Methods and systems for providing high-speed connectivity to aircraft
Methods for providing high-speed connectivity to an aircraft in flight from a satellite. Example methods include transmitting first radio frequency signals from a wide-beam antenna at the satellite at a beamwidth of at least 6 degrees orbital arc to provide a wide coverage area. The first radio frequency signals are transmitted at a first frequency of at least 10 gigahertz and at a low equivalent isotropic radiated power. The method also includes receiving second radio frequency signals from a mobile antenna located on the aircraft, wherein the second radio frequency signals are received at a second frequency of at least 13.75 gigahertz, and the second frequency is different than the first frequency.
1. A method for providing high-speed connectivity to an aircraft in flight from a geosynchronous satellite, the method comprising:
transmitting first radio frequency signals from a wide-beam antenna at the satellite towards Earth at a beamwidth of at least 6 degrees orbital arc to provide a wide coverage area, wherein the first radio frequency signals are transmitted at a first frequency of at least 10 gigahertz and at a low equivalent isotropic radiated power to avoid interference with ground stations or receivers of adjacent satellite operators; and
receiving second radio frequency signals from a mobile antenna located on the aircraft, wherein the second radio frequency signals are received at a second frequency of at least 13.75 gigahertz, and the second frequency is different than the first frequency,
wherein the second radio frequency signals are received at the satellite via a second satellite antenna, and wherein the second satellite antenna comprises a spot beam antenna.
2. The method of claim 1 , wherein the first frequency and the second frequency are within the Ku-band or Ka-band.
3. The method of claim 1 , wherein the first frequency is within the Ku-band and the low equivalent isotropic radiated power (EIRP) is a peak EIRP of 54 dBW or less.
4. The method of claim 1 , wherein the first frequency is within the Ka-band and the low equivalent isotropic radiated power (EIRP) is a peak EIRP of 61 dBW or less.
5. The method of claim 1 , wherein the low equivalent isotropic radiated power comprises an EIRP of no more than 46 dBW at the wide coverage area contour.
6. The method of claim 1 , wherein the spot beam antenna is a steerable antenna for tracking the aircraft during its flight path.
7. The method of claim 1 , wherein the aircraft is travelling at a height of at least 3 kilometers above sea level.
8. The method of claim 1 , further comprising providing RF-based communications from the aircraft to a coverage zone at ground level, and wherein the RF-based communications are relayed through the satellite.
9. The method of claim 1 , wherein the aircraft is an unmanned aircraft.
10. A geosynchronous satellite system for providing high-speed connectivity to an aircraft in flight, the satellite system comprising:
a wide-beam antenna;
a transmitter configured to transmit first radio frequency signals from the wide-beam antenna at the satellite towards Earth at a beamwidth of at least 6 degrees orbital arc to provide a wide coverage area, wherein the first radio frequency signals are transmitted at a first frequency of at least 10 gigahertz and at a low equivalent isotropic radiated power to avoid interference with ground stations or receivers of adjacent satellite operators;
a receiver configured to receive second radio frequency signals from a mobile antenna located on the aircraft, wherein the second radio frequency signals are received at a second frequency of at least 13.75 gigahertz, and the second frequency is different than the first frequency; and
a second satellite antenna connected to the receiver, and wherein the second radio frequency signals are received at the satellite via the second satellite antenna, and wherein the second satellite antenna comprises a spot beam antenna.
11. The satellite system of claim 10 , wherein the first frequency and the second frequency are within the Ku-band or Ka-band.
12. The satellite system of claim 10 , wherein the first frequency is within the Ku-band and the low equivalent isotropic radiated power (EIRP) is a peak EIRP of 54 dBW or less.
13. The satellite system of claim 10 , wherein the first frequency is within the Ka-band and the low equivalent isotropic radiated power (EIRP) is a peak EIRP of 61 dBW or less.
14. The satellite system of claim 10 , wherein the low equivalent isotropic radiated power comprises an EIRP of no more than 46 dBW at the wide coverage area contour.
15. The satellite system of claim 10 , wherein the spot beam antenna is a steerable antenna for tracking the aircraft during its flight path.
16. The satellite system of claim 10 , wherein the wide beam antenna and transmitter are configured to communicate with the aircraft when it is travelling at a height of at least 3 kilometers above sea level without causing interference with at ground level with adjacent satellite operators.
17. The satellite system of claim 10 , wherein the aircraft is configured to provide RF-based communications from the aircraft to a coverage zone at ground level, and wherein the RF-based communications are relayed through the satellite.
18. A geosynchronous satellite for providing high-speed connectivity to an aircraft in flight, the satellite comprising:
a wide-beam antenna;
a transmitter configured to transmit first radio frequency signals from the wide-beam antenna towards Earth to a wide coverage area using a beamwidth of at least 6 degrees orbital arc, wherein the first radio frequency signals are transmitted at a first frequency of at least 10 gigahertz and at a low equivalent isotropic radiated power to avoid interference with ground stations or receivers of adjacent satellite operators;
a spot beam antenna; and
a receiver configured to receive second radio frequency signals through the spot beam antenna from a mobile antenna located on the aircraft, wherein the second radio frequency signals are received at a second frequency of at least 13.75 gigahertz, and the second frequency is different than the first frequency.
19. The satellite of claim 18 , wherein the spot beam antenna is a steerable antenna for tracking the aircraft along its flight path.