Flexible beamforming for satellite communications
Systems and methods for supporting more flexible coverage areas and spatial capacity assignments using satellite communications systems are disclosed. A hub-spoke, bent-pipe satellite communications system includes: terminals; gateways; a controller for specifying data for controlling satellite operations in accordance with a frame definition including timeslots for a frame and defining an allocation of capacity between forward and return traffic. The satellite communications system may employ a satellite with a feed array assembly and may use on-board beamforming or ground-based beamforming. Beam hopping within timeslots of the frame may be used to provide coverage to different cells in different time periods. The flexible coverage areas may be provided using changes in satellite position, antenna patterns, or beam resource allocations.
1. A method for communications via a communications satellite having an antenna assembly with a plurality of antenna feed elements, the method comprising:
identifying a configuration of the antenna assembly for providing a communications service according to a time-varying schedule of spot beam coverage areas;
establishing, using the plurality of antenna feed elements and based at least in part on the identified configuration of the antenna assembly, a first set of beamformed spot beams forming a first pattern of non-overlapping spot beam coverage areas at a first time;
providing the communications service via the first set of beamformed spot beams;
establishing, using the plurality of antenna feed elements and based at least in part on the identified configuration of the antenna assembly, a second set of beamformed spot beams forming a second pattern of non-overlapping spot beam coverage areas at a second time, wherein the second pattern of non-overlapping spot beam coverage areas is different than the first pattern of non-overlapping spot beam coverage areas; and
providing the communications service via the second set of beamformed spot beams.
2. The method of claim 1 , wherein each beamformed spot beam of the second set is aligned in a different direction than the beamformed spot beams of the first set.
3. The method of claim 1 , wherein at least one beamformed spot beam of the second set is aligned in a same direction as a beamformed spot beam of the first set.
4. The method of claim 1 , further comprising:
identifying a traffic condition associated with the communications service; and
identifying the configuration of the antenna assembly based at least in part on the identified traffic condition.
5. The method of claim 1 , further comprising:
commanding an actuator of the communications satellite to provide a native antenna pattern of the plurality of antenna feed elements; and
identifying the configuration of the antenna assembly based at least in part on the provided native antenna pattern.
6. The method of claim 5 , wherein commanding the actuator comprises:
determining, at a ground segment, to provide the native antenna pattern; and
transmitting a command signal to the communications satellite based at least in part on the determining.
7. The method of claim 5 , wherein commanding the actuator comprises:
determining, at the communications satellite, to provide the native antenna pattern; and
commanding the actuator based at least in part on determining to provide the native antenna pattern.
8. The method of claim 1 , further comprising:
establishing the first set of beamformed spot beams based at least in part on a first native antenna pattern of the plurality of antenna feed elements;
commanding an actuator of the communications satellite to change from the first native antenna pattern to a second native antenna pattern of the plurality of antenna feed elements; and
establishing the second set of beamformed spot beams based at least in part on the second native antenna pattern.
9. The method of claim 8 , further comprising:
determining a traffic condition associated with the communications service,
wherein the commanding is triggered based at least in part on the determined traffic condition.
10. The method of claim 8 , further comprising:
determining, at a ground segment, a command for commanding the actuator.
11. The method of claim 8 , further comprising:
determining, at the communications satellite, a command for commanding the actuator.
12. The method of claim 8 , wherein commanding the actuator to change from the first native antenna pattern to the second native antenna pattern comprises:
commanding a spatial adjustment between a reflector of the antenna assembly and a feed array assembly of the antenna assembly comprising the plurality of antenna feed elements.
13. The method of claim 12 , wherein commanding the actuator to change from the first native antenna pattern to the second native antenna pattern comprises:
commanding an actuator coupled between the reflector and the feed array assembly.
14. The method of claim 8 , wherein commanding the actuator to change from the first native antenna pattern to the second native antenna pattern comprises:
commanding an adjustment to a focal region of a reflector of the antenna assembly.
15. The method of claim 14 , wherein the first native antenna pattern is based at least in part on the focal region having a first shape, and the second native antenna pattern is based at least in part on the focal region having a second shape, different from the first shape.
16. The method of claim 8 , wherein commanding the actuator to change from the first native antenna pattern to the second native antenna pattern comprises:
commanding an adjustment from a first spatial arrangement of the plurality of antenna feed elements to a second spatial arrangement of the plurality of antenna feed elements.
17. The method of claim 16 , wherein the antenna assembly comprises a direct radiating array antenna assembly.
18. The method of claim 16 , wherein the first native antenna pattern is based at least in part on the first spatial arrangement having a first orientation of at least a subset of the plurality of antenna feed elements, and the second native antenna pattern is based at least in part on the second spatial arrangement having a second orientation of the at least a subset of the plurality of antenna feed elements, different from the first orientation.
