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 satellite communications, comprising:
communicating, via a plurality of antenna feed elements of a satellite based at least in part on a first beamforming weight set that defines a plurality of first spot beams, with a first set of terminals located in a plurality of first coverage areas of a first system coverage area, each first coverage area of the plurality of first coverage areas associated with a respective one of the plurality of first spot beams;
changing a hardware configuration of the satellite; and
communicating, via the plurality of antenna feed elements based at least in part on the changed hardware configuration of the satellite and on a second beamforming weight set that defines a plurality of second spot beams, with a second set of terminals located in a plurality of second coverage areas of a second system coverage area, each second coverage area of the plurality of second coverage areas associated with a respective one of plurality of second spot beams.
2. The method of claim 1 , wherein changing the hardware configuration of the satellite comprises:
changing an allocation of one or more signal pathway hardware sections of the satellite between a forward traffic configuration and a return traffic configuration.
3. The method of claim 1 , wherein changing the hardware configuration of the satellite comprises:
commanding an actuator of the satellite to change a native antenna pattern associated with the plurality of antenna feed elements.
4. The method of claim 3 , wherein commanding the actuator of the satellite causes a spatial adjustment between a reflector of the satellite and the plurality of antenna feed elements.
5. The method of claim 3 , wherein commanding the actuator of the satellite causes an adjustment of the plurality of antenna feed elements relative to a focal region of a reflector of the satellite.
6. The method of claim 1 , wherein changing the hardware configuration of the satellite is based at least in part on receiving a command from a ground station.
7. The method of claim 1 , wherein changing the hardware configuration of the satellite is based at least in part on a predetermined change of coverage of the satellite.
8. The method of claim 7 , wherein the predetermined change of coverage of the satellite is based at least in part on a change of a spot beam coverage area diameter.
9. The method of claim 7 , wherein the predetermined change of coverage of the satellite is based at least in part on a change of area between the first system coverage area and the second system coverage area.
10. The method of claim 7 , wherein the predetermined change of coverage of the satellite is associated with a change of location of one or more gateway terminals or a change in quantity of gateway terminals.
11. The method of claim 7 , wherein the predetermined change of coverage of the satellite is based at least in part on a change of orbit slot of the satellite.
12. The method of claim 7 , further comprising:
receiving a command signal corresponding to the predetermined change of coverage of the satellite, wherein changing the hardware configuration of the satellite is based at least in part on the received command signal.
13. A satellite, comprising:
an antenna comprising a plurality of antenna feed elements; and
one or more controllers configured to cause the satellite to:
communicate, via the plurality of antenna feed elements based at least in part on a first beamforming weight set that defines a plurality of first spot beams, with a first set of terminals located in a plurality of first coverage areas of a first system coverage area, each first coverage area of the plurality of first coverage areas associated with a respective one of the plurality of first spot beams;
change a hardware configuration of the satellite; and
communicate, via the plurality of antenna feed elements based at least in part on the changed hardware configuration of the satellite and on a second beamforming weight set that defines a plurality of second spot beams, with a second set of terminals located in a plurality of second coverage areas of a second system coverage area, each second coverage area of the plurality of second coverage areas associated with a respective one of plurality of second spot beams.
14. The satellite of claim 13 , wherein, to change the hardware configuration of the satellite, the one or more controllers are configured to cause the satellite to:
change an allocation of one or more signal pathway hardware sections of the satellite between a forward traffic configuration and a return traffic configuration.
15. The satellite of claim 13 , wherein, to change the hardware configuration of the satellite, the one or more controllers are configured to cause the satellite to:
command an actuator of the satellite that is configured to change a native antenna pattern associated with the plurality of antenna feed elements.
16. The satellite of claim 15 , wherein the actuator is configured to cause a spatial adjustment between a reflector of the satellite and the plurality of antenna feed elements.
17. The satellite of claim 15 , wherein the actuator is configured to cause an adjustment of the plurality of antenna feed elements relative to a focal region of a reflector of the satellite.
18. The satellite of claim 13 , wherein the one or more controllers are configured to cause the satellite to change the hardware configuration of the satellite based at least in part on a command received from a ground station.
19. The satellite of claim 13 , wherein the one or more controllers are configured to cause the satellite to change the hardware configuration of the satellite based at least in part on a predetermined change of coverage of the satellite.
20. The satellite of claim 19 , wherein the predetermined change of coverage of the satellite is based at least in part on a change of a spot beam coverage area diameter.
21. The satellite of claim 19 , wherein the predetermined change of coverage of the satellite is based at least in part on a change of area between the first system coverage area and the second system coverage area.
22. The satellite of claim 19 , wherein the predetermined change of coverage of the satellite is based at least in part on a change of location of one or more gateway terminals or a change in quantity of gateway terminals.
23. The satellite of claim 19 , wherein the predetermined change of coverage of the satellite is based at least in part on a change of orbit slot of the satellite.
24. The satellite of claim 19 , wherein the one or more controllers are configured to cause the satellite to:
receive a command signal corresponding to the predetermined change of coverage of the satellite; and
change the hardware configuration of the satellite based at least in part on the received command signal.
25. A satellite, comprising:
means for communicating, via a plurality of antenna feed elements of a satellite based at least in part on a first beamforming weight set that defines a plurality of first spot beams, with a first set of terminals located in a plurality of first coverage areas of a first system coverage area, each first coverage area of the plurality of first coverage areas associated with a respective one of the plurality of first spot beams;
means for changing a hardware configuration of the satellite; and
means for communicating, via the plurality of antenna feed elements based at least in part on the changed hardware configuration of the satellite and on a second beamforming weight set that defines a plurality of second spot beams, with a second set of terminals located in a plurality of second coverage areas of a second system coverage area, each second coverage area of the plurality of second coverage areas associated with a respective one of plurality of second spot beams.