LOW EARTH ORBIT SATELLITE PROVIDING NAVIGATION SIGNALS

• US 20080001818A1
• Filed: 05/16/2007
• Published: 01/03/2008
• Est. Priority Date: 05/18/2006
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Ferrell, Barton, Brumley, Robert, Whelan, David, Cohen, Clark, Gutt, Gregory
• Granted Patent: US 7,579,987 B2
• Time in Patent Office: Days
• US Class Current: 342/357.01
• CPC Class Codes: G01S 19/07 providing data for correcting measured positioning data, e.g. DGPS [differential GPS] or ionosphere corrections
• CPC Class Codes: G01S 19/11 wherein the cooperating elements are pseudolites or satellite radio beacon positioning system signal repeaters
• CPC Class Codes: G01S 19/12 wherein the cooperating elements are telecommunication base stations
• CPC Class Codes: G01S 19/31 Acquisition or tracking of other signals for positioning

Abstract

Low earth orbit (LEO) satellites are used to provide navigation signals. In one embodiment, a method of providing a LEO signal from a LEO satellite includes providing a plurality of transmit channels over a plurality of transmit slots. The transmit channels comprise a set of communication channels and a set of navigation channels. The method also includes generating a first pseudo random noise (PRN) ranging overlay corresponding to a navigation signal. The method further includes applying the first PRN ranging overlay to a first set of the navigation channels. In addition, the method includes combining the communication channels and the navigation channels into a LEO signal. The method also includes broadcasting the LEO signal from the LEO satellite.

Claims

1. A method of providing a low earth orbit (LEO) signal from a LEO satellite, the method comprising:

providing a plurality of transmit channels over a plurality of transmit slots, wherein the transmit channels comprise a set of communication channels and a set of navigation channels;

generating a first pseudo random noise (PRN) ranging overlay corresponding to a navigation signal;

applying the first PRN ranging overlay to a first set of the navigation channels;

combining the communication channels and the navigation channels into a LEO signal; and

broadcasting the LEO signal from the LEO satellite.

2. The method of claim 1, wherein the transmit slots are configured in a time division multiple access (TDMA) frame.

3. The method of claim 1, wherein the transmit slots are configured in a plurality of frequency division multiple access (FDMA) frequency bands.

4. The method of claim 1, wherein the navigation signal comprises a ranging component and a data component.

5. The method of claim 4, wherein the data component corresponds to calibration information associated with at least a first ranging source.

6. The method of claim 1, further comprising providing a plurality of receive channels over a plurality of receive slots, wherein the receive channels and the communication channels are associated with a plurality of telephone calls, wherein each telephone call is associated with at least one of the transmit slots and at least one of the receive slots.

7. The method of claim 1, wherein the navigation signal is a military navigation signal, the method further comprising:

generating a second PRN ranging overlay corresponding to a commercial navigation signal;

applying the second PRN ranging overlay to a second set of the navigation channels;

generating a third PRN ranging overlay corresponding to a civil navigation signal; and

applying the third PRN ranging overlay to a third set of the navigation channels.

8. The method of claim 1, wherein the generating comprises:

generating a plurality of ciphers in response to a plurality of counter input values; and

selecting the navigation channels of the first set of the navigation channels using the ciphers.

9. The method of claim 1, wherein the generating comprises:

generating a plurality of ciphers in response to a plurality of counter input values; and

selecting a plurality of direct sequence chips using the ciphers, wherein the selected direct sequence chips correspond to the navigation signal.

10. The method of claim 1, wherein the LEO satellite is selected from the group consisting of an Iridium satellite and a Globalstar satellite.

11. The method of claim 1, further comprising disabling further broadcasting of the LEO signal over an area of operations.

12. The method of claim 1, further comprising:

receiving a data signal;

averaging a plurality of single bit measurements of the data signal to determine data encoded in the data signal; and

combining the data signal into the LEO signal.

13. A low earth orbit (LEO) satellite comprising:

an antenna adapted to broadcast a LEO signal from the LEO satellite; and

a processor adapted to;

provide a plurality of transmit channels over a plurality of transmit slots, wherein the transmit channels comprise a set of communication channels and a set of navigation channels,

generate a first pseudo random noise (PRN) ranging overlay corresponding to a navigation signal,

apply the first PRN ranging overlay to a first set of the navigation channels, and

combine the communication channels and the navigation channels into the LEO signal.

14. The LEO satellite of claim 13, wherein the transmit slots are configured in a time division multiple access (TDMA) frame.

15. The LEO satellite of claim 13, wherein the transmit slots are configured in a plurality of frequency division multiple access (FDMA) frequency bands.

16. The LEO satellite of claim 13, wherein the navigation signal comprises a ranging component and a data component.

17. The LEO satellite of claim 16, wherein the data component corresponds to calibration information associated with at least a first ranging source.

18. The LEO satellite of claim 13, wherein the processor is adapted to provide a plurality of receive channels over a plurality of receive slots, wherein the receive channels and the communication channels are associated with a plurality of telephone calls, wherein each telephone call is associated with at least one of the transmit slots and at least one of the receive slots.

19. The LEO satellite of claim 13, wherein the navigation signal is a military navigation signal, wherein the processor is adapted to:

generate a second PRN ranging overlay corresponding to a commercial navigation signal;

apply the second PRN ranging overlay to a second set of the navigation channels;

generate a third PRN ranging overlay corresponding to a civil navigation signal; and

apply the third PRN ranging overlay to a third set of the navigation channels.

20. The LEO satellite of claim 13, wherein the processor is adapted to:

generate a plurality of ciphers in response to a plurality of counter input values; and

select the navigation channels of the first set of the navigation channels using the ciphers.

21. The LEO satellite of claim 13, wherein the processor is adapted to:

generate a plurality of ciphers in response to a plurality of counter input values; and

select a plurality of direct sequence chips using the ciphers, wherein the selected direct sequence chips correspond to the navigation signal.

22. The LEO satellite of claim 13, wherein the LEO satellite is selected from the group consisting of an Iridium satellite and a Globalstar satellite.

23. The LEO satellite of claim 13, wherein the processor is adapted to disable broadcast of the LEO signal over an area of operations.

24. The LEO satellite of claim 13, wherein the antenna is adapted to receive a data signal, wherein the processor is adapted to:

average a plurality of single bit measurements of the data signal to determine data encoded in the data signal; and

combine the data signal into the LEO signal.

25. A low earth orbit (LEO) satellite comprising:

means for providing a plurality of transmit channels over a plurality of transmit slots, wherein the transmit channels comprise a set of communication channels and a set of navigation channels;

means for generating a first pseudo random noise (PRN) ranging overlay corresponding to a navigation signal;

means for applying the first PRN ranging overlay to a first set of the navigation channels;

means for combining the communication channels and the navigation channels into a LEO signal; and

means for broadcasting the LEO signal from the LEO satellite.