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 is mechanically steerable and has an asymmetric antenna beam pattern with a narrow beamwidth axis and a wide beamwidth axis at boresight;

a secondary antenna on the aircraft, the secondary antenna comprising an array of antenna elements; and

an antenna selection system to control communication of an uplink signal and a downlink signal between the aircraft and a target satellite via the primary antenna and the secondary antenna, wherein the antenna selection system switches transmission of the uplink signal from the primary antenna to the secondary antenna when an amount of interference with a non-target satellite reaches a threshold due to the wide beamwidth axis of the asymmetric antenna beam pattern, and maintains reception of the downlink signal via the primary antenna upon switching transmission of the uplink signal to the secondary antenna.

2. The antenna system of claim 1 , wherein:

the target satellite and the non-target satellite are each geostationary satellites along a geostationary arc; and

the antenna selection system switches transmission of the uplink signal when a skew angle between the asymmetric beam pattern and the geostationary arc reaches a predetermined value.

3. The antenna system of claim 1 , wherein at least one of the target satellite and the non-target satellite is a non-geostationary satellite.

4. The antenna system of claim 1 , wherein a half-power beamwidth of the wide beamwidth axis is at least three times greater than a half-power beamwidth of the narrow beamwidth axis.

5. The antenna system of claim 1 , wherein the narrow beamwidth axis and the wide beamwidth axis are a horizontal axis and a vertical axis respectively of the primary antenna.

6. The antenna system of claim 1 , wherein the secondary antenna has a second antenna pattern with a narrow beamwidth axis and a wide beamwidth axis when communicating the signal with the target satellite, and a half-power beamwidth of the wide beamwidth axis of the second antenna pattern is less than three times a half-power beamwidth of the narrow beamwidth axis of the second antenna pattern.

7. The antenna system of claim 1 , wherein the secondary antenna includes an azimuth adjustment mechanism and an elevation adjustment mechanism to steer a beam of the secondary antenna.

8. The antenna system of claim 1 , wherein the primary antenna includes a mechanical azimuth adjustment mechanism and a mechanical elevation adjustment mechanism.

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

a first transceiver coupled to the primary antenna; and

a second transceiver coupled to the secondary antenna.

10. The antenna system of claim 9 , further comprising a modem that is shared by the first transceiver and the second transceiver.

11. The antenna system of claim 1 , further comprising a positioner to maintain pointing of the primary antenna at the target satellite following the switching of transmission of the uplink signal to the secondary antenna.

12. The antenna system of claim 1 , wherein:

the threshold is a first threshold; and

the antenna selection system switches back the transmission of the uplink signal from the secondary antenna to the primary antenna when the amount of interference to the adjacent satellite is below a second threshold.

13. The antenna system of claim 12 , wherein the first threshold is different than the second threshold.

14. The antenna system of claim 12 , wherein the antenna selection system maintains reception of the downlink signal via the primary antenna upon the switching back the transmission of the uplink signal from the secondary antenna to the primary antenna.

15. A method comprising:

communicating an uplink signal and a downlink signal between a target satellite and an aircraft via a primary antenna on the aircraft, wherein the primary antenna is mechanically steerable and has an asymmetric antenna beam pattern with a narrow beamwidth axis and a wide beamwidth axis at boresight;

determining that an amount of interference with a non-target satellite reaches a threshold due to the wide beamwidth axis of the asymmetric antenna beam pattern;

in response to the determination, switching transmission of the uplink signal from the primary antenna to a secondary antenna on the aircraft to reduce interference with the non-target satellite, wherein the secondary antenna comprises an array of antenna elements; and

maintaining reception of the downlink signal via the primary antenna upon switching transmission of the uplink signal to the secondary antenna.

16. The method of claim 15 , wherein the amount of interference is based on a geographic location of the aircraft.

17. The method of claim 15 , wherein:

the target satellite and the non-target satellite are each geostationary satellites along a geostationary arc; and

the determining is based on when a skew angle between the asymmetric beam pattern and the geostationary arc is below a predetermined value.

18. The method of claim 15 , further comprising switching back transmission of the uplink signal from the secondary antenna to the primary antenna when the amount of interference to the non-target satellite is below a second threshold.

19. The method of claim 18 , further comprising maintaining reception of the downlink signal via the primary antenna upon the switching back the transmission of the uplink signal from the secondary antenna to the primary antenna.

20. The method of claim 18 , wherein the first threshold is different than the second threshold.