Architecture for simultaneous spectrum usage by air-to-ground and terrestrial networks
A network for providing air-to-ground (ATG) wireless communication in various cells may include an in-flight aircraft including an antenna assembly, a plurality of ATG base stations, a plurality of terrestrial base stations. Each of the ATG base stations defines a corresponding radiation pattern, and the ATG base stations are spaced apart from each other to define at least partially overlapping coverage areas to communicate with the antenna assembly in an ATG communication layer defined between a first altitude and a second altitude. The terrestrial base stations are configured to communicate primarily in a ground communication layer below the first altitude. The terrestrial base stations and the ATG base stations are each configured to communicate using the same radio frequency (RF) spectrum in the ground communication layer and ATG communication layer, respectively.
1. A system for supporting air-to-ground (ATG) wireless communication in various cells, the system comprising:
a plurality of ATG base stations, each of which defines a corresponding radiation pattern focusing energy toward the horizon, wherein the ATG base stations are spaced apart from each other to define at least partially overlapping coverage areas forming an ATG communication layer defined between a first altitude and a second altitude; and
an antenna assembly of an aircraft, the antenna assembly being configured to communicate with the ATG base stations in the ATG communication layer above a terrestrial communication layer defined by terrestrial transmitters configured to communicate with user equipment located on the ground in a ground communication layer below the first altitude,
wherein the antenna assembly comprises a blade antenna,
wherein the blade antenna comprises multiple transmission elements having selectable directivity, and
wherein the blade antenna is configured to employ side lobe suppression techniques to reduce interference with the terrestrial transmitters.
2. The system of claim 1 , wherein the blade antenna is operably coupled to a remote radio head on the aircraft.
3. The system of claim 2 , wherein the blade antenna is disposed at a first portion of the aircraft and another antenna is disposed at a second portion of the aircraft.
4. The system of claim 3 , wherein the blade antenna operates in the same frequency band as at least some of the terrestrial transmitters.
5. The system of claim 1 , wherein the blade antenna is disposed on a bottom surface of the aircraft.
6. The system of claim 5 , wherein the blade antenna is configured to be electrically steered to steer a radiation pattern of the blade antenna toward the horizon.
7. The system of claim 6 , wherein steering of the blade antenna is performed to compensate for pitch and roll of the aircraft.
8. The system of claim 5 , wherein the blade antenna is configured to be electrically steered to have a narrow horizontal pattern in azimuth.
9. The system of claim 8 , wherein the blade antenna is configured to be electrically steered to have a wide vertical pattern.
10. The system of claim 1 , wherein the antenna assembly is configured to communicate with the ATG base stations using unlicensed band frequencies of about 2.4 GHz or 5.8 GHz.
11. An antenna assembly for an aircraft, the antenna assembly being configured to wirelessly communicate in an air-to-ground (ATG) wireless communication network, the antenna assembly being configured to employ steerable beams to communicate with ATG base stations in an ATG communication layer defined above a terrestrial communication layer formed by terrestrial base stations configured to communicate with user equipment located on the ground in a ground communication layer below a first altitude,
wherein the antenna assembly comprises multiple antenna elements housed within a long blade, and
wherein the antenna assembly is configured to communicate with the ATG base stations using unlicensed band frequencies of about 2.4 GHz or 5.8 GHz.
12. The antenna assembly of claim 11 , wherein the long blade is operably coupled to a remote radio head.
13. The antenna assembly of claim 12 , wherein the antenna assembly comprises a second antenna disposed at a second portion of the aircraft relative to a first portion of the aircraft at which the long blade is disposed.
14. The antenna assembly of claim 11 , wherein the multiple antenna elements of the long blade are configured to generate a horizon focused beam pattern.
15. The antenna assembly of claim 14 , wherein the long blade is disposed on a bottom surface of the aircraft.
16. The antenna assembly of claim 15 , wherein the multiple antenna elements of the long blade are configured to be electrically steered to steer a radiation pattern of the multiple antenna elements toward the horizon.
17. The antenna assembly of claim 16 , wherein steering of the multiple antenna elements is performed to compensate for pitch and roll of the aircraft.
18. The antenna assembly of claim 15 , wherein the multiple antenna elements are configured to be electrically steered to have a narrow horizontal pattern in azimuth.
19. The antenna assembly of claim 18 , wherein the multiple antenna elements are configured to be electrically steered to have a wide vertical pattern.
20. The antenna assembly of claim 11 , wherein the blade antenna is configured to employ side lobe suppression techniques to reduce interference with the terrestrial base stations.