Techniques for spatial diversity in satellite communications

1. A method for controlling communication in a satellite communication network having multiple constellations and a satellite terminal with a single electronically steered flat-panel antenna capable of generating a plurality of beams for communication links with multiple satellites, the method comprising:

determining, under network control, availability of a plurality of networks by which network traffic may be exchanged with the single electronically steered flat-panel antenna; and

managing, under network control, two or more satellite links between the single electronically steered flat-panel antenna and two or more satellites of different networks to route the network traffic, including determining when to use each of the two or more satellite links, the two or more satellite links being generated using two or more beams from the single electronically steered flat-panel antenna.

2. The method of claim 1 further comprising generating the two or more beams simultaneously by beam splitting to maintain the two or more links for communication between the single electronically steered flat-panel antenna and two or more different satellites at the same time.

3. The method of claim 2 further comprising:

generating a first beam with a single electronically steered flat-panel antenna;

routing network traffic with the first hub via a first link between the antenna and a first satellite using the first beam;

maintaining a network connection to a second hub via a second link between the antenna and a second satellite by generating a second beam with the single electronically steered flat-panel antenna simultaneously while generating the first beam, the second hub being different than the first hub and the second beam being different than the first beam;

determining, by the network control, to route the network traffic through the second hub in response to determining a disruption condition exists with respect to the first link; and

routing the network traffic with the second hub via the second link between the antenna and the second satellite using the second beam.

4. The method of claim 3 wherein the disruption condition relates to a line-of-sight (LOS) disruption or another outage condition related to the first link.

5. The method of claim 2 further comprising weighting each of the two or more beams based on one or more network functions.

6. The method of claim 5 wherein weighting each of the two or more beams based on one or more network functions comprises weighting a primary beam more strongly to increase spectral efficiency while reducing weighting on one or more secondary beams to a level sufficient only to sustain a connection to a secondary satellite network.

7. The method of claim 5 wherein weighting each of the two or more beams based on one or more network functions comprises weighting beams based on throughput performance or a reduced cost of data transfer.

8. The method of claim 2 wherein a multi-wide area network (MWAN) edge router associated with the single electronically steered flat-panel antenna and a software-defined wide area network (SDWAN) controller work together to maintain a network connection on secondary networks for protected fail over during LOS blockages or other outages.

9. The method of claim 1 wherein the two or more beams are generated one at a time, and wherein managing the two or more satellite links comprises switching between the two or more links to communicate the network traffic between the single electronically steered flat-panel antenna and the two or more different satellites while toggling between use of two or more beams generated by the single electronically steered flat-panel antenna for the two or more satellite links.

10. The method of claim 9 wherein the single electronically steered flat-panel antenna is part of a satellite terminal having an edge compute appliance and a software-defined modem, and further comprising directing, by the edge compute appliance, the software-defined modem to switch between the two or more links to communicate the network traffic between the single electronically steered flat-panel antenna and the two or more different satellites.

11. The method of claim 10 wherein the edge compute appliance directs the software-defined modem to switch between the two or more links to improve quality of service (QOS) and/or one or more network efficiency goals.

12. A satellite communication network topology comprising:

a single electronically steered flat-panel antenna capable of generating a plurality of beams;

a first network comprising a first hub and a first satellite;

a second network comprising a second hub and a second satellite; and

network control to

determine availability of a first and second networks for exchanging network traffic with the single electronically steered flat-panel antenna; and

manage first and second satellite links between the single electronically steered flat-panel antenna and the first and second satellites, respectively, to route the network traffic, wherein the network control is configured to determine when to use the first and second satellite links to first and second satellites, respectively, the first and second satellite links being generated using first and second beams of the plurality of beams from the single electronically steered flat-panel antenna.

13. The satellite communication network topology of claim 12 wherein the single electronically steered flat-panel antenna is operable to generate the first and second beams simultaneously by beam splitting to maintain the first and second links for communication between the single electronically steered flat-panel antenna and first and second satellites at the same time.

14. The satellite communication network topology of claim 13 wherein the single electronically steered flat-panel antenna is operable to:

generate the first beam;

route network traffic with the first hub via the first link between the antenna and the first satellite using the first beam;

maintain a network connection to the second hub via the second link between the antenna and the second satellite by generating the second beam simultaneously while generating the first beam, the second hub being different than the first hub and the second beam being different than the first beam;

wherein the network control is operable to determine to route the network traffic through the second hub in response to determining a disruption condition exist with respect to the first link and causes routing of the network traffic with the second hub via the second link between the antenna and the second satellite using the second beam.

15. The satellite communication network topology of claim 14 wherein the disruption condition relates to a line-of-sight (LOS) disruption or another outage condition related to the first link.

16. The satellite communication network topology of claim 13 wherein the single electronically steered flat-panel antenna is operable to weight the first and second beams based on one or more network functions.

17. The satellite communication network topology of claim 16 wherein the single electronically steered flat-panel antenna is operable to weight the first and second beams by weighting the first beam more strongly to increase spectral efficiency while reducing weighting on the second beams to a level only sufficient to sustain a connection to the second satellite.

18. The satellite communication network topology of claim 13 further comprising:

a multi-wide area network (MWAN) edge router associated with the single electronically steered flat-panel antenna; and

a software-defined wide area network (SDWAN) controller, the MWAN edge router and the SDWAN controller working together to maintain a network connection on second network for protected fail over during LOS blockages or other outages on the first network.

19. The satellite communication network topology of claim 12 wherein the single electronically steered flat-panel antenna is operable to generate the first and second beams one at a time, and wherein the network control manages the first and second satellite links by switching between the first and second links to communicate the network traffic between the single electronically steered flat-panel antenna and the first and second satellites while the single electronically steered flat-panel antenna toggles between use of first and second beams for the first and second satellite links.

20. The satellite communication network topology of claim 19 wherein the single electronically steered flat-panel antenna is part of a satellite terminal having an edge compute appliance and a software defined modem, and further wherein the edge compute appliance is operable to direct the software defined modem to switch between the first and second links to communicate the network traffic between the single electronically steered flat-panel antenna and the first and second satellites.