Local clock frequency calibration using low earth orbit (LEO) satellites

• US 7,859,455 B2
• Filed: 01/06/2009
• Issued: 12/28/2010
• Est. Priority Date: 01/06/2009
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Ferrell, Barton G., Gutt, Gregory M., Whelan, David A., Brumley, Robert W., Martens, Christopher J., Haddad, Anne T.
• Primary Examiner(s): Tarcza; Thomas H
• Assistant Examiner(s): GALT, CASSI J
• Application Number:
  US12/349,362
• Publication Number:
  US 20100171652A1
• Time in Patent Office: 721 Days
• Field of Search: 342/342.69, 342/357.16, 342/357.62, 342/357.64
• US Class Current: 342/357.62
• CPC Class Codes: G01S 19/235 Calibration of receiver components

Abstract

Various techniques are provided for calibrating a frequency of a local clock using a satellite signal. In one example, a method of transferring frequency stability from a satellite to a device includes receiving a signal from the satellite. The method also includes determining a code phase from the satellite signal. The method further includes receiving aiding information. In addition, the method includes calibrating a frequency of a local clock of the device using the code phase and the aiding information to substantially synchronize the local clock frequency with a satellite clock frequency.

Claims

1. A method of transferring frequency stability from a satellite to a device, the method comprising:

receiving a signal from the satellite;

determining a code phase from the satellite signal, wherein;

the satellite is a low earth orbit (LEO) satellite having a clock frequency,

the signal comprises a plurality of message frames each having an ordinal number, and at least one time transfer structure message having a unique pseudorandom code, and

the code phase corresponds to the ordinal number of the message frame whose time transfer structure message is identified through its unique pseudorandom code;

receiving aiding information; and

calibrating a frequency of a local clock of the device to substantially synchronize the local clock frequency with the satellite clock frequency, wherein the calibrating comprises measuring a frequency of the satellite signal using the code phase and the aiding information.

2. The method of claim 1, wherein:

the calibrating comprises correcting the local clock frequency to compensate for a Doppler shift associated with relative motion of the satellite and the device.

3. The method of claim 1, wherein the calibrating comprises:

correcting the measured frequency of the satellite signal to compensate for a Doppler shift associated with relative motion of the satellite and the device;

determining the satellite clock frequency; and

generating a frequency correction for the local clock frequency using the satellite clock frequency and the corrected measured frequency of the satellite signal.

4. The method of claim 1, wherein:

the satellite signal comprises a plurality of message frames, wherein each message frame comprises a time transfer structure message.

5. The method of claim 4, wherein:

each message frame further comprises payload bits associated with communication data.

6. The method of claim 4, wherein:

the determining the code phase comprises identifying a code that is unique for each of the time transfer structure messages of at least one of the message frames.

7. The method of claim 6, wherein:

the code is a binary code having a code set, wherein cross-correlation between distinct members of the code set is relatively low and auto-correlation for each individual member of the code set is relatively high.

8. The method of claim 1, wherein:

the aiding information comprises satellite orbit information.

9. The method of claim 1, further comprising:

using the calibrated local clock frequency to lock onto a Global Positioning System (GPS) signal; and

determining a position of the device using the GPS signal.

10. The method of claim 1, wherein:

the calibrating comprises calculating a range rate from an orbital model of the LEO satellite and an approximate location of the device.

11. A receiver unit comprising:

an antenna adapted to receive a signal from a satellite, wherein;

the satellite is a low earth orbit (LEO) satellite having a clock frequency, and

the signal comprises a plurality of message frames each having an ordinal number, and at least one time transfer structure message having a unique pseudorandom code;

a local clock;

an analog-to-digital (A/D) converter adapted to sample data from the time transfer structure message in the satellite signal;

a memory adapted to store aiding information; and

a computer adapted to determine a code phase using the sampled data, wherein;

the code phase corresponds to the ordinal number of the message frame whose time transfer structure message is identified through its unique pseudorandom code, and

the computer is further adapted to measure a frequency of the satellite signal using the code phase and the aiding information to determine a frequency correction for the local clock to substantially synchronize the local clock frequency with the clock frequency of the satellite.

12. The receiver unit of claim 11, wherein:

the frequency correction includes a Doppler frequency correction to the measured frequency of the satellite signal to compensate for a Doppler shift associated with relative motion of the satellite and the receiver unit.

13. The receiver unit of claim 11, wherein:

the aiding information comprises ephemeredes for the satellite orbit; and

the aiding information comprises an approximate location of the receiver unit.

14. The receiver unit of claim 11, wherein:

the time transfer structure message comprises a binary code having a code set, wherein cross-correlation between distinct members of the code set is relatively low, auto-correlation for each individual member of the code set is relatively high, and each member of the code set uniquely identifies a message frame of the time transfer structure message.

15. The receiver unit of claim 11, wherein:

the identity of the message frame determines a code phase; and

the aiding information includes a time slot offset and a distance from the satellite to the receiver unit.