CONTINUOUS INTEGRATION BASED SATELLITE NAVIGATIONAL SIGNAL ACQUISITION

• US 20070013583A1
• Filed: 07/12/2005
• Published: 01/18/2007
• Est. Priority Date: 07/12/2005
• Status: Active Grant

• Current Assignee: CSR Technology Holdings Inc. (Qualcomm, Inc.)
• Original Assignee: SiRF Technology Holdings Incorporated (Qualcomm, Inc.)
• Inventors: Wang, Chi-Shin, Wang, Hansheng, Jia, Zhike
• Granted Patent: US 7,180,446 B2
• Time in Patent Office: Days
• US Class Current: 342/357.690
• CPC Class Codes: G01S 19/30 code related G01S19/246 takes precedence

Abstract

A method and device to acquire navigational satellite signals combines non-coherent and coherent integrations and can efficiently acquire both strong and weak signals. Successive steps eliminate lower powered and less likely combinations of code offsets and carrier frequencies or dwells of a given satellite signal. Only remaining dwells then are correlated and integrated over larger time duration to obtain the most probable dwell or dwells, which results in reduced computational load. The selection of most likely dwells is based on Parseval'"'"'s theorem on equivalence of power in time and frequency domains. An optimal estimator algorithm efficiently estimates the probable navigation data bits embedded in the received signal. In case of an ambiguity due to several possible dwells, the steps are repeated with a new set of signal samples.

Claims

1. A method implemented in a global satellite navigation receiver for acquisition of signals received from navigational satellites, the method comprising:

in a coarse acquisition phase;

for a selected dwell in a list of code-frequency dwells, calculating a non-coherent accumulated power from the signals,

if the non-coherent accumulated power is less than a low threshold value then eliminating the selected dwell from the list of code-frequency dwells and continuing the coarse acquisition phase,

if the non-coherent accumulated power is greater than a high threshold then initiating a fine acquisition phase using the selected dwell;

if a number of integration intervals for the selected dwell exceeds a predetermined duration then initiating the fine acquisition phase using the list of code-frequency dwells in the fine acquisition phase;

for a given dwell, calculating a fast Fourier transform of a set of recent signal samples to determine coherent accumulated powers for a set of frequencies, and discarding frequencies whose coherent accumulated powers are less than an average power.

2. The method of claim 1 wherein the average power is calculated from the set of recent signal samples based on Parseval'"'"'s theorem.

3. The method of claim 1 wherein calculating the fast Fourier transform comprises determining navigation data bits using an optimal estimation algorithm.

4. The method of claim 3 wherein the optimal estimation algorithm comprises selecting a data sequence with maximum energy.

5. The method of claim 1 wherein calculating the non-coherent accumulated power comprises adding a square of an in-phase signal component and a square of a quadrature signal component to a prior non-coherent accumulated power.

6. The method of claim 1 wherein the high threshold is equal to the product of a constant power threshold, a number of integration intervals, and a power of a constant attenuation factor.

7. The method of claim 1 wherein the low threshold value is a function of a noise power level in a coherent integration interval.

8. The method of claim 1 further comprising:

if multiple dwells have non-coherent accumulated powers greater than the high threshold, then performing additional integrations to obtain the selected dwell and initiating a fine acquisition phase using the selected dwell.

9. The method of claim 1 further comprising:

if multiple frequencies remain after discarding frequencies whose coherent accumulated powers are less than the average power, then collecting additional signal samples and re-computing the fast Fourier transform.

10. A global satellite navigation system receiver device comprising an RF front end for receiving signals from navigational satellites, a baseband section receiving IF signals from the RF front end, and a processor receiving I,Q signal samples from the baseband section, wherein the processor implements a two-phase signal acquisition process comprising a coarse acquisition phase and a fine acquisition phase,

wherein the coarse acquisition phase comprises:

for a selected dwell in a list of code-frequency dwells, calculating a non-coherent accumulated power from the signals,

if the non-coherent accumulated power is less than a low threshold value then eliminating the selected dwell from the list of code-frequency dwells and continuing the coarse acquisition phase,

if the non-coherent accumulated power is greater than a high threshold then initiating a fine acquisition phase using the selected dwell;

if a number of integration intervals for the selected dwell exceeds a predetermined duration then initiating the fine acquisition phase using the list of code-frequency dwells wherein the fine acquisition phase comprises;

for a given dwell, calculating a fast Fourier transform of a set of recent signal samples to determine coherent accumulated powers for a set of frequencies, and

discarding frequencies whose coherent accumulated powers are less than an average power.

11. The device of claim 10 wherein the average power is calculated from the set of recent signal samples based on Parseval'"'"'s theorem.

12. The device of claim 10 wherein calculating the fast Fourier transform comprises determining navigation data bits using an optimal estimation algorithm.

13. The device of claim 12 wherein the optimal estimation algorithm comprises selecting a data sequence with maximum energy.

14. The device of claim 10 wherein calculating the non-coherent accumulated power comprises adding a square of an in-phase signal component and a square of a quadrature signal component to a prior non-coherent accumulated power.

15. The device of claim 10 wherein the high threshold is equal to the product of a constant power threshold, a number of integration intervals, and a power of a constant attenuation factor.

16. The device of claim 10 wherein the low threshold value is a function of a noise power level in a coherent integration interval.

17. The device of claim 10 further comprising:

if multiple dwells have non-coherent accumulated powers greater than the high threshold, then performing additional integrations to obtain the selected dwell and initiating a fine acquisition phase using the selected dwell.

18. The device of claim 10 further comprising:

if multiple frequencies remain after discarding frequencies whose coherent accumulated powers are less than the average power, then collecting additional signal samples and re-computing the fast Fourier transform.