High sensitivity GPS receiver

• US 8,755,472 B2
• Filed: 07/09/2013
• Issued: 06/17/2014
• Est. Priority Date: 06/27/2007
• Status: Expired due to Fees

• Current Assignee: Qualcomm, Inc.
• Original Assignee: Qualcomm, Inc.
• Inventors: Sun, Qinfang, Chen, Ho-Chung, Yeh, Wen-Chang
• Primary Examiner(s): Yu, Lihong
• Application Number:
  US13/937,757
• Publication Number:
  US 20130294549A1
• Time in Patent Office: 343 Days
• Field of Search: 375/340
• US Class Current: 375/343
• 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
• CPC Class Codes: G01S 19/30 code related G01S19/246 takes precedence
• CPC Class Codes: G01S 19/36 relating to the receiver frond end
• CPC Class Codes: G01S 19/37 Hardware or software details of the signal processing chain
• CPC Class Codes: H04L 7/0016 correction of synchronization errors

Abstract

A high sensitivity GPS receiver includes an acquisition engine and a tracking engine. The acquisition engine processes GPS satellite data at data rate that is substantially equal to twice the coarse acquisition (CA) code chip rate. This data rate advantageously enables the acquisition engine to process GPS satellite data with relatively less hardware area than traditional GPS acquisition approaches. In one embodiment, the high efficiency acquisition engine may be over-clocked, thereby allowing different phases of a CA code to be correlated quickly. The tracking engine can advantageously process GPS satellite data at a data rate that does not have an integer relationship to the CA code chip rate.

Claims

1. A method of tracking a Global Positioning Satellite (GPS) signal, the method comprising:

executing a pull-in stage by setting a center frequency of a phase-locked loop (PLL) having an initial bandwidth to a Doppler frequency of the GPS signal;

determining whether the PLL has converged in a first occurrence over an initial integration time;

determining whether the PLL has false convergence by comparing a power of an in-phase component to a power of a quadrature component of the GPS signal if the PLL has converged in the first occurrence;

executing a transition stage by decreasing the initial bandwidth and increasing the initial integration time if the PLL does not have false convergence;

determining whether the PLL has converged in a second occurrence after execution of the transition stage; and

executing a tracking stage by fixing a decreased bandwidth for the PLL and an increased integration time if the PLL has converged in the second occurrence.

2. The method of claim 1, wherein determining whether the PLL has converged comprises:

comparing a change in an average PLL output with a root-mean-square variation of the PLL output.

3. The method of claim 1, further comprising:

returning to executing the transition stage if the PLL has not converged in the second occurrence.

4. The method of claim 1, further comprising:

returning to executing the pull-in stage if the PLL has not converged in the first occurrence.

5. The method of claim 1, further comprising:

determining whether the PLL is set to a last possible setting if the PLL does have false convergence, wherein the last possible setting corresponds to a narrowest bandwidth for the PLL and a maximum integration time; and

using another PLL setting and returning to executing the pull-in stage if the PLL is not set to the last possible setting.

6. The method of claim 5, further comprising:

terminating the method with a tracking failure if the PLL is set to the last possible setting.

7. The method of claim 1, further comprising:

in response to executing the tracking stage, determining whether the PLL is diverging;

returning to executing the pull-in stage if the PLL is diverging; and

returning to executing the tracking stage if the PLL is not diverging.

8. A tracking engine for tracking a Global Positioning Satellite (GPS) signal, the tracking engine comprising:

means for executing a pull-in stage by setting a center frequency of a phase-locked loop (PLL) having an initial bandwidth to a Doppler frequency of the GPS signal;

means for determining whether the PLL has converged in a first occurrence over an initial integration time;

means for determining whether the PLL has false convergence by comparing a power of an in-phase component to a power of a quadrature component of the GPS signal if the PLL has converged in the first occurrence;

means for executing a transition stage by decreasing the initial bandwidth and increasing the initial integration time if the PLL does not have false convergence;

means for determining whether the PLL has converged in a second occurrence after execution of the transition stage; and

means for executing a tracking stage by fixing a decreased bandwidth for the PLL and an increased integration time if the PLL has converged in the second occurrence.

9. The tracking engine of claim 8, wherein the means for determining whether the PLL has converged is to compare a change in an average PLL output with a root-mean-square variation of the PLL output.

10. The tracking engine of claim 8, further comprising:

means for returning to execution of the transition stage if the PLL has not converged in the second occurrence.

11. The tracking engine of claim 8, further comprising:

means for returning to execution of the pull-in stage if the PLL has not converged in the first occurrence.

12. The tracking engine of claim 8, further comprising:

means for determining whether the PLL is set to a last possible setting if the PLL does have false convergence, wherein the last possible setting corresponds to a narrowest bandwidth for the PLL and a maximum integration time; and

means for using another PLL setting and returning to executing the pull-in stage if the PLL is not set to the last possible setting.

13. The tracking engine of claim 12, further comprising:

means for indicating a tracking failure if the PLL is set to the last possible setting.

14. The tracking engine of claim 8, further comprising:

means for determining whether the PLL is diverging in response to executing the tracking stage;

means for returning to execution of the pull-in stage if the PLL is diverging; and

means for returning to execution of the tracking stage if the PLL is not diverging.

15. A Global Positioning Satellite (GPS) receiver for tracking a GPS signal, the GPS receiver comprising:

an antenna to receive the GPS signal; and

a tracking engine to;

execute a pull-in stage by setting a center frequency of a phase-locked loop (PLL) having an initial bandwidth to a Doppler frequency of the GPS signal;

determine whether the PLL has converged in a first occurrence over an initial integration time;

determine whether the PLL has false convergence by comparing a power of an in-phase component to a power of a quadrature component of the GPS signal if the PLL has converged in the first occurrence;

execute a transition stage by decreasing the initial bandwidth and increasing the initial integration time if the PLL does not have false convergence;

determine whether the PLL has converged in a second occurrence after execution of the transition stage; and

execute a tracking stage by fixing a decreased bandwidth for the PLL and an increased integration time if the PLL has converged in the second occurrence.

16. The GPS receiver of claim 15, wherein the tracking engine is to determine whether the PLL has converged by:

comparing a change in an average PLL output with a root-mean-square variation of the PLL output.

17. The GPS receiver of claim 15, wherein the tracking engine is to further:

return to executing the transition stage if the PLL has not converged in the second occurrence.

18. The GPS receiver of claim 15, wherein the tracking engine is to further:

return to executing the pull-in stage if the PLL has not converged in the first occurrence.

19. The GPS receiver of claim 15, wherein the tracking engine is to further:

determine whether the PLL is set to a last possible setting if the PLL does have false convergence, wherein the last possible setting corresponds to a narrowest bandwidth for the PLL and a maximum integration time; and

use another PLL setting and returning to executing the pull-in stage if the PLL is not set to the last possible setting.

20. The GPS receiver of claim 19, wherein the tracking engine is to further:

indicate a tracking failure if the PLL is set to the last possible setting.

21. The GPS receiver of claim 15, wherein the tracking engine is to further:

determine whether the PLL is diverging in response to executing the tracking stage;

return to executing the pull-in stage if the PLL is diverging; and

return to executing the tracking stage if the PLL is not diverging.