AIRCRAFT BROADBAND WIRELESS SYSTEM AND METHODS

• US 20090186611A1
• Filed: 12/17/2008
• Published: 07/23/2009
• Est. Priority Date: 12/18/2007
• Status: Abandoned Application

• Current Assignee: The Brown Family Trust
• Original Assignee: Voyant International Corporation
• Inventors: Stiles, W. Herschel, Wolcott, Theodore J., Waldman, Dana R., Gerhardt, Edward C.
• Application Number:
  US12/337,042
• Publication Number:
  US 20090186611A1
• Time in Patent Office: Days
• US Class Current: 455/431
• CPC Class Codes: H01Q 3/24 varying the orientation by switching energy from one active radiating element to another, e.g. for beam switching
• CPC Class Codes: H01Q 3/242 Circumferential scanning
• CPC Class Codes: H04B 7/18506 Communications with or from aircraft, i.e. aeronautical mobile service
• CPC Class Codes: H04W 84/005 Moving wireless networks
• CPC Class Codes: H04W 84/06 Airborne or Satellite Networks space-based or airborne stations H04B7/185

Abstract

A broadband wireless system includes a plurality of spaced-apart ground stations for transmitting and receiving signals to and from a respective plurality of aircraft. Each of the plurality of ground stations may include a ground station transceiver including a ground station antenna carried by a mechanically steered platform, a ground station router in communication with the ground station transceiver, and a ground station beacon transceiver in communication with the ground station router. An aircraft transceiver may be carried by each of the plurality of aircraft to be positioned in communication with one of the plurality of ground stations. The aircraft transceiver may include an aircraft antenna mounted to the aircraft, an aircraft transceiver carried by the aircraft and in communication with the aircraft antenna, and an aircraft radio transceiver carried by the aircraft and in communication with the aircraft beacon transceiver. The broadband wireless system may also include a network operations center in communication with each of the ground stations via a global communications network. A ground station transceiver may transmit signals to and receives signals from not more than one aircraft at a time and ground station antenna may track the aircraft with which it is in communication.

Claims

1. A broadband wireless system comprising:

a plurality of spaced-apart ground stations for transmitting and receiving signals to and from a respective plurality of aircraft, each of said plurality of ground stations comprising

at least one ground station transceiver including a ground station antenna carried by a mechanically steered platform;

at least one ground station router in communication with the at least one ground station transceiver, and

at least one ground station beacon transceiver in communication with the at least one ground station router;

an aircraft transceiver carried by each of the plurality of aircraft to be positioned in communication with one of the plurality of ground stations, said aircraft transceiver comprising

an aircraft antenna mounted to the aircraft,

an aircraft beacon transceiver carried by the aircraft and in communication with the aircraft antenna, and

an aircraft radio transceiver carried by the aircraft and in communication with the aircraft beacon transceiver; and

a network operations center in communication with each of said plurality of ground stations via a global communications network;

wherein the at least one ground station transceiver transmits signals to and receives signals from not more than one aircraft at a time; and

wherein the ground station antenna tracks the aircraft with which it is in communication.

2. A broadband wireless system according to claim 1 wherein the at least one ground station transceiver includes a ground station radio frequency transceiver and a ground station modem;

and wherein the ground station modem transmits at a rate up to about 70 Mb/s.

3. A broadband wireless system according to claim 1 wherein the at least one ground station transceiver operates in a burst mode;

and wherein the burst mode is defined by a transmission being sent from the ground station transceiver and received by the aircraft transceiver followed by a transmission being sent from the aircraft transceiver and being received by the ground station transceiver.

4. A broadband wireless system according to claim 1 wherein the at least one ground station transceiver and the aircraft radio transceiver operate in at least one of time-division duplex mode and frequency division duplex mode.

5. A broadband wireless system according to claim 1 wherein each of said plurality of ground stations further comprises a processor in communication with the at least one ground station transceiver, and at least one stepper motor in communication with the processor;

and wherein the at least one stepper motor steers the platform to move the ground station antenna responsive to the processor.

6. A broadband wireless system according to claim 5 wherein the processor is in communication with the aircraft transceiver;

and wherein the processor steers the platform based on signals received from the aircraft transceiver.

7. A broadband wireless system according to claim 6 wherein the signals received from the aircraft transceiver include GPS signals indicating a location of the aircraft to be positioned in communication with a respective one of the plurality of ground stations transceivers.

