System and method for GNSS position aided signal acquisition

• US 8,106,822 B2
• Filed: 02/19/2008
• Issued: 01/31/2012
• Est. Priority Date: 02/19/2008
• Status: Expired due to Fees

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Schipper, Brian, Ariyur, Kartik B.
• Primary Examiner(s): Issing, Gregory C
• Application Number:
  US12/033,822
• Publication Number:
  US 20090207076A1
• Time in Patent Office: 1,442 Days
• Field of Search: 342/357.15, 342/357.63
• 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

A Global Navigation Satellite System (GNSS) device, such as the Global Positioning System (GPS) device, uses satellite orbital position information from almanac and/or ephemeris data to change a search parameter, such as reducing the number of analyzed frequency bins or setting signal strength threshold, so that satellite signal acquisition times are reduced. An exemplary embodiment estimates an orbital position for at least one GNSS satellite based upon at least one of almanac data and ephemeris data, detects a signal emitted from the at least one GNSS satellite, and based upon the estimated orbital position information for the at least one GNSS satellite that is determined from the almanac data and the ephemeris data, adjusts at least one parameter used in the analysis of the detected signal.

Claims

1. A method for acquiring a Global Navigation Satellite System (GNSS) signal, the method comprising:

estimating an orbital position for at least one GNSS satellite based upon at least one of almanac data and ephemeris data;

detecting a signal emitted from the at least one GNSS satellite; and

based upon the estimated orbital position information for the at least one GNSS satellite, adjusting at least one signal threshold used in a GNSS satellite signal acquisition process in a navigational system processor;

wherein the at least one signal threshold is one of a signal strength threshold or a signal-to-noise ratio threshold.

2. The method of claim 1, further comprising:

selecting at least one frequency bin associated with a Fourier analysis of the signal such that the selected frequency bin is used in the GNSS satellite signal acquisition process, the selection of the at least one frequency bin based upon the estimated orbital position information for the at least one GNSS satellite.

3. The method of claim 1, further comprising:

deselecting at least one frequency bin associated with a Fourier analysis of the signal such that the deselected frequency bin is not used in the GNSS satellite signal acquisition process the deselection of the at least one frequency bin based upon the estimated orbital position information for the at least one GNSS satellite.

4. The method of claim 1, wherein adjusting at least one signal threshold further comprises:

based upon the estimated orbital position information for the at least one GNSS satellite, estimating a characteristic of the detected signal; and

adjusting the at least one signal threshold based upon the estimated characteristic, wherein the method further comprises;

identifying at least one frequency bin having a corresponding signal characteristic that corresponds to the adjusted signal threshold such that the identified frequency bin is used in the GNSS satellite signal acquisition process.

5. The method of claim 1, wherein adjusting at least one signal threshold further comprises:

based upon the estimated orbital position information for the at least one GNSS satellite, estimating a signal-to-noise ratio of a signal emitted by the at least one GNSS satellite; and

adjusting the signal-to-noise ratio threshold based upon the estimated signal-to-noise ratio, wherein the method further comprises;

identifying at least one frequency bin having a corresponding signal-to-noise ratio that is greater than the adjusted signal-to-noise ratio threshold such that the identified at least one frequency bin is used in the GNSS satellite signal acquisition process.

6. The method of claim 1, wherein adjusting at least one signal threshold further comprises:

based upon the estimated orbital position information for the at least one GNSS satellite, estimating a signal strength of the detected signal; and

adjusting the signal strength threshold based upon the estimated signal strength, wherein the method further comprises;

identifying at least one frequency bin having a corresponding signal strength that corresponds to the adjusted signal strength threshold such that the identified frequency bin is used in the GNSS satellite signal acquisition process.

7. The method of claim 1, wherein estimating the orbital position for the at least one GNSS satellite based upon at least one of the almanac data and the ephemeris data comprises:

estimating a coarse satellite orbital position based upon the almanac data.

8. The method of claim 1, wherein estimating the orbital position for the at least one GNSS satellite based upon at least one of the almanac data and the ephemeris data comprises:

estimating a high accuracy satellite orbital position based upon the ephemeris data.

9. The method of claim 1, wherein estimating the orbital position for the at least one GNSS satellite based upon at least one of the almanac data and the ephemeris data comprises;

estimating a coarse satellite orbital position based upon the almanac data; and

after estimation of the coarse satellite orbital position, estimating a high accuracy satellite orbital position based upon the ephemeris data.

10. The method of claim 1 further comprising:

adjusting a frequency range of a frequency bin based upon the estimated orbital position information for the at least one GNSS satellite.

11. The method of claim 1 further comprising:

adjusting a time range of a frequency bin based upon the estimated orbital position information for the at least one GNSS satellite.

12. The method of claim 1, further comprising:

receiving the almanac data from a local memory.

13. The method of claim 1, further comprising:

receiving the almanac data from a satellite signal prior to estimating the orbital position for the at least one GNSS satellite.

14. An apparatus that is configured to acquire a Global Positioning System (GNSS) signal, comprising:

a GNSS front end -configured to receive a GNSS signal emitted by at least one GNSS satellite and configured to frequency downconvert the GNSS signal into a downconverted GNSS satellite signal by mixing the GNSS satellite signal with a local oscillator signal to shift the carrier frequency of the incoming GNSS satellite signal; and

a GNSS system processor communicatively coupled to the GNSS front end and configured to;

receive the downconverted GNSS satellite signal from the GNSS front end;

convert the downconverted GNSS satellite signal to a digital GNSS satellite signal;

process the digital GNSS satellite signal into a plurality of frequency bins;

estimate an orbital position for at least one GNSS satellite based upon at least one of almanac data and ephemeris data;

based upon the estimated orbital position information for the at least one GNSS satellite, adjust at least one signal threshold used in a GNSS satellite signal acquisition process; and

based upon the adjusted signal threshold, identify at least one of the frequency bins that corresponds to the GNSS signal emitted by the GNSS satellite;

wherein the signal threshold is one of a signal strength threshold or a signal-to-noise ratio threshold.

15. The apparatus of claim 14, wherein based upon the adjusted signal threshold, the processing system is configured to select a plurality of the frequency bins such that the selected frequency bins are used in the GNSS satellite signal acquisition process.

16. The apparatus of claim 14, wherein based upon the adjusted signal threshold, the processing system is configured to deselect a plurality of frequency bins such that the deselected frequency bins are not used in the GNSS satellite signal acquisition process.

17. The apparatus of claim 14, wherein, the processing system is configured to:

estimate a signal-to-noise ratio corresponding to the received GNSS signal emitted by the at least one GNSS satellite;

adjust the signal-to-noise ratio threshold based upon the estimated signal-to-noise ratio; and

identify at least one frequency bin having a corresponding signal-to-noise ratio that is greater than the adjusted signal-to-noise ratio threshold such that the identified at least one frequency bin is used in the GNSS satellite signal acquisition process.

18. The apparatus of claim 14, wherein, the processing system is configured to:

estimate a signal strength corresponding to the received GNSS signal emitted by the at least one GNSS satellite;

adjust the signal strength threshold based upon the estimated signal strength; and

identify at least one frequency bin having a corresponding signal strength that corresponds to the adjusted signal strength threshold such that the identified frequency bin is used in the GNSS satellite signal acquisition process.

19. The apparatus of claim 14, wherein the processing system is configured to estimate a coarse satellite orbital position based upon the almanac data.

20. The apparatus of claim 19, wherein the processing system is configured to, after estimation of the coarse satellite orbital position, estimate a high accuracy satellite orbital position based upon the ephemeris data.