19. A communications satellite for providing a communications service, the communications satellite comprising:
an antenna assembly comprising a feed array assembly having a plurality of antenna feed elements;
a beamformer configured for establishing beamformed spot beams using the plurality of antenna feed elements; and
a controller configured to:
identify a configuration of the antenna assembly for providing the communications service according to a time-varying schedule of spot beam coverage areas;
cause the beamformer to establish, at a first time, a first set of beamformed spot beams based at least in part on the identified configuration of the antenna assembly, the first set of beamformed spot beams forming a first pattern of non-overlapping spot beam coverage areas;
provide the communications service via the first set of beamformed spot beams;
cause the beamformer to establish, at a second time, a second set of beamformed spot beams based at least in part on the identified configuration of the antenna assembly, the second set of beamformed spot beams forming a second pattern of non-overlapping spot beam coverage areas that is different than the first pattern of non-overlapping spot beam coverage areas; and
provide the communications service via the second set of beamformed spot beams.
20. The communications satellite of claim 19 , wherein each beamformed spot beam of the second set is aligned in a different direction than the beamformed spot beams of the first set.
21. The communications satellite of claim 19 , wherein at least one beamformed spot beam of the second set is aligned in a same direction as a beamformed spot beam of the first set.
22. The communications satellite of claim 19 , wherein the controller is configured to:
identify a traffic condition associated with the communications service; and
identify the configuration of the antenna assembly based at least in part on the identified traffic condition.
23. The communications satellite of claim 19 , wherein the controller is configured to:
command an actuator of the communications satellite to provide a native antenna pattern of the plurality of antenna feed elements; and
identify the configuration of the antenna assembly based at least in part on the provided native antenna pattern.
24. The communications satellite of claim 23 , wherein, to command the actuator, the controller is configured to:
receive a command signal from a ground segment; and
command the actuator based at least in part on the received command signal.
25. The communications satellite of claim 23 , wherein, to command the actuator, the controller is configured to:
determine to provide the native antenna pattern; and
command the actuator based at least in part on determining to provide the native antenna pattern.
26. The communications satellite of claim 19 , wherein the controller is configured to:
cause the beamformer to establish the first set of beamformed spot beams based at least in part on a first native antenna pattern of the plurality of antenna feed elements;
command an actuator of the communications satellite to change from the first native antenna pattern to a second native antenna pattern of the plurality of antenna feed elements; and
cause the beamformer to establish the second set of beamformed spot beams based at least in part on the second native antenna pattern.
27. The communications satellite of claim 26 , wherein the controller is configured to:
determine a traffic condition associated with the communications service,
wherein the commanding the actuator is triggered based at least in part on the determined traffic condition.
28. The communications satellite of claim 26 , wherein the controller is configured to:
receive, from a ground segment, a command for the commanding the actuator.
29. The communications satellite of claim 26 , wherein the controller is configured to:
determine a command for the commanding the actuator.
30. The communications satellite of claim 26 , wherein, to command the actuator to change from the first native antenna pattern to the second native antenna pattern, the controller is configured to:
command a spatial adjustment between a reflector of the antenna assembly and the feed array assembly.
31. The communications satellite of claim 30 , wherein, to command the actuator to change from the first native antenna pattern to the second native antenna pattern, the controller is configured to:
command an actuator coupled between the reflector and the feed array assembly.
32. The communications satellite of claim 26 , wherein, to command the actuator to change from the first native antenna pattern to the second native antenna pattern, the controller is configured to:
command an adjustment to a focal region of a reflector of the antenna assembly.
33. The communications satellite of claim 32 , wherein the first native antenna pattern is based at least in part on the focal region having a first shape, and the second native antenna pattern is based at least in part on the focal region having a second shape, different from the first shape.
34. The communications satellite of claim 26 , wherein, to command the actuator to change from the first native antenna pattern to the second native antenna pattern, the controller is configured to:
command an adjustment from a first spatial arrangement of the plurality of antenna feed elements to a second spatial arrangement of the plurality of antenna feed elements.
35. The communications satellite of claim 34 , wherein the antenna assembly comprises a direct radiating array antenna assembly.
36. The communications satellite of claim 34 , wherein the first native antenna pattern is based at least in part on the first spatial arrangement having a first orientation of at least a subset of the plurality of antenna feed elements, and the second native antenna pattern is based at least in part on the second spatial arrangement having a second orientation of the at least a subset of the plurality of antenna feed elements, different from the first orientation.