SYSTEM AND METHOD FOR CORRECTING GLOBAL NAVIGATION SATELLITE SYSTEM PSEUDORANGE MEASUREMENTS IN RECEIVERS HAVING CONTROLLED RECEPTION PATTERN ANTENNAS

• US 20110050489A1
• Filed: 08/26/2009
• Published: 03/03/2011
• Est. Priority Date: 08/26/2009
• Status: Active Grant

• Current Assignee: Raytheon Company (Rtx Corporation)
• Original Assignee: Raytheon Company (Rtx Corporation)
• Inventors: Maenpa, Jon E., Sain, Patrick M., Hautzik, Andrew M.
• Granted Patent: US 8,044,857 B2
• Time in Patent Office: Days
• US Class Current: 342/357.23
• CPC Class Codes: G01S 19/23 Testing, monitoring, correcting or calibrating of receiver elements

Abstract

Global Navigation Satellite System (GNSS) pseudorange measurements are compensated for receiver hardware and directionally dependent antenna errors to obtain desired accuracies for high precision GNSS positioning applications using a multiple element controlled reception pattern antenna (CRPA). Pseudorange errors are calibrated and stored in a sky map by azimuth, elevation, radio frequency (RF) channel, and frequency. Corrections are applied in real time to each pseudorange measurement by applying a combination of the stored errors. The coefficients of the errors in the combination are computed as a function of steering vectors and CRPA filter weights. This implements a generalized pseudorange correction able to compensate a GNSS CRPA sensor for channel dependent errors such as group delay for both the case of uniform weights for all frequencies and the more complex case of frequency-dependent weights.

Claims

1. An apparatus for calibrating a global navigation satellite system (GNSS) receiver system for group delay errors in GNSS transmitter signals, the apparatus comprising:

a controlled reception pattern antenna (CRPA) comprising a plurality of receiving elements and configured to sense a plurality of signals from a plurality of GNSS transmitters using one or more transmitter frequencies;

a signal conditioner configured to convert a plurality of sensed GNSS signals to a plurality of time domain digital signals;

a processor configured to;

convert the time domain digital signals into a plurality of filtered signals using a plurality of signal weights;

access group delay calibration correction data for combinations of the plurality of receiving elements, a plurality of transmitter orientations with respect to the CRPA, and the one or more transmitter frequencies;

track code modulations of the plurality of filtered signals and convert the filtered signals into GNSS pseudorange measurements for the plurality of GNSS transmitters at the one or more transmitter frequencies;

combine the group delay calibration correction data and the signal weights to generate weighted pseudorange error corrections for the plurality of GNSS transmitters at the one or more transmitter frequencies; and

combine the weighted pseudorange error corrections and the GNSS pseudorange measurements to generate corrected pseudorange measurements for the plurality of GNSS transmitters at the one or more transmitter frequencies.

2. The apparatus of claim 1, wherein the processor is further configured to:

track the code modulations of the plurality of filtered signals and convert the filtered signals into pseudorange measurements by using a plurality of delay-locked loops; and

determine the transmitter orientation with respect to the CRPA for each of the plurality of GNSS transmitters by obtaining a directional angle from the CRPA to each of the plurality of GNSS transmitters, obtaining an attitude of the CRPA, and combining the directional angle from the CRPA and the attitude of the CRPA for each of the plurality of GNSS transmitters.

3. The apparatus of claim 2, wherein the GNSS uses two or more transmitter frequencies and the group delay calibration correction data is further organized by the two or more transmitter frequencies.

4. The apparatus of claim 2, wherein the processor is further configured to:

generate frequency-independent signal weights; and

combine the group delay calibration correction data and the frequency-independent signal weights to generate the weighted pseudorange error corrections for the plurality of GNSS transmitters at the one or more transmitter frequencies.

5. The apparatus of claim 2, wherein the processor is further configured to:

convert the time domain digital signals to frequency domain digital signals;

compute frequency-dependent signal weights from the frequency domain digital signals; and

combine the group delay calibration correction data and the frequency-independent signal weights to generate weighted pseudorange error corrections for the plurality of GNSS transmitters at the one or more transmitter frequencies.

6. The apparatus of claim 2, wherein the apparatus is configured to perform in real time.

7. The apparatus of claim 2, wherein the GNSS is Global Positioning System (GPS).

8. The apparatus of claim 2, wherein the CRPA has seven elements.

9. The apparatus of claim 2, wherein the apparatus is mounted on a static platform.

10. The apparatus of claim 2, wherein the apparatus is mounted on a dynamic platform.

11. The apparatus of claim 10, wherein the apparatus is mounted on an aircraft, ship, or land vehicle and wherein the apparatus determines the corrected pseudorange measurements accounting for the variable attitude of the dynamic platform.

12. A method for calibrating a global navigation satellite system (GNSS) receiver system for group delay errors in GNSS transmitter signals, the method comprising:

sensing a plurality of signals from a plurality of GNSS transmitters with a controlled reception pattern antenna (CRPA) comprising a plurality of receiving elements using one or more transmitter frequencies;

converting the plurality of sensed GNSS signals to a plurality of time domain digital signals;

converting the time domain digital signals into a plurality of filtered signals using a plurality of signal weights;

accessing group delay calibration correction data for combinations of the plurality of receiving elements, a plurality of transmitter orientations with respect to the CRPA, and the one or more transmitter frequencies;

tracking code modulations of the plurality of filtered signals and converting the filtered signals into GNSS pseudorange measurements for the plurality of GNSS transmitters at the one or more transmitter frequencies;

combining the group delay calibration correction data and the signal weights to generate weighted pseudorange error corrections for the plurality of GNSS transmitters at the one or more transmitter frequencies; and

combining the weighted pseudorange error corrections and the GNSS pseudorange measurements to generate corrected pseudorange measurements for the plurality of GNSS transmitters at the one or more transmitter frequencies.

13. The method of claim 12, further comprising:

determining the transmitter orientation with respect to the CRPA for each of the plurality of GNSS transmitters by obtaining a directional angle from the CRPA to each of the plurality of GNSS transmitters, obtaining an attitude of the CRPA, and combining the directional angle from the CRPA and the attitude of the CRPA for each of the plurality of GNSS transmitters,

wherein the tracking the code modulations of the plurality of filtered signals and converting the filtered signals into pseudorange measurements comprises using a plurality of delay-locked loops.