GPS GYRO CALIBRATION

• US 20100013703A1
• Filed: 05/25/2006
• Published: 01/21/2010
• Est. Priority Date: 05/25/2006
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Tekawy, Jonathan A., O'Brien, Kevin M.
• Granted Patent: US 7,667,645 B2
• Time in Patent Office: Days
• US Class Current: 342/357.395
• CPC Class Codes: G01S 19/02 Details of the space or ground control segments
• CPC Class Codes: G01S 19/11 wherein the cooperating elements are pseudolites or satellite radio beacon positioning system signal repeaters
• CPC Class Codes: H01Q 3/267 Phased-array testing or checking devices

Abstract

GPS gyro calibration methods and systems are described. In an embodiment, a ground station can receive antenna position data for a spot beam antenna from a global positioning system (GPS) platform where the antenna position data indicates a boresight direction of the spot beam antenna. GPS-enabled receiver(s) can receive scan signals transmitted via the spot beam antenna of the GPS platform, and the GPS-enabled receivers can determine signal power measurements for each of the scan signals. The ground station can receive the signal power measurements from the GPS-enabled receiver(s) and estimate a pointing error of the spot beam antenna based on the signal power measurements and the antenna position data received from the GPS platform. The ground station can then determine gyro calibration parameters from the estimated pointing error and communicate the gyro calibration parameters to the GPS platform to calibrate for gyro drift errors.

Claims

1. A method comprising:

receiving, in a GPS enabled receiver, scan signals transmitted via a spot beam antenna of a global positioning system (GPS) platform;

determining, in the GPS enabled receiver, one or more signal power measurements of each of the scan signals; and

communicating the signal power measurements from the GPS enabled receiver to a ground station that (i) estimates a pointing error of the spot beam antenna based on the signal power measurements and antenna position data received from the GPS platform, wherein the estimated pointing error includes the difference between where the signal power measurement is measured and where it was expected to be, (ii) determines gyro calibration parameters from the estimated pointing error, and (iii) communicates the gyro calibration parameters to the GPS platform to calibrate for gyro drift errors, wherein the gyro calibration parameters include information to correct for the gyro rate output and to provide accurate rate and attitude estimates, wherein the corrected gyro estimates are used to accurately point the spot beam antenna and a GPS earth coverage antenna.

2. A method as recited in claim 1, wherein the scan signals are received at the GPS enabled receiver which includes at least one of:

a stationary GPS enabled receiver;

a mobile GPS enabled receiver;

multiple GPS enabled receivers.

3. A method as recited in claim 1, further comprising, time-tagging the scan signals when received at the GPS enabled receiver for the ground station to correlate the signal power measurements of each of the scan signals with the antenna position data to estimate the pointing error of the spot beam antenna.

4. A method as recited in claim 1, wherein the scan signals are transmitted from the GPS platform with a known amplitude, and wherein the scan signals are received in a pattern of a predetermined scan profile, wherein the pattern of a predetermined scan profile being the GPS platform slewing the spot beam antenna across one or more of the GPS enabled receivers in a cross scan pattern, wherein the slewing performed at a low rate in azimuth and elevation coordinate frames utilizing a scan pattern that produces a measurable change in signal-to-noise ratio measurements.

5. A method as recited in claim 1, wherein the signal power measurements are determined as signal-to-noise ratio measurements at the GPS enabled receiver, wherein the difference between where a signal-to-noise ratio is measured and where it is expected to be provides an estimate of the pointing error.

6. A method as recited in claim 1, wherein the gyro calibration parameters include a rate bias and a scale factor communicated to the GPS platform which calibrates for the gyro drift errors, wherein the pointing error is input to a Kalman filter algorithm to estimate the gyro calibration parameters to calibrate for the gyro drift errors, wherein the pointing error is based on the difference between where a signal-to-noise ratio is measured and where it is expected to be.

