Precise absolute time transfer from a satellite system

• US 8,542,147 B2
• Filed: 10/06/2011
• Issued: 09/24/2013
• Est. Priority Date: 05/30/2008
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Whelan, David A., Gutt, Gregory M.
• Primary Examiner(s): Phan, Dao
• Application Number:
  US13/267,714
• Publication Number:
  US 20120218147A1
• Time in Patent Office: 719 Days
• Field of Search: 342/357.22, 342/357.39, 342/357.42, 342/357.63, 701/468, 701/470
• US Class Current: 342/357.63
• CPC Class Codes: G01S 19/05 providing aiding data
• CPC Class Codes: G01S 19/21 Interference related issues ; Issues related to cross-correlation, spoofing or other methods of denial of service
• CPC Class Codes: G01S 19/23 Testing, monitoring, correcting or calibrating of receiver elements
• CPC Class Codes: G01S 19/256 relating to timing, e.g. time of week, code phase, timing offset

Abstract

Various techniques are provided for obtaining a precise absolute time using a satellite system. In one example, a method of transferring precise absolute time from a satellite to a device includes receiving data from a messaging channel, wherein the data has a frame structure. The method also includes using the data to identify the satellite and a position of the satellite, correcting for signal time of flight using the satellite identity and the position, and using the data as a time reference to align a receiver clock to the frame structure. The method also includes, with the receiver clock aligned to the frame structure, receiving a precision time signal from the satellite, wherein the precision time signal comprises a periodic repeating code. The method also includes determining a timing phase of the code and using the timing phase to determine a precise absolute time.

Claims

1. A method of transferring precise absolute time from a satellite to a device, the method comprising:

receiving data from a messaging channel, wherein the data has a frame structure;

using the data to identify the satellite and a position of the satellite;

correcting for signal time of flight using the satellite identity and the position of the satellite;

using the data as a time reference to align a receiver clock to the frame structure;

with the receiver clock aligned to the frame structure, receiving a precision time signal from the satellite, wherein the precision time signal comprises a periodic repeating code;

determining a timing phase of the code; and

using the timing phase to determine a precise absolute time.

2. The method of claim 1, further comprising:

receiving the data from the messaging channel in response to an acquisition channel being unavailable, wherein the messaging channel is distinct from the acquisition channel.

3. The method of claim 1, wherein:

the messaging channel is one of a plurality of messaging channels carrying the data.

4. The method of claim 1, wherein:

the messaging channel is one of a plurality of messaging channels carrying the data and for which a priori acquisition information is possessed by the receiver.

5. The method of claim 1, wherein:

the messaging channel is one of a plurality of distinct messaging channels carrying the data from the same satellite.

6. The method of claim 1, wherein:

the messaging channel is one of a plurality of messaging channels carrying the data;

at least one of the messaging channels carries data from a different satellite from the satellite; and

the satellite and the different satellite are in the same satellite constellation.

7. The method of claim 1, wherein:

the messaging channel is one of a plurality of messaging channels carrying the data;

at least one of the messaging channels carries data from a different satellite from the satellite; and

the satellite and the different satellite are in different satellite constellations.

8. The method of claim 1, wherein:

the frame structure is an L band frame structure; and

the data includes an L band frame count (LBFC).

9. The method of claim 1, wherein the data includes at least one of X, Y, and Z coordinates for the position of the satellite or a satellite vehicle identification (SVID) of the satellite.

10. The method of claim 1, wherein:

the messaging channel is one of a plurality of messaging channels carrying the data; and

the device is programmed with a specific acquisition class according to a priority levels-queuing methodology for receiving data on a back-up frequency of one or more of the plurality of messaging channels.

11. A receiver unit adapted for use in attenuated or jammed environments, comprising:

an antenna adapted to receive a signal from a satellite acquisition channel or a messaging channel;

a processor;

a receiver clock; and

a memory for storing a plurality of machine readable instructions which when executed by the processor cause the receiver unit to;

receive data from the acquisition channel or the messaging channel, wherein the data has a frame structure,

use the data to determine an identity of the satellite and a position of the satellite,

correct for signal time of flight using the identity of the satellite and the position of the satellite,

use the data as a time reference to align the receiver clock to the frame structure,

with the receiver clock aligned to the frame structure, receive a precision time signal from the satellite, wherein the precision time signal comprises a periodic repeating code,

determine a timing phase of the code, and

use the timing phase to determine a precise absolute time.

12. The receiver unit of claim 11, wherein the instructions when executed by the processor further cause the receiver unit to:

receive the data from the messaging channel in response to an acquisition channel being unavailable, wherein the messaging channel is distinct from the acquisition channel.

13. The receiver unit of claim 11, wherein:

the messaging channel is one of a plurality of messaging channels carrying the data.

14. The receiver unit of claim 11, wherein:

the messaging channel is one of a plurality of messaging channels carrying the data and for which a priori acquisition information is possessed by the receiver unit.

15. The receiver unit of claim 11, wherein:

the messaging channel is one of a plurality of distinct messaging channels carrying the data from the same satellite.

16. The receiver unit of claim 11, wherein:

the messaging channel is one of a plurality of messaging channels carrying the data;

at least one of the messaging channels carries data from a different satellite from the satellite; and

the satellite and the different satellite are in the same satellite constellation.

17. The receiver unit of claim 11, wherein:

the messaging channel is one of a plurality of messaging channels carrying the data;

at least one of the messaging channels carries data from a different satellite from the satellite; and

the satellite and the different satellite are in different satellite constellations.

18. The receiver unit of claim 11, wherein:

the frame structure is an L band frame structure; and

the data includes an L band frame count (LBFC).

19. The receiver unit of claim 11, wherein the data includes a satellite vehicle identification (SVID) of the satellite.