Tandem satellite frame synchronization

• US 9,386,550 B2
• Filed: 03/14/2013
• Issued: 07/05/2016
• Est. Priority Date: 06/11/2012
• Status: Active Grant

• Current Assignee: ViaSat Incorporated
• Original Assignee: ViaSat Incorporated
• Inventors: Becker, Donald W.
• Primary Examiner(s): Chriss, Andrew
• Assistant Examiner(s): Preval, Voster
• Application Number:
  US13/830,838
• Publication Number:
  US 20130329630A1
• Time in Patent Office: 1,209 Days
• Field of Search: 370/326
• US Class Current: 1/1
• CPC Class Codes: H04B 7/18513 Transmission in a satellite or space-based system
• CPC Class Codes: H04B 7/2048 Frame structure, synchronisation or frame acquisition in SS-TDMA systems
• CPC Class Codes: H04B 7/2125 Synchronisation
• CPC Class Codes: H04W 56/0015 one node acting as a reference for the others

Abstract

Systems and methods are described synchronizing communications frames and their respective time slots for satellite communications architectures having multiple satellites in the same orbital slot in such a way that addresses inter-satellite inter-beam interference. In some embodiments, the first and second satellites communicate with a respective number of ground terminals (e.g., gateway and user terminals) according to first and second satellite time slots, respectively. The satellites maintain relative positions in their orbital slot to manifest a maximum path delay difference between first and second path delays, the first path delay being between the first ground terminals and the first satellite, and the second path delay being between the first ground terminals and the second satellite. A synchronization system can offset the first satellite time slots from the second satellite time slots as a function of the maximum path delay difference.

Claims

1. A satellite communications system comprising:

a first satellite configured to relay first satellite communications for first ground terminals, the first communications synchronized according to first satellite time slots;

a second satellite configured to relay second satellite communications for second ground terminals, the second satellite communications synchronized according to second satellite time slots,

the first and second satellites configured to maintain relative positions in a single orbital slot such that there is a maximum path delay difference between first and second path delays, the first path delay being between the first ground terminals and the first satellite, and the second path delay being between the first ground terminals and the second satellite; and

a synchronization system configured to offset the first satellite time slots from the second satellite time slots as a function of the maximum path delay difference with respect to the first satellite time slots being lined up with the second satellite time slots.

2. The system of claim 1, wherein the synchronization system is configured to offset the first satellite time slots from the second satellite time slots by approximately the maximum path delay difference.

3. The system of claim 1, wherein the synchronization system is further configured to define a duration for each of the first and second time slots as at least twice the maximum path delay difference.

4. The system of claim 1, wherein:

the synchronization system is further configured to define a duration for each of the first and second time slots according to the maximum path delay difference; and

the synchronization system is configured to offset the first satellite time slots from the second satellite time slots by approximately one-half of the duration.

5. The system of claim 1, wherein the first and second satellites are configured to maintain relative positions in the single orbital slot such that there is the maximum path delay difference defined according to timing of the first and second satellite time slots.

6. The system of claim 1, wherein each satellite communicates with its respective ground terminals via a respective plurality of spot beams according to a beam switching scheme.

7. The system of claim 6, wherein the beam switching scheme selects spot beams to communicate via the satellites during each of the first and second satellite time slots in such a way as to limit selection of potentially interfering spot beams on the first and second satellites during overlapping first and second satellite time slots.

8. The system of claim 6, wherein:

the first satellite communications via the first satellite uses first spot beams selected according to the beam switching scheme during a time slot N of the first satellite time slots;

the first satellite communications via the first satellite uses second spot beams selected according to the beam switching scheme during a time slot N+1 of the first satellite time slots; and

the second satellite communications via the second satellite uses third spot beams selected according to the beam switching scheme during a time slot M of the second satellite time slots,

wherein a first portion of time slot M overlaps with time slot N so that the first and third spot beams experience first interference levels during the first portion of time slot M, and a second portion of time slot M overlaps with time slot N+l so that the second and third spot beams experience second interference levels during the second portion of time slot M.