8. A broadband wireless system according to claim 1 wherein the aircraft radio transceiver is in communication with an aircraft router carried by the aircraft.

9. A broadband wireless system according to claim 8 wherein the aircraft router provides at least one connection to at least one aircraft service point;

and wherein the at least one aircraft service point includes at least one of an in flight entertainment system, an aircraft cockpit, at least one wireless access point and at least one pico/femto cell for connection to a service provider.

10. A broadband wireless system according to claim 8 wherein the aircraft router includes software to buffer the at least one connection to the at least one aircraft service point.

11. A broadband wireless system according to claim 1 further comprising an aircraft terminal processor in communication with the aircraft antenna to track the aircraft antenna towards the respective at least one ground station transceiver with which it is in communication.

12. A broadband wireless system according to claim 1 wherein signals transmitted between the aircraft transceiver and the plurality of ground station transceivers are transmitted using a high frequency so that a transmission beam associated with the signals being transmitted is narrow.

13. A broadband wireless system according to claim 1 wherein the aircraft beacon transceiver operates at or below 1 GHz.

14. A broadband wireless system according to claim 1 wherein the aircraft beacon transceiver operates in a band substantially similar to a communications link between the aircraft and the ground station transceiver.

15. A broadband wireless system according to claim 1 wherein the aircraft beacon transceiver transmits a service request message;

and wherein an available one of the plurality of ground station transceivers accepts the service request message and transmits a service accept message;

wherein the available one of the plurality of ground station transceivers is defined by a ground station transceiver that is not in communication with another aircraft.

16. A broadband wireless system according to claim 15 wherein the aircraft transceiver disconnects from communication with one of the plurality of ground station transceivers upon receipt of the service accept message from the available one of the plurality of ground stations transceivers.

17. A broadband wireless system according to claim 16 wherein signal transmission data rate and modulation format are modified when the aircraft transceiver disconnects from communication with one of the plurality of ground station transceivers and receives the service accept message from the available one of the plurality of ground station transceivers to maximize receipt of the service accept message.

18. A broadband wireless system according to claim 15 wherein the aircraft beacon transceiver transmits the service request message once every second.

19. A broadband wireless system according to claim 15 wherein the aircraft beacon transceiver transmits the service request message upon reaching a predetermined altitude.

20. A broadband wireless system according to claim 15 wherein the service request message identifies the aircraft and provides the GPS location of the aircraft.

21. A broadband wireless system according to claim 1 further comprising a ground station database in communication with the aircraft transceiver, the ground station database including ground station locations and points to the nearest ground station.

22. A broadband wireless system according to claim 15 wherein each of said plurality of ground stations has a predetermined coverage range;

wherein the aircraft sends a service request message to a closest available ground station transceiver and receives a service accept message prior to disconnecting from the ground station transceiver with which it is in communication.

23. A broadband wireless system comprising:

a plurality of spaced-apart ground stations for transmitting and receiving signals to and from a respective plurality of aircraft, each of said plurality of ground stations comprising

a ground station antenna subsystem including a plurality of ground station antennas arranged in a stacked formation;

a ground station router in communication with the plurality of ground station antennas, and

a ground station beacon transceiver in communication with the ground station router;

an aircraft transceiver carried by each of the plurality of aircraft to be positioned in communication with one of the plurality of ground stations, said aircraft transceiver comprising

an aircraft antenna mounted to the aircraft,

an aircraft beacon transceiver carried by the aircraft and in communication with the aircraft antenna, and

an aircraft radio transceiver carried by the aircraft and in communication with the aircraft beacon transceiver; and

wherein the ground station antenna subsystem transmits signals to and receives signals from not more than one aircraft at a time.

24. A broadband wireless system according to claim 23 wherein the stacked formation of the plurality of ground station antennas includes a plurality of rings of ground station antennas.

25. A broadband wireless system according to claim 24 wherein the plurality of rings of ground station antennas includes five rings, wherein a lowermost one of the five rings includes a first predetermined plurality of ground station antennas;

wherein upper rings positioned above the lowermost one of the five rings includes less ground station antennas than the lowermost ring; and

wherein an uppermost one of the five rings includes one ground station antenna.

26. A broadband wireless system according to claim 23 wherein the ground station antenna subsystem includes a ground station radio frequency transceiver and a ground station modem;

and wherein the ground station modem transmits at a rate up to about 70 Mb/s.

