SYSTEM AND METHOD FOR IN-FLIGHT WIRELESS COMMUNICATION

• US 20090318138A1
• Filed: 06/20/2008
• Published: 12/24/2009
• Est. Priority Date: 06/20/2008
• Status: Abandoned Application

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: LaBerge, E.F. Charles, Zeng, Dongsong
• Application Number:
  US12/143,343
• Publication Number:
  US 20090318138A1
• Time in Patent Office: Days
• US Class Current: 455/431
• CPC Class Codes: H04B 7/18506 Communications with or from aircraft, i.e. aeronautical mobile service
• CPC Class Codes: H04W 16/14 Spectrum sharing arrangements between different networks
• CPC Class Codes: H04W 8/005 Discovery of network devices, e.g. terminals
• CPC Class Codes: H04W 84/06 Airborne or Satellite Networks space-based or airborne stations H04B7/185

Abstract

An aircraft radio comprises a transmitter configured to transmit wireless signals over a transmit frequency; a receiver configured to receive wireless signals over a receive frequency; and a processing unit configured to adjust the transmission frequency of the aircraft radio based on received sensor data in order to avoid interference with other wireless transmissions; wherein the processing unit is further configured to determine if a ground station is in range of the aircraft radio and to communicate directly with a second aircraft radio on another aircraft when a ground station is not in range.

Claims

1. An aircraft radio comprising:

a transmitter configured to transmit wireless signals over a transmit frequency;

a receiver configured to receive wireless signals over a receive frequency; and

a processing unit configured to adjust the transmission frequency of the aircraft radio based on received sensor data in order to avoid interference with other wireless transmissions;

wherein the processing unit is further configured to determine if a ground station is in range of the aircraft radio and to communicate directly with a second aircraft radio on another aircraft when a ground station is not in range.

2. The aircraft radio of claim 1, wherein the transmit frequency and the receive frequency are in the spectrum assigned to analog television broadcasts.

3. The aircraft radio of claim 1, wherein the analog television broadcast spectrum comprises the frequency ranges of 54-72 MHz, 76-88 MHz, 174-216 MHz, and 470-698 MHz.

4. The aircraft radio of claim 1, wherein the processing unit is further configured to adjust at least one of the transmission power and modulation scheme based on the received sensor data.

5. The aircraft radio of claim 1, wherein the processing unit is further configured to provide the received sensor data to a ground station when in range, and to adjust the transmit frequency based on commands received from the ground station.

6. The aircraft radio of claim 1, wherein the processing unit is configured to discover network topology when not in range of a ground station.

7. An aircraft communication system comprising:

at least one sensor configured to provide data regarding the environment surrounding the aircraft communication system;

a scanner configured to perform distributed measurement of a set frequency spectrum;

a radio coupled to the at least one sensor and the scanner, the radio configured to adjust the transmission frequency of the radio based on data received from the at least one sensor and the scanner in order to avoid interference with other wireless transmissions;

wherein the radio is further configured to determine if a ground station is in range and to communicate directly with a second aircraft'"'"'s radio when a ground station is not in range.

8. The aircraft communication system of claim 7, wherein the scanner is configured to perform distributed measurement of a frequency spectrum assigned to analog television broadcasts.

9. The aircraft communication system of claim 8, wherein the frequency spectrum includes the frequency ranges of 54-72 MHz, 76-88 MHz, 174-216 MHz, and 470-698 MHz.

10. The aircraft communication system of claim 7, wherein the at least one sensor includes one or more of an altimeter, a global positioning system (GPS) receiver, an Automatic Dependent Surveillance-Broadcast (ADS-B) receiver, and an accelerometer.

11. The aircraft communication system of claim 7, wherein the radio is further configured to provide the received sensor data to a ground station when in range, and to adjust the transmit frequency based on commands received from the ground station.

12. The aircraft communication system of claim 7, wherein the radio is configured to discover network topology when not in range of a ground station.

13. The aircraft communication system of claim 12, wherein the radio is further configured to select a transmission path from the aircraft to a ground station based on the discovered network topology.

14. The aircraft communication system of claim 7, wherein the radio is configured to forward wireless communication signals received from other aircraft.

15. A method of providing in-flight personal wireless communication on a first aircraft, the method comprising:

receiving data from a device on the first aircraft;

determining if a ground station is in range;

when a ground station is in range, transmitting the received data to the ground station over a frequency assigned by the ground station; and

when a ground station is not in range,

discovering network topology;

selecting a transmission path;

selecting a transmission frequency to avoid interference with other wireless transmissions; and

transmitting the data on the selected transmission frequency.

16. The method of claim 15, wherein selecting a transmission frequency comprises selecting a transmission frequency from a frequency spectrum assigned to analog television broadcasts.

17. The method of claim 16, wherein selecting a transmission frequency comprises selecting a transmission frequency from the frequency ranges of 54-72 MHz, 76-88 MHz, 174-216 MHz, and 470-698 MHz.

18. The method of claim 15, wherein discovering network topology comprises:

broadcasting a discovery message from the first aircraft;

forwarding the broadcast message via additional aircraft until a ground station is reached;

broadcasting a discovery response from the ground station; and

forwarding the discovery response aggregated with information regarding each additional aircraft which forwards the discovery response until the first aircraft is reached;

analyzing the aggregated discovery responses to identify the additional aircraft between the first aircraft and the ground station.

19. The method of claim 15, wherein discovering network topology comprises:

obtaining automatic dependent surveillance-broadcast (ADS-B) information regarding aircraft surrounding the first aircraft;

determining which surrounding aircraft has priority to forward a discovery message from the first aircraft;

broadcasting the discovery message with the ADS-B information and an indication of which surrounding aircraft has priority to forward the discovery message;

forwarding the discovery message only from the surrounding aircraft with the highest priority;

receiving the forwarded message at additional aircraft within range of the surrounding aircraft with the highest priority;

forwarding the discovery message from the additional aircraft until a ground station is reached;

broadcasting a discovery response from the ground station;

forwarding the discovery response aggregated with information regarding each additional aircraft which forwards the discovery response until the first aircraft is reached; and

analyzing the aggregated discovery responses to identify the additional aircraft between the first aircraft and the ground station.

20. The method of claim 19, wherein determining which surrounding aircraft has the highest priority comprises at least one of:

determining which surrounding aircraft is located closest to a target ground station; and

determining which surrounding aircraft has priority based on airline agreements.