primary Examiner(s): Tarcza; Thomas H
• Assistant Examiner(s): LIU, HARRY K
• Application Number:
  US11/274,054
• Publication Number:
  US 20070109189A1
• Time in Patent Office: 1,163 Days
• Field of Search: 34235701-35717, 375/150, 375/224, 375/345
• US Class Current: 342/357.63
• CPC Class Codes: G01S 19/24 Acquisition or tracking or demodulation of signals transmitted by the system synchronisation aspects of direct sequence spread spectrum modulation H04B1/7073

Abstract

The techniques to detect and mitigate the false reacquisition in a global satellite navigation receiver are disclosed. The false reacquisition due to frequency side-lobes and code autocorrelation secondary lobes are considered for mitigation. A set of two threshold values is used to detect correct reacquisition and reject false reacquisition. While the reacquisition of the signal is straight forward when the correlation is clear with the power above the first threshold, it is not so clear when the power is between two thresholds. So a further search for the maximum power among the retained dwells results in correct reacquisition. The search range depends upon the signal blockage interval and receiver dynamics. The feedback from navigational solution may be used to determine the search range both in frequency and code phase. In the case of frequency side-lobes, which occur only at specified frequency components, these frequencies are tested for maximum power response. The code side-lobes have similar characteristics and can be distinguished by the actual peak.

Claims

1. A method for reacquisition of signals in a global satellite navigation receiver, the method comprising:

collecting, for each carrier frequency and PN code phase dwell within a selected frequency range and selected code phase range, a sequence of correlation values derived from signals originating from a navigational satellite;

declaring a valid reacquisition at a selected dwell if a maximum power of the selected dwell exceeds a pre-determined high threshold value;

declaring a valid reacquisition at the selected dwell if the maximum power of the selected dwell is below the predetermined high threshold value, the maximum power of the selected dwell is above a pre-determined low threshold value, and the maximum power of the selected dwell is above a maximum power of all other dwells in the selected frequency range and selected code phase range.

2. The method of claim 1 wherein the predetermined high threshold value is selected based on a maximum received signal power level.

3. The method of claim 1 wherein the predetermined low threshold value is selected based on a receiver sensitivity level.

4. The method of claim 1 wherein the collecting comprises performing a search of PN code phase values within the selected code phase range, followed by a search of carrier frequency values within the selected frequency range.

5. The method of claim 4 wherein the search of carrier frequency values comprises searching frequency values spaced 1000 Hz or 1500 Hz apart.

6. The method of claim 4 wherein the search of carrier frequency values comprises determining a frequency search direction toward a frequency main lobe.

7. The method of claim 4 wherein the search of carrier frequency values comprises searching carrier frequency values in a range based on feedback from a position, velocity and time (PVT) computation.

10. The method of claim 4 wherein the search of PN code phase values comprises searching PN code phase values in a range based on feedback from a position, velocity and time (PVT) computation.

13. The method of claim 1 further comprising determining the maximum power of the selected dwell by performing a frequency domain transformation of the sequence of correlation values for the selected dwell, and identifying a frequency domain component with maximum power.

14. The method of claim 1 further comprising confirming a valid reacquisition at the selected dwell if there is no PN code autocorrelation side lobe within a predetermined number of chips from the selected dwell.

15. The method of claim 1 wherein the high threshold value is derived from a power value of the signals prior to signal blocking.

16. The method of claim 1 wherein the high threshold value is derived from a predicted power value computed from a short term average power level of the signals prior to signal blocking.

17. The method of claim 1 wherein the high threshold value is derived from a predicted power value computed by extrapolating power levels of the signals prior to blockage.

8. A method for reacquisition of signals in a global satellite navigation receiver, the method comprising:

collecting, for each carrier frequency and PN code phase dwell within a selected frequency range and selected code phase range, a sequence of correlation values derived from signals originating from a navigational satellite, wherein the collecting comprises performing a search of PN code phase values within the selected code phase range, followed by a search of carrier frequency values within the selected frequency range, and wherein the search of carrier frequency values comprises searching carrier frequency values in a range based on a duration of signal blockage and receiver dynamics;

declaring a valid reacquisition at a selected dwell if a maximum power of the selected dwell exceeds a pre-determined high threshold value; and

declaring a valid reacquisition at the selected dwell if the maximum power of the selected dwell is below the predetermined high threshold value, the maximum power of the selected dwell is above a predetermined low threshold value, and the maximum power of the selected dwell is above a maximum power of all other dwells in the selected frequency range and selected code phase range.