27. A broadband wireless system according to claim 23 wherein the ground station antenna subsystem operates in a burst mode;

and wherein the burst mode is defined by a transmission being sent from the ground station antenna subsystem and received by the aircraft transceiver followed by a transmission being sent from the aircraft transceiver and being received by the ground station antenna subsystem.

28. A broadband wireless system according to claim 23 wherein the ground station antenna subsystem and the aircraft radio transceiver operate in at least one of time-division duplex mode and frequency division duplex mode.

29. A broadband wireless system according to claim 23 wherein the aircraft transceiver transmits GPS signals indicating a location of the aircraft to be positioned in communication with a respective one of the plurality of ground station antenna subsystems.

30. A broadband wireless system according to claim 23 wherein the aircraft radio transceiver is in communication with an aircraft router carried by the aircraft.

31. A broadband wireless system according to claim 30 wherein the aircraft router provides at least one connection to at least one aircraft service point;

and wherein the at least one aircraft service point includes at least one of an in flight entertainment system, an aircraft cockpit, at least one wireless access point and at least one pico/femto cell for connection to a service provider.

32. A broadband wireless system according to claim 31 wherein the aircraft router includes software to buffer the at least one connection to the at least one aircraft service point.

33. A broadband wireless system according to claim 23 further comprising an aircraft terminal processor carried by the aircraft and in communication with the aircraft antenna to track the aircraft antenna towards the respective at least one ground station antenna subsystem with which it is in communication.

34. A broadband wireless system according to claim 23 wherein signals transmitted between the aircraft transceiver and the respective ground station antenna subsystem with which it is in communication are transmitted using a high frequency so that a transmission beam associated with the signals being transmitted is narrow.

35. A broadband wireless system according to claim 23 wherein the aircraft beacon transceiver operates at or below 1 GHz.

36. A broadband wireless system according to claim 23 wherein the aircraft beacon transceiver operates in a band substantially similar to a communications link between the aircraft and the ground station antenna subsystem.

37. A broadband wireless system according to claim 23 wherein the aircraft beacon transceiver transmits a service request message;

and wherein an available one of the plurality of ground station antenna subsystems accepts the service request message and transmits a service accept message;

wherein the available one of the plurality of ground station antenna subsystems is defined by a ground station antenna subsystem that is not in communication with another aircraft.

38. A broadband wireless system according to claim 37 wherein the aircraft transceiver disconnects from communication with one of the plurality of ground station antenna subsystems upon receipt of the service accept message from the available one of the plurality of ground station antenna subsystems.

39. A broadband wireless system according to claim 38 wherein signal transmission data rate and modulation format are modified when the aircraft transceiver disconnects from communication with one of the plurality of ground station antenna subsystems and receives the service accept message from the available one of the plurality of ground station antenna subsystems to maximize receipt of the service accept message.

40. A broadband wireless system according to claim 37 wherein the aircraft beacon transceiver transmits the service request message at least one of once every second and upon reaching a predetermined altitude;

and wherein the service request message identifies the aircraft and provides the GPS location of the aircraft.

41. A broadband wireless system according to claim 23 further comprising a ground station database in communication with the aircraft transceiver, the ground station database including ground station locations and open loop points to the nearest ground station.

42. A broadband wireless system according to claim 37 wherein each of said plurality of ground station antenna subsystems has a predetermined coverage range;

wherein the aircraft sends a service request message to a closest available ground station antenna subsystem and receives a service accept message prior to disconnecting from the ground station antenna subsystem with which it is in communication.

43. A method for providing broadband wireless access to a moving aircraft, the method comprising:

positioning a plurality of ground station transceivers of a respective plurality of ground stations in communication with a respective plurality of aircraft to transmit and receive signals to and from the respective plurality of aircraft, each of the plurality of ground stations comprising at least one ground station transceiver including a ground station antenna, at least one ground station router in communication with the at least one ground station transceiver, and at least one ground station beacon transceiver in communication with the at least one ground station router;

transmitting and receiving signals from the at least one ground station transceiver to one aircraft so that the at least one ground station transceiver is in communication with not more than one aircraft at a time; and

tracking the ground station antenna to the aircraft when the at least one ground station transceiver with which the ground station antenna is associated is in communication with the aircraft.

44. A method according to claim 43 further comprising positioning each of the plurality of ground stations in communication with a network operations center.