9. The system of claim 8, wherein the synchronization system operates to reduce the impact of potentially interfering spot beams from the satellites on the first and second interference levels at least by:

predicting whether any of the third spot beams potentially interferes with any of the first or second respective spot beams during time slot M according to the beam switching scheme; and

avoiding communicating via the potentially interfering third spot beams during time slot M.

10. The system of claim 1, wherein the first ground terminals comprises at least one gateway terminal and a plurality of user terminals in communication via a hub-spoke communications architecture.

11. The system of claim 1, wherein:

each ground terminal is configured to communicate with one of the first or second satellites, to calculate its path delay to its respective satellite, and to synchronize its communications with its respective satellite so that a communication associated with a particular satellite time slot is received by its respective satellite at a slot boundary of the particular satellite time slot.

12. The system of claim 1, wherein the synchronization system comprises:

a core node in communication with at least one gateway terminal of the first ground terminals and at least one gateway terminal of the second ground terminals and configured to synchronize the first and second satellite communications via the gateway terminals.

13. The system of claim 1, wherein each of the first and second satellites is a bent pipe satellite.

14. A method for synchronizing communications via first and second satellites in an orbital slot, the method comprising:

synchronizing first satellite communications by a first ground terminal via the first satellite in the orbital slot according to first satellite time slots;

synchronizing second satellite communications by a second ground terminal via the second satellite in the orbital slot according to second satellite time slots;

maintaining relative positions of the satellites with station keeping such that there is the maximum path delay difference defined according to timing of the first and second satellite time slots;

and synchronizing the first satellite time slots to be offset with respect to the second satellite time slots as a function of a maximum path delay difference between first and second path delays with respect to the first satellite time slots being lined up with the second satellite time slots, the first path delay being between the first ground terminal and the first satellite, and the second path delay being between the first ground terminal and the second satellite.

15. The method of claim 14, wherein the first satellite time slots are synchronized to be offset with respect to the second satellite time slots by approximately the maximum path delay difference.

16. The method of claim 14, further comprising:

defining a duration for each of the first and second satellite time slots as approximately twice the maximum path delay difference.

17. The method of claim 14, further comprising:

defining a duration for each of the first and second satellite time slots according to the maximum path delay difference; and

synchronizing the first satellite time slots to be offset with respect to the second satellite time slots by approximately one-half of the duration.

18. The method of claim 14, further comprising:

selecting a first plurality of ground terminals that comprises the first ground terminal to communicate via the first satellite and selecting a second plurality of ground terminals that comprises the second ground terminal to communicate via the second satellite so as to group potentially interfering spot beams by satellite.

19. The method of claim 14, further comprising:

communicating, during a time slot N of the first satellite time slots, via the first satellite using first spot beams selected according to a beam switching scheme;

communicating, during a time slot N+l of the first satellite time slots, via the first satellite using second spot beams selected according to the beam switching scheme; and

communicating, during a time slot M of the second satellite time slots, via the second satellite using third spot beams selected according to the beam switching scheme,

wherein a first portion of time slot M overlaps with time slot N so that the first and third spot beams experience first interference levels during the first portion of time slot M, and a second portion of time slot M overlaps with time slot N+l so that the second and third spot beams experience second interference levels during the second portion of time slot M.

20. The method of claim 19, further comprising:

generating the beam switching scheme to select pairs of ground terminals to communicate via the satellites during each of the first and second satellite time slots in such a way that limits selection of potentially interfering spot beams on the first and second satellites during overlapping first and second satellite time slots.

21. The method of claim 19, further comprising:

predicting whether any of the third spot beams potentially interferes with any of the first or second spot beams during time slot M according to the beam switching scheme; and

avoiding communicating via the potentially interfering third spot beams during time slot M.