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 base stations 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 steerable matrix antenna that is configured to be steered based on knowledge of respective locations of the ATG base stations.
2. The system of claim 1 , wherein the steerable matrix antenna comprises a first antenna element disposed at a first portion of the aircraft and a second antenna element disposed at a second portion of the aircraft.
3. The system of claim 2 , wherein the first antenna element is configured for fore and aft reception and the second antenna element is configured for reception on opposing sides of the aircraft.
4. The system of claim 3 , the first antenna element or the second antenna element is configured to be electrically steered or tilted to steer a radiation pattern of the corresponding one of the first and antenna element or the second antenna element toward the horizon.
5. The system of claim 4 , wherein steering or tilting of the corresponding one of the first and antenna element or the second antenna element is performed to compensate for pitch and roll of the aircraft.
6. The system of claim 1 , wherein the first antenna element or the second antenna element comprises a blade antenna.
7. The system of claim 6 , wherein the blade antenna comprises four or more transmission elements having selectable directivity.
8. The system of claim 7 , wherein the antenna assembly comprises a remote radio head having distributed elements, and wherein a distributed element is provided in communication with each of the first and second antenna elements.
9. 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 base stations 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 steerable matrix antenna,
wherein the steerable matrix antenna comprises a first antenna element disposed at a first portion of the aircraft and a second antenna element disposed at a second portion of the aircraft,
wherein the first antenna element is configured for fore and aft reception and the second antenna element is configured for reception on opposing sides of the aircraft, and
wherein the first antenna element or the second antenna element is configured to be mechanically steered or tilted to steer a radiation pattern of the corresponding one of the first and antenna element or the second antenna element toward the horizon.
10. The system of claim 9 , wherein steering or tilting of the corresponding one of the first and antenna element or the second antenna element is performed to compensate for pitch and roll of the aircraft.
11. An antenna assembly for an aircraft, the antenna element being configured to wirelessly communicate in an air-to-ground (ATG) wireless communication network, the antenna assembly comprising a steerable matrix antenna configured 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 ATG base stations each define 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 the first altitude and a second altitude, and
wherein the steerable matrix antenna is configured to be steered based on knowledge of respective locations of the ATG base stations.
12. The antenna assembly of claim 11 , wherein the steerable matrix antenna comprises a first antenna element disposed at a first portion of the aircraft and a second antenna element disposed at a second portion of the aircraft.
13. The antenna assembly of claim 12 , wherein the first antenna element is configured for fore and aft reception and the second antenna element is configured for reception on opposing sides of the aircraft.
14. The antenna assembly of claim 13 , the first antenna element or the second antenna element is configured to be mechanically steered or tilted to steer a radiation pattern of the corresponding one of the first and antenna element or the second antenna element toward the horizon.
15. The antenna assembly of claim 14 , wherein steering or tilting of the corresponding one of the first and antenna element or the second antenna element is performed to compensate for pitch and roll of the aircraft.
16. The antenna assembly of claim 13 , the first antenna element or the second antenna element is configured to be electrically steered or tilted to steer a radiation pattern of the corresponding one of the first and antenna element or the second antenna element toward the horizon.
17. The antenna assembly of claim 16 , wherein steering or tilting of the corresponding one of the first and antenna element or the second antenna element is performed to compensate for pitch and roll of the aircraft.
18. The antenna assembly of claim 11 , wherein the first antenna element or the second antenna element comprises a blade antenna.
19. The antenna assembly of claim 18 , wherein the blade antenna comprises four or more transmission elements having selectable directivity.
20. The antenna assembly of claim 19 , wherein the antenna assembly comprises a remote radio head having distributed elements, and wherein a distributed element is provided in communication with each of the first and second antenna elements.