45. A method according to claim 43 wherein each of the plurality of aircraft include an aircraft transceiver to be positioned in communication with one of the plurality of ground station transceivers, each aircraft transceiver including an aircraft antenna mounted to the aircraft, an aircraft beacon transceiver carried by the aircraft and in communication with the aircraft antenna, and an aircraft radio transceiver carried by the aircraft and in communication with the aircraft beacon transceiver.

46. A method according to claim 43 wherein the at least one ground station transceiver includes a ground station radio frequency transceiver and a ground station modem;

and further comprising transmitting signals from the ground station modem at a rate up to about 70 Mb/s.

47. A method according to claim 45 further comprising operating the at least one ground station transceiver in a burst mode;

and wherein the burst mode is defined by transmitting a signal from the at least one ground station transceiver to the aircraft transceiver followed by transmitting a signal from the aircraft transceiver to the ground station transceiver; and

further comprising operating the at least one ground station transceiver and the aircraft radio transceiver in at least one of time-division duplex mode and frequency division duplex mode.

48. A method according to claim 45 wherein tracking the ground station antenna comprises mechanically steering the ground station antenna;

and further comprising steering the platform to move the ground station antenna responsive to a processor in communication with the at least one ground station transceiver;

wherein the processor is in communication with the aircraft transceiver and steers the platform based on signals received from the aircraft transceiver.

49. A method according to claim 45 further comprising transmitting GPS signals from the aircraft transceiver to the ground station transceiver to indicate a location of the aircraft to be positioned in communication with a respective one of the plurality of ground stations.

50. A method according to claim 45 wherein the aircraft radio transceiver is in communication with an aircraft router carried by the aircraft;

wherein the aircraft router provides at least one connection to at least one aircraft service point; and

wherein the at least one aircraft service point includes at least one of an in flight entertainment system, an aircraft cockpit, at least one wireless access point and at least one pico/femto cell for connection to a service provider; and

further comprising buffering the at least one connection to the at least one aircraft service point.

51. A method according to claim 45 further comprising tracking the aircraft antenna towards the respective at least one ground station transceiver with which it is in communication.

52. A method according to claim 45 further comprising using a high frequency to transmit signals between the aircraft transceiver and the at least one ground station transceiver so that a transmission beam associated with the signals being transmitted is narrow.

53. A method according to claim 45 wherein the aircraft beacon transceiver operates at or below 1 GHz.

54. A method according to claim 45 wherein the aircraft beacon transceiver operates in a band substantially similar to a communications link between the aircraft and the at least one ground station transceiver.

55. A method according to claim 45 further comprising transmitting a service request message from the aircraft beacon transceiver to an available one of the plurality of ground station transceivers and wherein the available one of the plurality of ground station transceivers accepts the service request message;

and transmitting a service accept message from the available one of the ground station transceivers;

wherein the available one of the plurality of ground station transceivers is defined by a ground station transceiver that is not in communication with another aircraft.

56. A method according to claim 55 further comprising disconnecting the aircraft transceiver from communication with one of the plurality of ground station transceivers upon receipt of the service accept message from the available one of the plurality of ground station transceivers.

57. A method according to claim 56 further comprising modifying signal transmission data rate and modulation format when the aircraft transceiver disconnects from communication with one of the plurality of ground station transceivers and receives the service accept message from the available one of the plurality of ground station transceivers to maximize receipt of the service accept message.

58. A method according to claim 55 wherein transmitting the service request message comprises at least one of transmitting the service request message once every second and transmitting the service request message upon the aircraft reaching a predetermined altitude;

and wherein the service request message identifies the aircraft and provides the GPS location of the aircraft.

59. A method according to claim 55 wherein each of the plurality of ground station transceivers has a predetermined coverage range;

wherein the aircraft sends a service request message to a closest available one of the plurality of ground station transceivers and receives a service accept message prior to disconnecting from the ground station transceiver with which it is in communication.

60. A method for providing broadband wireless access to a moving aircraft, the method comprising:

positioning a plurality of ground station antenna subsystems of a respective plurality of ground stations in communication with a respective plurality of aircraft to transmit and receive signals to and from the respective plurality of aircraft, each of the ground station antenna subsystem including a plurality of ground station antennas arranged in a stacked formation, a ground station router in communication with the plurality of ground station antennas, and a ground station beacon transceiver in communication with the ground station router; and

transmitting and receiving signals from the ground station antenna subsystem to one aircraft so that the ground station antenna subsystem is in communication with not more than one aircraft at a time.