9. A method for reacquisition of signals in a global satellite navigation receiver, the method comprising:

collecting, for each carrier frequency and PN code phase dwell within a selected frequency range and selected code phase range, a sequence of correlation values derived from signals originating from a navigational satellite, wherein the collecting comprises performing a search of PN code phase values within the selected code phase range, followed by a search of carrier frequency values within the selected frequency range, and wherein the search of carrier frequency values comprises searching carrier frequency values in a range based on duration of signal blockage, results of PYT computation, quality of the PVT results, and receiver dynamics;

declaring a valid reacquisition at a selected dwell if a maximum power of the selected dwell exceeds a pre-determined high threshold value; and

declaring a valid reacquisition at the selected dwell if the maximum power of the selected dwell is below the predetermined high threshold value, the maximum power of the selected dwell is above a predetermined low threshold value, and the maximum power of the selected dwell is above a maximum power of all other dwells in the selected frequency range and selected code phase range.

11. A method for reacquisition of signals in a global satellite navigation receiver, the method comprising:

collecting, for each carrier frequency and PN code phase dwell within a selected frequency range and selected code phase range, a sequence of correlation values derived from signals originating from a navigational satellite, wherein the collecting comprises performing a search of PN code phase values within the selected code phase range, followed by a search of carrier frequency values within the selected frequency range, and wherein the search of PN code phase values comprises searching PN code phase values in a range based on duration of signal blockage and receiver dynamics;

declaring a valid reacquisition at a selected dwell if a maximum power of the selected dwell exceeds a pre-deterrnined high threshold value; and

declaring a valid reacquisition at the selected dwell if the maximum power of the selected dwell is below the predetermined high threshold value, the maximum power of the selected dwell is above a predetermined low threshold value, and the maximum power of the selected dwell is above a maximum power of all other dwells in the selected frequency range and selected code phase range.

12. A method for reacquisition of signals in a global satellite navigation receiver, the method comprising:

collecting, for each carrier frequency and PN code phase dwell within a selected frequency range and selected code phase range, a sequence of correlation values derived from signals originating from a navigational satellite, wherein the collecting comprises performing a search of PN code phase values within the selected code phase range, followed by a search of carrier frequency values within the selected frequency range, and wherein the search of PN code phase values comprises searching PN code phase values in a range based on duration of signal blockage, results of PVT computation, quality of the PVT computation results, and receiver dynamics;

declaring a valid reacquisition at a selected dwell if a maximum power of the selected dwell exceeds a pre-determined high threshold value; and

declaring a valid reacquisition at the selected dwell if the maximum power of the selected dwell is below the predetermined high threshold value, the maximum power of the selected dwell is above a predetermined low threshold value, and the maximum power of the selected dwell is above a maximum power of all other dwells in the selected frequency range and selected code phase range.

18. A global satellite navigation receiver device comprising an RF front end for receiving signals originating from navigation satellites, a baseband section receiving IF signals from the RF front end and generating one-millisecond correlation values, and a processor receiving correlation values from the baseband section, wherein the processor performs reacquisition of signals by:

collecting, for each carrier frequency and PN code phase dwell within a selected frequency range and selected code phase range, a sequence of correlation values derived from signals originating from a navigational satellite;

declaring a valid reacquisition at a selected dwell if a maximum power of the selected dwell exceeds a pre-determined high threshold value;

declaring a valid reacquisition at the selected dwell if the maximum power of the selected dwell is below the predetermined high threshold value, the maximum power of the selected dwell is above a pre-determined low threshold value, and the maximum power of the selected dwell is above a maximum power of all other dwells in the selected frequency range and selected code phase range.

19. The device of claim 18 wherein the predetermined high threshold value is selected based on a maximum received signal power level.

20. The device of claim 18 wherein the predetermined low threshold value is selected based on a receiver sensitivity level.

21. The device of claim 18 wherein the collecting comprises performing a search of PN code phase values within the selected code phase range, followed by a search of carrier frequency values within the selected frequency range.

22. The device of claim 21 wherein the search of carrier frequency values comprises searching frequency values spaced 1000 Hz or 1500 Hz apart.

23. The device of claim 21 wherein the search of carrier frequency values comprises determining a frequency search direction toward a frequency main lobe.

24. The device of claim 21 wherein the search of carrier frequency values comprises searching carrier frequency values in a range based on feedback from a position, velocity and time (PVT) computation.

27. The device of claim 21 wherein the search of PN code phase values comprises searching PN code phase values in a range based on feedback from a position, velocity and time (PVT) computation.

30. The device of claim 18 further comprising determining the maximum power of the selected dwell by performing a frequency domain transformation of the sequence of correlation values for the selected dwell, and identifying a frequency domain component with maximum power.

31. The device of claim 18 further comprising confirming a valid reacquisition at the selected dwell if there is no PN code autocorrelation side lobe within a predetermined number of chips from the selected dwell.

32. The device of claim 18 wherein the high threshold value is derived from a power value of the signals prior to signal blocking.

