Coverage area adjustment to adapt satellite communications
The described features generally relate to adjusting a native antenna pattern of a satellite to adapt communications via the satellite. For example, a communications satellite may include an antenna having a feed array assembly, a reflector, and a linear actuator coupled between the feed array assembly and the reflector. The feed array assembly may have a plurality of feeds for communicating signals associated with a communications service, and the reflector may be configured to reflect the signals transmitted between the feed array assembly and one or more target devices. The linear actuator may have an adjustable length, or otherwise provide an adjustable position between the feed array assembly and the reflector. By adjusting the position of the feed array assembly relative to the reflector, the communications satellite may provide a communications service according to a plurality of native antenna patterns.
1. A method for communications via a communications satellite having an antenna assembly with a plurality of antenna feed elements, the method comprising:
providing a communications service via a first plurality of beamformed spot beams, the first plurality of beamformed spot beams based at least in part on a first beamforming configuration and a first native antenna pattern of the antenna assembly, the first native antenna pattern corresponding to a first defocused position of a feed array assembly of the antenna assembly relative to a reflector of the antenna assembly, and the first native antenna pattern comprising a composite of first native feed element patterns of the plurality of antenna feed elements;
commanding the communications satellite to change from the first native antenna pattern of the antenna assembly to a second native antenna pattern of the antenna assembly, the second native antenna pattern corresponding to a second defocused position of the feed array assembly relative to the reflector, and the second native antenna pattern comprising a composite of second native feed element patterns of the plurality of antenna feed elements, wherein a given antenna feed element of the plurality of antenna feed elements is associated with one of the first native feed element patterns and one of the second native feed element patterns, and wherein the one of the second native feed element patterns is different from the one of the first native feed element patterns; and
providing the communications service via a second plurality of beamformed spot beams, the second plurality of beamformed spot beams based at least in part on a second beamforming configuration and the second native antenna pattern.
2. The method of claim 1 , wherein commanding the communications satellite to change from the first native antenna pattern to the second native antenna pattern comprises:
commanding an actuator of the communications satellite to provide the change from the first native antenna pattern to the second native antenna pattern.
3. The method of claim 2 , wherein commanding the actuator to provide the change from the first native antenna pattern to the second native antenna pattern comprises:
commanding a spatial adjustment between the reflector of the antenna assembly and the feed array assembly of the antenna assembly comprising the plurality of antenna feed elements.
4. The method of claim 3 , wherein the actuator is coupled between the reflector of the antenna assembly and the feed array assembly.
5. The method of claim 3 , wherein commanding the communications satellite to change from the first native antenna pattern to the second native antenna pattern comprises:
commanding a linear actuator coupled between the reflector and the feed array assembly to change from a first length to a second length.
6. The method of claim 5 , further comprising:
commanding a secondary actuator coupled between the feed array assembly and the reflector to provide the second native antenna pattern, the commanding of the secondary actuator causing a change in relative position between the feed array assembly and the reflector about an axis different from an axis of the linear actuator.
7. The method of claim 2 , wherein commanding the actuator to provide the change from the first native antenna pattern to the second native antenna pattern comprises:
commanding an adjustment to a focal region of the reflector of the antenna assembly.
8. The method of claim 1 , wherein one or both of the first defocused position or the second defocused position is associated with one or more of the plurality of antenna feed elements being located between the reflector and a focal region of the reflector.
9. The method of claim 1 , wherein the first native antenna pattern is associated with a first boresight direction of the antenna assembly, and the second native antenna pattern is associated with a second boresight direction of the antenna assembly that is different from the first boresight direction.
10. The method of claim 1 , wherein the first native antenna pattern is associated with a first native feed element pattern beamwidth of the given antenna feed element, and the second native antenna pattern is associated with a second native feed element pattern beamwidth of the given antenna feed element that is different from the first native feed element pattern beamwidth.
11. The method of claim 1 , wherein the first native antenna pattern is associated with a first amount of overlap of native feed element patterns of two or more antenna feed elements of the antenna assembly, and the second native antenna pattern is associated with a second, different amount of overlap of the native feed element patterns of the two or more antenna feed elements of the antenna assembly.
12. The method claim 1 , further comprising:
adjusting an orbital characteristic of the communications satellite, wherein providing the communications service via the second plurality of beamformed spot beams comprises providing the communications service according to the adjusted orbital characteristic.
13. The method of claim 1 , wherein the communications satellite is at a same geostationary orbital position while providing the communications service via the first plurality of beamformed spot beams and while providing the communications service via the second plurality of beamformed spot beams.
14. The method of claim 1 , wherein:
the communications satellite is at a first geostationary orbital position while providing the communications service via the first plurality of beamformed spot beams;
commanding the communications satellite to change from the first native antenna pattern to the second native antenna pattern comprises commanding the communications satellite to move from the first geostationary orbital position to a second, different geostationary orbital position; and
the communications satellite is at the second geostationary orbital position while providing the communications service via the second plurality of beamformed spot beams.
15. The method of claim 1 , wherein the communications satellite comprises a second antenna assembly with a second plurality of antenna feed elements, the method further comprising:
providing the communications service via a third plurality of beamformed spot beams using the second antenna assembly, the third plurality of beamformed spot beams based at least in part on a third beamforming configuration and a third native antenna pattern of the second antenna assembly, the third native antenna pattern comprising a composite of third native feed element patterns of the second plurality of antenna feed elements.
16. The method of claim 1 , wherein providing the communications service via the first plurality of beamformed spot beams or providing the communications service via the second plurality of beamformed spot beams comprises one or both of:
providing a first plurality of signals between a plurality of access node terminals and the communications satellite; and
providing a second plurality of signals between the communications satellite and a plurality of user terminals.
17. The method of claim 1 , wherein the first beamforming configuration comprises applying a first beamforming weight set to a first plurality of feed element signals carried via the plurality of antenna feed elements, and the second beamforming configuration comprises applying a second beamforming weight set to a second plurality of feed element signals carried via the plurality of antenna feed elements, different from the first beamforming weight set.