Methods and systems for mitigating interference with a nearby satellite

1. An antenna system for mounting on an aircraft, the antenna system comprising:

a primary antenna on the aircraft, wherein the primary antenna has a first acceptable service area for communication of a signal between the aircraft and a target satellite while satisfying a performance characteristic for communicating with the target satellite;

a secondary antenna on the aircraft, wherein the secondary antenna has a second acceptable service area for communication of the signal between the aircraft and the target satellite while satisfying the performance characteristic for communicating with the target satellite, and wherein the second acceptable service area overlaps with a portion of the first acceptable service area; and

an antenna selection system to control communication of the signal between the aircraft and the target satellite via the primary antenna and the secondary antenna, wherein the antenna selection system:

selects the primary antenna for communication of the signal with the target satellite when the aircraft is at a first position that is within the portion of the first acceptable service area that overlaps with the second acceptable service area, wherein both the primary antenna and the secondary antenna satisfy the performance characteristic for communicating with the target satellite at the first position, and wherein a data stream associated with the secondary antenna is deactivated when the primary antenna is selected, and

selects the secondary antenna for communication of the signal with the target satellite when the aircraft is at a second position that is different than the first position, within the second acceptable service area, and not within the first acceptable service area of the primary antenna.

2. The antenna system of claim 1 , wherein a data stream associated with the primary antenna is deactivated when the secondary antenna is selected.

3. The antenna system of claim 1 , wherein the antenna selection system switches communication of the signal from the primary antenna to the secondary antenna at a boundary of the first acceptable service area.

4. The antenna system of claim 3 , wherein the antenna selection system switches back to the primary antenna to communicate the signal at a second boundary of the first acceptable service area.

5. The antenna system of claim 1 , wherein the antenna selection system comprises:

a switch that is coupled with the primary antenna, the secondary antenna, and a modem on the aircraft, wherein the switch couples one of the primary antenna and the secondary antenna to the modem based on whether the primary antenna or the secondary antenna is selected.

6. The antenna system of claim 1 , wherein the antenna selection system comprises:

a first switch positioned between the primary antenna and a modem, and

a second switch positioned between the secondary antenna and the modem, wherein the antenna selection system is configured to open the first switch and close the second switch when the secondary antenna is selected.

7. The antenna system of claim 6 , wherein:

a first intermediate frequency signal associated with the signal is received at the first switch, and

a second intermediate frequency signal associated with the signal is received at the second switch, wherein the second intermediate frequency signal is passed to the secondary antenna or the modem based at least in part on the secondary antenna being selected, the data stream associated with the secondary antenna being based at least in part on the second intermediate frequency signal.

8. The antenna system of claim 1 , further comprising:

a first modem coupled with the primary antenna and configured to establish a first connection with the target satellite via the primary antenna when the primary antenna is selected; and

a second modem coupled with the secondary antenna and configured to establish a second connection with the target satellite when the secondary antenna is selected.

9. The antenna system of claim 8 , wherein:

the first modem terminates the first connection after the second modem establishes the second connection, and

the second modem terminates the second connection after the first modem establishes the first connection.

10. The antenna system of claim 8 , wherein:

a data stream associated with the primary antenna is generated by the first modem based at least in part on establishing the first connection with the target satellite, and

the data stream associated with the secondary antenna is generated by the second modem based at least in part on establishing the second connection with the target satellite.

11. The antenna system of claim 8 , further comprising:

a network access unit that routes data associated with the signal between one of the first modem and the second modem based on whether the primary antenna or the secondary antenna is selected.

12. The antenna system of claim 8 , wherein the signal is a return uplink signal.

13. The antenna system of claim 1 , wherein the first acceptable service area and the second acceptable service area are incongruous.

14. The antenna system of claim 1 , wherein a positioner for the primary antenna is controlled to point at the target satellite upon selection of the secondary antenna.

15. The antenna system of claim 1 , further comprising:

a radome, wherein the primary antenna and the secondary antenna are under the radome.

16. The antenna system of claim 1 , wherein the second position is within a keyhole region of the target satellite.

17. The antenna system of claim 16 , wherein the first position is outside the keyhole region.

18. The antenna system of claim 1 , wherein the second position is closer to a sub-satellite point of the target satellite than the first position.

19. The antenna system of claim 1 , wherein, after selecting the secondary antenna for communication of the signal at the second position of the aircraft, the antenna selection system:

reselects the primary antenna for communication of the signal at a third position of the aircraft within the portion of the first acceptable service area that overlaps with the second acceptable service area, wherein both the primary antenna and the secondary antenna satisfy the performance characteristic for communicating with the target satellite at the third position of the aircraft.

20. The antenna system of claim 19 , wherein, at the third position of the aircraft, the performance characteristic for the secondary antenna exceeds the performance characteristic for the primary antenna.

21. The antenna system of claim 1 , wherein the first acceptable service area comprises a first geographic area and a second geographic area that is non-overlapping with the first geographic area, and wherein the second acceptable service area comprises a third geographic area that overlaps with the first geographic area and the second geographic area.

22. The antenna system of claim 1 , wherein the performance characteristic is an interference requirement with a non-target satellite.

23. The antenna system of claim 1 , wherein the performance characteristic is a pointing error to the target satellite.

24. The antenna system of claim 23 , wherein the antenna selection system switches to the secondary antenna to communicate the signal based on a slew rate of a positioner of the primary antenna exceeding a first threshold, wherein an amount of the pointing error to the target satellite is based on the slew rate of the positioner.

25. The antenna system of claim 24 , wherein the antenna selection system switches back to the primary antenna to communicate the signal based on the slew rate of the primary antenna satisfying a second threshold.

26. The antenna system of claim 1 , wherein the antenna selection system switches to the secondary antenna to communicate the signal based on an elevation angle of a boresight of the primary antenna exceeding a threshold relative to a horizon.

27. The antenna system of claim 1 , wherein a first field of view of the primary antenna and a second field of view of the secondary antenna overlap.

28. The antenna system of claim 1 , further comprising:

a first positioner of the primary antenna for mechanically orienting the primary antenna.

29. The antenna system of claim 28 , further comprising:

a steering mechanism of the secondary antenna, wherein a range of the steering mechanism is less than that of the first positioner in at least one axis.

30. The antenna system of claim 29 , wherein the at least one axis is an elevation axis.

31. The antenna system of claim 1 , wherein the primary antenna has at least one performance characteristic for communicating the signal that is different than that of the secondary antenna.

32. The antenna system of claim 31 , wherein the primary antenna has at least one of higher gain, lower sidelobes, or lower cross-polarization than that of the secondary antenna.

33. The antenna system of claim 31 , wherein a beamwidth of the primary antenna along a vertical axis is greater than a beamwidth of the secondary antenna along the vertical axis.

34. The antenna system of claim 1 , wherein the first acceptable service area and the second acceptable service area define a composite acceptable service area of the antenna system, the composite acceptable service area larger than each of the first acceptable service area and the second acceptable service area.

35. The antenna system of claim 1 , wherein the antenna selection system selects the primary antenna to transmit the signal when a geographic location of the aircraft is within the first acceptable service area.

36. The antenna system of claim 1 , wherein differences between the first acceptable service area and the second acceptable service area are due to differences between the primary antenna and the secondary antenna.