33. The device of claim 18 wherein the high threshold value is derived from a predicted power value computed from a short term average power level of the signals prior to signal blocking.

34. The device of claim 18 wherein the high threshold value is derived from a predicted power value computed by extrapolating power levels of the signals prior to blockage.

25. A global satellite navigation receiver device comprising an RF front end for receiving signals originating from navigation satellites, a baseband section receiving IF signals from the RF front end and generating one-millisecond correlation values, and a processor receiving correlation values from the baseband section, wherein the processor performs reacquisition of signals by:

collecting, for each carrier frequency and PN code phase dwell within a selected frequency range and selected code phase range, a sequence of correlation values derived from signals originating from a navigational satellite, wherein the collecting comprises performing a search of PN code phase values within the selected code phase range, followed by a search of carrier frequency values within the selected frequency range, and wherein the search of carrier frequency values comprises searching carrier frequency values in a range based on a duration of signal blockage and receiver dynamics;

declaring a valid reaquisition at a selected dwell if a maximum power of the selected dwell exceeds a pre-determined high threshold value; and

declaring a valid requisition at the selected dwell if the maximum power of the selected dwell is below the predetermined high threshold value, the maximum power of the selected dwell is above a pre-determined low threshold value, and the maximum power of the selected dwell is above a maximum power of all other dwells in the selected frequency range and selected code phase range.

26. A global satellite navigation receiver device comprising an RF front end for receiving signals originating from navigation satellites, a baseband section receiving IF signals from the RF front end and generating one-millisecond correlation values, and a processor receiving correlation values from the baseband section, wherein the processor performs reacquisition of signals by:

collecting, for each carrier frequency and PN code phase dwell within a selected frequency range and selected code phase range, a sequence of correlation values derived from signals originating from a navigational satellite, wherein the collecting comprises performing a search of PN code phase values within the selected code phase range, followed by a search of carrier frequency values within the selected frequency range, and wherein the search of carrier frequency values comprises searching carrier frequency values in a range based on duration of signal blockage, results of PVT computation, quality of the PVT results, and receiver dynamics;

declaring a valid reacquisition at a selected dwell if a maximum power of the selected dwell exceeds a pre-determined high threshold value; and

declaring a valid reacquisition at the selected dwell if the maximum power of the selected dwell is below the predetermined high threshold value, the maximum power of the selected dwell is above a pre-determined low threshold value, and the maximum power of the selected dwell is above a maximum power of all other dwells in the selected frequency range and selected code phase range.

28. A global satellite navigation receiver device comprising an RF front end for receiving signals originating from navigation satellites, a baseband section receiving IF signals from the RF front end and generating one-millisecond correlation values, and a processor receiving correlation values from the baseband section, wherein the processor performs reacquisition of signals by:

collecting, for each carrier frequency and PN code phase dwell within a selected frequency range and selected code phase range, a sequence of correlation values derived from signals originating from a navigational satellite, wherein the collecting comprises performing a search of PN code phase values within the selected code phase range, followed by a search of carrier frequency values within the selected frequency range, and wherein the search of PN code phase values comprises searching PN code phase values in a range based on duration of signal blockage and receiver dynamics;

declaring a valid reacquisition at a selected dwell if a maximum power of the selected dwell exceeds a pre-determined high threshold value; and

declaring a valid reacquisition at the selected dwell if the maximum power of the selected dwell is below the predetermined high threshold value, the maximum power of the selected dwell is above a pre-determined low threshold value, and the maximum power of the selected dwell is above a maximum power of all other dwells in the selected frequency range and selected code phase range.

29. A global satellite navigation receiver device comprising an RF front end for receiving signals originating from navigation satellites, a baseband section receiving IF signals from the RF front end and generating one-millisecond correlation values, and a processor receiving correlation values from the baseband section, wherein the processor performs reacquisition of signals by:

collecting, for each carrier frequency and PN code phase dwell within a selected frequency range and selected code phase range, a sequence of correlation values derived from signals originating from a navigational satellite, wherein the collecting comprises performing a search of PN code phase values within the selected code phase range, followed by a search of carrier frequency values within the selected frequency range, and wherein the search of PN code phase values comprises searching PN code phase values in a range based on duration of signal blockage, results of PVT computation, quality of the PVT computation results, and receiver dynamics;

declaring a valid reacquisition at a selected dwell if a maximum power of the selected dwell exceeds a pre-determined high threshold value; and

declaring a valid reacquisition at the selected dwell if the maximum power of the selected dwell is below the predetermined hinh threshold value, the maximum power of the selected dwell is above a pre-detennined low threshold value, and the maximum power of the selected dwell is above a maximum power of all other dwells in the selected frequency range and selected code phase range.