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:
transmitting, from a ground segment of a satellite communication system, a first configuration for a satellite to communicate, via a plurality of antenna feed elements of the 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; and
transmitting, from the ground segment, a second configuration for the satellite to communicate, via the plurality of antenna feed elements based at least in part on a 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 the plurality of second spot beams.
2 . The method of claim 1 , wherein transmitting the second configuration comprises:
transmitting a command, wherein the changed hardware configuration of the satellite is based at least in part on transmitting the command.
3 . The method of claim 1 , wherein:
the first configuration is associated with a first allocation of one or more signal pathway hardware sections of the satellite between a forward traffic configuration and a return traffic configuration; and
the second configuration is associated with a second allocation of the one or more signal pathway hardware sections between the forward traffic configuration and the return traffic configuration that is different from the first allocation.
4 . The method of claim 3 , wherein the changed hardware configuration comprises a changed configuration of at least one of the one or more signal pathway hardware sections between a forward pathway gain associated with the forward traffic configuration and a return pathway gain associated with the return traffic configuration.
5 . The method of claim 1 , wherein the changed hardware configuration comprises a change of a native antenna pattern associated with the plurality of antenna feed elements.
6 . The method of claim 5 , wherein the change of the native antenna pattern is based at least in part on a spatial adjustment between a reflector of the satellite and the plurality of antenna feed elements.
7 . The method of claim 5 , the change of the native antenna pattern is based at least in part on an adjustment of the plurality of antenna feed elements relative to a focal region of a reflector of the satellite.
8 . The method of claim 1 , wherein transmitting the second configuration is based at least in part on a change in demand profile within the first system coverage area or within the second system coverage area.
9 . The method of claim 1 , wherein transmitting the second configuration is based at least in part on a desired change of characteristics relative to the plurality of first spot beams.
10 . The method of claim 1 , wherein transmitting the second configuration is based at least in part on a desired change of area between the first system coverage area and the second system coverage area.
11 . The method of claim 1 , wherein transmitting the second configuration is based at least in part on a desired change of a spot beam coverage area diameter provided using the plurality of antenna feed elements.
12 . The method of claim 1 , wherein transmitting the second configuration is based at least in part on a change in orbital position of the satellite.
13 . The method of claim 2 , wherein transmitting the second configuration 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.
14 . A controller of a satellite communications system, the controller configured to cause one or more ground terminals of the satellite communications system to:
transmit a first configuration for a satellite to communicate, via a plurality of antenna feed elements of the 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; and
transmit a second configuration for the satellite to communicate, via the plurality of antenna feed elements based at least in part on a 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 the plurality of second spot beams.
15 . The controller of claim 14 , further configured to cause the one or more ground terminals of the satellite communications system to:
transmit a command, wherein the changed hardware configuration of the satellite is based at least in part on transmitting the command.
16 . The controller of claim 14 , wherein:
the first configuration is associated with a first allocation of one or more signal pathway hardware sections of the satellite between a forward traffic configuration and a return traffic configuration; and
the second configuration is associated with a second allocation of the one or more signal pathway hardware sections between the forward traffic configuration and the return traffic configuration that is different from the first allocation.
17 . The controller of claim 16 , wherein the changed hardware configuration comprises a changed configuration of at least one of the one or more signal pathway hardware sections between a forward pathway gain associated with the forward traffic configuration and a return pathway gain associated with the return traffic configuration.
18 . The controller of claim 14 , wherein the changed hardware configuration comprises a change of a native antenna pattern associated with the plurality of antenna feed elements.
19 . The controller of claim 18 , wherein the change of the native antenna pattern is based at least in part on a spatial adjustment between a reflector of the satellite and the plurality of antenna feed elements.
20 . The controller of claim 18 , the change of the native antenna pattern is based at least in part on an adjustment of the plurality of antenna feed elements relative to a focal region of a reflector of the satellite.
21 . The controller of claim 18 , further configured to cause the one or more ground terminals of the satellite communications system to:
transmit the second configuration based at least in part on a change in demand profile within the first system coverage area or within the second system coverage area.
22 . The controller of claim 18 , further configured to cause the one or more ground terminals of the satellite communications system to:
transmit the second configuration based at least in part on a desired change of characteristics relative to the plurality of first spot beams.
23 . The controller of claim 18 , further configured to cause the one or more ground terminals of the satellite communications system to:
transmit the second configuration based at least in part on a desired change of area between the first system coverage area and the second system coverage area.
24 . The controller of claim 18 , further configured to cause the one or more ground terminals of the satellite communications system to:
transmit the second configuration based at least in part on a desired change of a spot beam coverage area diameter provided using the plurality of antenna feed elements.
25 . The controller of claim 18 , further configured to cause the one or more ground terminals of the satellite communications system to:
transmit the second configuration based at least in part on a change in orbital position of the satellite.
26 . The controller of claim 18 , further configured to cause the one or more ground terminals of the satellite communications system to:
transmit the second configuration based at least in part on a change of location of one or more gateway terminals or a change in quantity of gateway terminals.
27 . A system for satellite communications, comprising:
means for transmitting, from a ground segment of a satellite communication system, a first configuration for a satellite to communicate, via a plurality of antenna feed elements of the 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; and
means for transmitting, from the ground segment, a second configuration for the satellite to communicate, via the plurality of antenna feed elements based at least in part on a 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 the plurality of second spot beams.