7. A method comprising:

receiving, at a ground station, antenna position data for a spot beam antenna from a global positioning system (GPS) platform, the antenna position data indicating a boresight direction of the spot beam antenna;

receiving, at the ground station, signal power measurements from one or more GPS enabled receivers that each configured to receive scan signals transmitted via the spot beam antenna of the GPS platform, the signal power measurements being determined, by the one or more GPS enabled receivers, for each of the scan signals;

estimating, at the ground station, a pointing error of the spot beam antenna based on the signal power measurements and the antenna position data received from the GPS platform, wherein the estimated pointing error includes the difference between where the signal power measurement is measured and where it was expected to be;

determining gyro calibration parameters from the estimated pointing error; and

communicating the gyro calibration parameters, from the ground station, to the GPS platform to calibrate for gyro drift errors, the gyro calibration parameters including information to correct for the gyro rate output and to provide accurate rate and attitude estimates usable to accurately point the spot beam antenna and a GPS earth coverage antenna.

8. A method as recited in claim 7, further comprising correlating the signal power measurements that each correspond to a received scan signal with the antenna position data based on time indications that are assigned to each scan signal received by a GPS enabled receiver.

9. A method as recited in claim 7, wherein the signal power measurements are received from a GPS enabled receiver that includes at least one of:

a stationary GPS enabled receiver;

a mobile GPS enabled receiver.

10. A method as recited in claim 7, further comprising determining a corrected boresight direction of the spot beam antenna from the gyro calibration parameters.

11. A method as recited in claim 7, wherein the gyro calibration parameters include a rate bias and a scale factor communicated to the GPS platform which calibrates for the gyro drift errors.

12. A method as recited in claim 7, wherein the signal power measurements are received from the one or more GPS enabled receivers as signal-to-noise ratio measurements.

13. A method as recited in claim 7, wherein the scan signals are transmitted via the spot beam antenna of the GPS platform to the one or more GPS enabled receivers in a pattern of a pre determined scan profile that corresponds to the antenna position data of the spot beam antenna.

14. A method comprising:

communicating antenna position data for a spot beam antenna of a global positioning system (GPS) platform to a ground station, the antenna position data indicating a boresight direction of the spot beam antenna;

transmitting scan signals to one or more GPS enabled receivers via the spot beam antenna of the GPS platform, the one or more GPS enabled receivers each being configured to determine signal power measurements for each of the scan signals, assign a time-tag to each scan signal when received, correlate the signal power measurements that each correspond to a received scan signal with the antenna position data based on the time-tag that is assigned to each scan signal received by the GPS enabled receiver and communicate the signal power measurements to the ground station that (i) estimates a pointing error of the spot beam antenna based on the signal power measurements and the antenna position data received from the GPS platform, and (ii) determines gyro calibration parameters from the estimated pointing error;

receiving the gyro calibration parameters from the ground station; and

calibrating for gyro drift errors in the GPS platform.

15. A method as recited in claim 14, wherein the scan signals are transmitted to a GPS enabled receiver that includes at least one of:

a stationary GPS enabled receiver;

a mobile GPS enabled receiver.

16. A method as recited in claim 14, wherein the scan signals being transmitted to the one or more GPS enabled receivers with a known amplitude and in a pattern of a pre-determined scan profile, the pattern of the predetermined scan profile being defined by the GPS platform slewing the spot beam antenna across one or more of the GPS enabled receivers in a cross-scan pattern, the slewing performed at a low rate in azimuth, and elevation coordinate frames utilizing a scan pattern that produces a measurable change in signal-to-noise ratio measurements.

17. A method as recited in claim 14, wherein the one or more GPS enabled receivers each determine the signal power measurements for the scan signals as signal-to-noise ratio measurements that are communicated to the ground station.

18. A method as recited in claim 14, wherein a rate bias and a scale factor are received as the gyro calibration parameters from the ground station to calibrate for the gyro drift errors in the GPS platform.

19. A method as recited in claim 14, further comprising determining a corrected boresight direction of the spot beam antenna from the gyro calibration parameters.

20. (canceled)