Smart antenna for airborne cellular system

• US 6,642,894 B1
• Filed: 03/11/2002
• Issued: 11/04/2003
• Est. Priority Date: 09/13/1999
• Status: Expired due to Fees

• Current Assignee: Torsal Technology Group Limited LLC (Intellectual Ventures LLC)
• Original Assignee: Motorola, Inc. (Motorola Solutions, Inc.)
• Inventors: Emmons, Thomas Peter Jr., Gross, Jonathan H., Startup, James W., Hanson, Duke E.
• Primary Examiner(s): Wong, Don
• Assistant Examiner(s): DINH, TRINH VO
• Application Number:
  US10/070,844
• Time in Patent Office: 603 Days
• Field of Search: H01/Q.128, H04/Q.720, 343/705, 343/706, 342/352, 342/354, 342/357, 342/359, 342/360, 342/361, 455/12.1, 455/431, 455/13.1, 455/11.1
• US Class Current: 343/705
• CPC Class Codes: H01Q 1/28 Adaptation for use in or on aircraft, missiles, satellites, or balloons
• CPC Class Codes: H01Q 21/29 Combinations of different interacting antenna units for giving a desired directional characteristic H01Q25/00 takes precedence
• CPC Class Codes: H01Q 3/2605 Array of radiating elements provided with a feedback control over the element weights, e.g. adaptive arrays
• CPC Class Codes: H04B 7/18506 Communications with or from aircraft, i.e. aeronautical mobile service

Abstract

An airborne repeater antenna array (70) in which beams transmitted from multiple antenna elements (80) of the array to form terrestrial communications. cells are shaped according to predetermined system parameters. At least one of airplane telemetry data (58) indicating an airplane flight pattern location, adjacent cellular system beam footprint data, and call distribution load within a terrestrial cell are received, and a complex gain is dynamically computed for each of the multiple antenna elements based on such data to thereby output a plurality of beams that form desired geographic communications coverage cells (100, 102, 104, 108).

Claims

1. An aircraft-based cellular communications system, comprising:

a base transceiving station for switching calls to call destinations;

an aircraft including a beamformer for generating communications beams, an antenna having a plurality of antenna elements and corresponding amplifiers for transmitting the beams to form terrestrial communications cells that create a link between wireless communications devices within the terrestrial cells and the base transceiving station, and a telemetry link between the base transceiving station and the beamformer;

the base transceiving station including a beam shape optimizer for computing a complex gain of the antenna amplifiers based on mapping of the aircraft flight and location data to stored communications coverage cell coefficient data and for transmitting the complex gain to the antenna amplifiers of the beamformer via the telemetry link to control shapes of each of the communications coverage cells.

2. The aircraft-based cellular communications system of claim 1, wherein the beam shape optimizer dynamically computes the complex gain of the antenna amplifiers to compensate for beam pattern movement caused by movement of the aircraft.

3. The aircraft-based cellular communications system of claim 2, wherein the movement of the aircraft comprises airplane pitch, roll and yaw.

4. The aircraft-based cellular communications system of claim 1, wherein the beam shape optimizer dynamically computes the complex gain of the antenna amplifiers to adjust each of the geographic communications coverage cells based on population within the cell.

5. The aircraft-based cellular communications system of claim 1, wherein the beam shape optimizer dynamically computes the complex gain of the antenna amplifiers to minimize interference with geographic communications coverage cells of other systems.

6. The aircraft-based cellular communications system of claim 1, wherein the beam shape optimizer dynamically computes the complex gain of the antenna elements to minimize beam interference and thereby reduce overall system loading.

7. The aircraft-based cellular communications system of claim 1, wherein the beam shape optimizer dynamically computes the complex gain of the antenna elements to reduce angular spread on transmit and receive paths of antenna element beams to thereby reduce multipath Doppler spread within each geographic communications coverage cell of each of the multiple antenna elements.

8. The aircraft-based cellular communications system of claim 1, wherein the beam shape optimizer dynamically computes the complex gain of the antenna elements to re-allocate call traffic within the geographic communications coverage cell of each of them multiple antenna elements to provide for more even system call distribution.

9. An optimizer for shaping communications beams transmitted from an airborne wireless communications system repeater antenna array, comprising a processor for computing a complex gain associated with the antenna array based on mapping of repeater location data to stored communications coverage cell coefficient data, and for transmitting the complex gain to the antenna array to optimize shapes of each of the communications coverage cells.

10. The optimizer of claim 9, wherein the processor is implemented with the airborne repeater.

11. The optimizer of claim 9, wherein the processor is implemented in a terrestrial base transceiving station and communicates with the antenna array via a telemetry link.

12. A method of managing operation of an airborne repeater antenna array comprising:

receiving at least one of airplane telemetry data indicating an airplane flight pattern location, adjacent cellular system beam footprint data, and call distribution load within an airplane beam footprint;

computing desired beam direction and shape parameters based on the at least one of airplane telemetry data indicating an airplane flight pattern location, adjacent cellular system beam footprint data, and call distribution load within an airplane beam footprint; and

calculating complex gains for each of multiple antenna elements to form a set of communications beams each having a desired direction and shape to thereby form terrestrial cells with corresponding locations and shapes.

13. The method of claim 12, wherein the computing of desired beam direction and shape parameters and the calculating of a complex gain for each of multiple antenna elements compensates for beam pattern movement caused by airplane movement.

14. The method of claim 13, wherein the airplane movement comprises airplane pitch, roll and yaw.

15. The method of claim 12, wherein the computing of desired beam direction and shape parameters and the calculating of a complex gain for each of multiple antenna elements comprise adjusting the communications beams to adjust the terrestrial cells based on population within each of the terrestrial cells.

16. The method of claim 12, wherein the computing of desired beam direction and shape parameters and the calculating of a complex gain for each of multiple antenna elements are performed to minimize interference with geographic communications coverage cells of other systems.

17. The method of claim 12, wherein the computing of desired beam direction and shape parameters and the calculating of a complex gain for each of multiple antenna elements comprise dynamically computing beam patterns of the communications beams to minimize inter-beam interference and thereby reduce overall system loading.

18. The method of claim 12, wherein the computing of desired beam direction and shape parameters and the calculating of a complex gain for each of multiple antenna elements accounts for angular spread of incident energy to reduce Doppler and delay spread impact.

19. The method of claim 12, wherein the computing of desired beam direction and shape parameters and the calculating of a complex gain for each of multiple antenna elements reallocates call traffic within the airplane beam footprint to balance load between the terrestrial cells.

20. A method of managing operation of an airborne repeater antenna including multiple planar antennas comprising:

receiving at least one of airplane telemetry data indicating an airplane flight pattern location, adjacent cellular system beam footprint data, and call distribution load within an airplane beam footprint;

computing desired beam direction and shape parameters based on the at least one of airplane telemetry data indicating an airplane flight pattern location, adjacent cellular system beam footprint data, and call distribution load within an airplane beam footprint; and

calculating a complex gain for multiple antenna elements for each of multiple planar antennas to form a set of communications beams each having a desired direction and shape to thereby form terrestrial cells with corresponding locations and shapes; and

switching beam traffic among the multiple antennas to maintain antenna scan angles within a predetermined range.

21. The method of claim 20, further comprising switching steering directions of each of the multiple planar antennas simultaneously with the switching of beam traffic among the multiple antennas to maintain antenna scan angles within a predetermined range.