61. A method according to claim 60 wherein the stacked formation of the plurality of ground station antennas includes a plurality of rings of ground station antennas.

62. A method according to claim 61 wherein the plurality of rings of ground station antennas includes five rings, wherein a lowermost one of the five rings includes a first predetermined plurality of ground station antennas, and upper rings positioned above the lowermost one of the five rings includes less ground station antennas than the lowermost ring, and wherein an uppermost one of the five rings includes one ground station antenna.

63. A method according to claim 60 wherein each of the plurality of aircraft include an aircraft transceiver to be positioned in communication with one of the plurality of ground stations, each aircraft transceiver including an aircraft antenna mounted to the aircraft, an aircraft beacon transceiver carried by the aircraft and in communication with the aircraft antenna, and an aircraft radio transceiver carried by the aircraft and in communication with the aircraft beacon transceiver.

64. A method according to claim 63 wherein the ground station antenna subsystem includes a ground station radio frequency transceiver and a ground station modem;

and further comprising transmitting signals from the ground station modem at a rate up to about 70 Mb/s.

65. A method according to claim 63 further comprising operating the ground station antenna subsystem in a burst mode;

and wherein the burst mode is defined by transmitting a signal from the ground station antenna subsystem to the aircraft transceiver followed by transmitting a signal from the aircraft transceiver to the ground station antenna subsystem.

66. A method according to claim 63 further comprising operating the ground station antenna subsystem and the aircraft radio transceiver operate in at least one of time-division duplex mode and frequency division duplex mode.

67. A method according to claim 63 further comprising transmitting GPS signals from the aircraft transceiver to the ground station antenna subsystem to indicate a location of the aircraft to be positioned in communication with a respective one of the plurality of ground station antenna subsystems.

68. A method according to claim 63 wherein the aircraft radio transceiver is in communication with an aircraft router carried by the aircraft;

wherein the aircraft router provides at least one connection to at least one aircraft service point; and

wherein the at least one aircraft service point includes at least one of an in flight entertainment system, an aircraft cockpit, at least one wireless access point and at least one pico/femto cell for connection to a service provider; and

further comprising buffering the at least one connection to the aircraft service point.

69. A method according to claim 63 further comprising tracking the aircraft antenna towards the respective at least one ground station antenna subsystem with which it is in communication.

70. A method according to claim 63 further comprising using a high frequency to transmit signals between the aircraft transceiver and the plurality of ground station antenna subsystem with which it is in communication so that a transmission beam associated with the signals being transmitted is narrow.

71. A method according to claim 63 wherein the aircraft beacon transceiver operates at or below 1 GHz.

72. A method according to claim 63 wherein the aircraft beacon transceiver operates in a band substantially similar to a communications link between the aircraft and the ground station antenna subsystem.

73. A method according to claim 63 further comprising transmitting a service request message from the aircraft beacon transceiver to an available one of the plurality of ground station antenna subsystems and wherein the available one of the plurality of ground station antenna subsystems accepts the service request message;

and transmitting a service accept message from the available one of the ground station antenna subsystems;

wherein the available one of the plurality of ground station antenna subsystems is defined by a ground station antenna subsystem that is not in communication with another aircraft.

74. A method according to claim 73 further comprising disconnecting the aircraft transceiver from communication with one of the plurality of ground station antenna subsystems upon receipt of the service accept message from the available one of the plurality of ground station antenna subsystems.

75. A method according to claim 74 further comprising modifying signal transmission data rate and modulation format when the aircraft transceiver disconnects from communication with one of the plurality of ground station antenna subsystems and receives the service accept message from the available one of the plurality of ground station antenna subsystems to maximize receipt of the service accept message.

76. A method according to claim 73 wherein transmitting the service request message comprises at least one of transmitting the service request message once every second and transmitting the service request message upon reaching a predetermined altitude;

and wherein the service request message identifies the aircraft and provides the GPS location of the aircraft.

77. A method according to claim 73 wherein each of the plurality of ground station antenna subsystems has a predetermined coverage range;

wherein the aircraft sends a service request message to a closest available ground station antenna subsystem and receives a service accept message prior to disconnecting from the ground station antenna subsystem with which it is in communication.