Scanning correlator for global navigation satellite system signal tracking

• US 9,515,697 B2
• Filed: 03/30/2015
• Issued: 12/06/2016
• Est. Priority Date: 03/30/2015
• Status: Expired due to Fees

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Raasakka, Jussi, Orejas, Martin, Kutik, Ondrej, Skalicky, Jakub
• Primary Examiner(s): Wong, Linda
• Application Number:
  US14/672,569
• Publication Number:
  US 20160294438A1
• Time in Patent Office: 617 Days
• Field of Search: 375/130, 375/140, 375/146, 375/142, 375/147, 375/148, 375/149, 375/150, 375/141, 375/219, 375/220, 375/221, 375/222, 37524026-24028, 375/259, 375/267, 375/278, 375/285, 375/284, 375/295, 375/302, 375/307, 375/306, 375/304, 375/309, 375/316, 375/322, 375/324, 375/325, 375/326, 375/327, 375/328, 375/338, 375/339, 375/340, 375/343, 375/346, 375/347, 375/349, 375/354, 375/359, 375/360, 375/362, 375/364, 375/365, 375/371, 375/373, 375/374, 375/375, 375/376, 455/3.02, 455/3.01, 455/427, 455/404.2, 455/440, 455/441, 455/456.1, 455/456.3, 455/456.5, 455/456.6, 455/457, 455/12.1, 455/91, 455/98, 455/95, 455/39, 455/500
• US Class Current: 1/1
• CPC Class Codes: G01S 19/22 Multipath-related issues
• CPC Class Codes: G01S 19/26 involving a sensor measurement for aiding acquisition or tracking
• CPC Class Codes: G01S 19/29 carrier including Doppler, related G01S19/246 takes precedence
• 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: H04B 1/709 Correlator structure

Abstract

Systems and methods for a scanning correlator for global navigation satellite system signal tracking are provided. In one embodiment, a method for Global Navigation Satellite System (GNSS) receiver tracking comprises: receiving a GNSS navigation signal; generating a local Pseudo Random Noise (PRN) sequence; sampling the GNSS navigation signal over a plurality of integration periods to produce a plurality of scanning values, wherein each scanning value has a respective time offset such that at least one first time offset is not equal to at least one second time offset; estimating at least two points of an autocorrelation function for the GNSS navigation signal based on the plurality of scanning values; and calculating an alignment between the GNSS signal and the local PRN sequence based on the autocorrelation function estimate.

Claims

1. A Global Navigation Satellite System (GNSS) receiver, the receiver comprising:

a front end configured to receive GNSS signals;

a code and carrier remover coupled to the front end;

a carrier numerically controlled oscillator coupled to the code and carrier remover and generating a first oscillating signal,

a code numerically controlled oscillator coupled to the code and carrier remover and generating a second oscillating signal,

wherein the code and carrier remover comprises;

a carrier remover configured to down convert a received GNSS signal based on the first oscillating signal,

a correlator block comprising at least a scanning correlator; and

a Pseudo Random Noise generator coupled to the correlator block, the Pseudo Random Noise generator producing a local Pseudo Random Noise sequence based at least in part on the second oscillating signal,

wherein the scanning correlator is configured to estimate at least two points of an autocorrelation function of the received GNSS signal based on a plurality of scanning values derived from sampling the received GNSS signal, wherein the at least two points of the autocorrelation function are based on scanning values of the plurality of scanning values that are captured during different integration periods, wherein each scanning value of the plurality of scanning values has a respective time offset variably controlled such that at least one first time offset of the plurality of scanning values is not equal to at least one second time offset of the plurality of scanning values;

wherein the scanning correlator calculates an alignment between the received GNSS signal and the Pseudo Random Noise sequence based on the autocorrelation function estimate; and

a control block coupled to the code numerically controlled oscillator and the carrier numerically controlled oscillator;

wherein the correlator block further includes a reference correlator that generates a second value by processing the received GNSS signal; and

wherein the respective time offset for each scanning value of the plurality of scanning values is varied by the control block either forward or backward by a fraction of a code chip with respect to a fixed reference point provided by a time offset of the reference correlator.

2. The receiver of claim 1, wherein the control block controls the first oscillating signal and the second oscillating signal based on feedback from the correlator block.

3. The receiver of claim 2, wherein the feedback from the correlator block is based on the plurality of scanning values.

4. The receiver of claim 1, wherein the carrier remover comprises a mixer that downconverts the received GNSS signal from an Intermediate Frequency to a Baseband frequency based on the first oscillating signal.

5. The receiver of claim 1, wherein a difference between the at least one first time offset and the at least one second time offset is at least one of the following:

+/−

0.5 chips, +/−

0.1 chips or +/−

0.01 chips.

6. The receiver of claim 1, wherein the respective time offsets of the plurality of scanning values together span a span duration of at least one of the following:

1 chip, 2 chips, 3 chips, 4 chips, 5 chips or 6 chips.

7. The receiver of claim 1, wherein the plurality of scanning values are normalized with respect to a scanning value that has the greatest magnitude.

8. The receiver of claim 1, wherein the reference correlator comprises a prompt correlator that generates a prompt value by processing the received GNSS signal.

9. The receiver of claim 8, wherein the plurality of scanning values are normalized with respect to the prompt values.

10. A method for Global Navigation Satellite System (GNSS) receiver tracking, the method comprising:

receiving a GNSS navigation signal;

generating a local Pseudo Random Noise (PRN) sequence;

sampling the GNSS navigation signal over a plurality of integration periods to produce a plurality of scanning values, wherein each scanning value of the plurality of scanning values has a respective time offset variably controlled by a control block such that at least one first time offset is not equal to at least one second time offset;

estimating at least two points of an autocorrelation function for the GNSS navigation signal based on scanning values of the plurality of scanning values captured during different integration periods;

calculating an alignment between the GNSS signal and the local PRN sequence based on the autocorrelation function estimate; and

applying the received GNSS signal to a reference correlator to generate a second value;

wherein the respective time offset for each scanning value of the plurality of scanning values is varied by the control block either forward or backward by a fraction of a code chip with respect to a fixed reference point provided by a time offset of the reference correlator.

11. The method of claim 10, further comprising:

adjusting a chip rate of the local PRN sequence based on the calculated alignment.

12. The method of claim 10, further comprising:

wherein the plurality of scanning values are calculated at least in part based on the local PRN sequence.

13. The method of claim 10, further comprising:

converting the received GNSS signal from an Intermediate Frequency to a Baseband frequency.

14. The method of claim 10, wherein a difference between the at least one first time offset and the at least one second time offset is at least one of the following:

+/−

0.5 chips, +/−

0.1 chips or +/−

0.01 chips.

15. The method of claim 10, wherein the respective time offsets of the scanning values together span a span duration at least one of the following:

1 chip, 2 chips, 3 chips, 4 chips, 5 chips or 6 chips.

16. The method of claim 10, further comprising normalizing the plurality of scanning values with respect to a scanning value that has the greatest magnitude.

17. The method of claim 10, wherein the reference correlator comprises a prompt correlator that generates a prompt value by processing the received GNSS signal.

18. The method of claim 17, wherein the plurality of scanning values are normalized with respect to the prompt value.