Datalink preferred channel selection

• US 20020009993A1
• Filed: 05/22/2001
• Published: 01/24/2002
• Est. Priority Date: 07/05/2000
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Manberg, Charles C., Vollmer, Mark A., Dastrup, Therin L.
• Granted Patent: US 7,027,812 B2
• 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

Abstract

An apparatus, method and computer program product that utilizes user defined channel and frequency preferences to effect airborne voice and data telecommunications.

Claims

1. A method for aircraft telecommunications comprising the steps of:

identifying a current service volume;

identifying an available VHF communications channel frequency from a table of preferred VHF communications frequencies associated with said current service volume;

selecting a preferred communications attribute from a table of attributes associated with said current service volume and according to said available VHF communications channel frequency; and

effecting airborne communications utilizing said preferred communications attribute.

2. The method of claim 1 wherein said predefined service volumes comprise geographic regions other than rectangular regions.

3. The method of claim 1 wherein said service volumes further include at least one subset of area.

4. The method of claim 1 wherein said step of selecting a preferred communications attribute includes the step of selecting a VHF communications channel.

5. The method of claim 1 wherein said step of selecting a preferred communications attribute includes the step of selecting a SATCOM communications channel.

6. The method of claim 1 wherein said step of selecting a preferred communications attribute includes the step of selecting an HF communications channel.

7. The method of claim 1 further comprising the step of manually selecting a second preferred communications attribute different than said preferred communications attribute.

8. The method of claim 1 wherein said step of identifying a current service volume further comprises the steps of:

determining a current aircraft position; and

comparing said current aircraft position with a set of predefined service volumes to identify the current service volume encompassing said current aircraft position.

26. The communications apparatus of claim 7 wherein said apparatus comprises an Airborne Communications Addressing and Reporting System (ACARS) Management Unit.

9. A method for aircraft telecommunications comprising the steps of:

defining a plurality of service volumes having nonrectangular boundaries;

associating a set of preferred communications attributes with each of said plurality of service volumes;

identifying a current service volume;

selecting a preferred communications attribute from said set of preferred communications attributes associated with said current service volume; and

effecting airborne communications utilizing said preferred communications attribute.

10. The method of aircraft telecommunications of claim 9 wherein said step of selecting a preferred communications attribute further comprises the step of selecting a preferred communications channel.

11. The method of aircraft telecommunications of claim 9 wherein said step of defining a plurality of service volumes further comprises the step of defining at least one area located within at least one service volume.

12. The method of aircraft telecommunications of claim 9 wherein said step of identifying a current service volume comprises the step of identifying a current position of the aircraft.

13. A computer program product for use on an aircraft, the computer program product comprising:

a computer readable storage medium having computer readable program code means embodied in said medium, said computer readable program code means comprising;

a first computer instruction means for identifying a current service volume to be used for airborne communications;

a second computer instruction means for identifying an available VHF communications channel frequency from a table of preferred VHF communications frequencies associated with said current service volume;

a third computer instruction for selecting a preferred communications attribute from a table of attributes associated with said current service volume and according to said available VHF communications channel frequency; and

a fourth computer instruction means for effecting airborne communications utilizing said preferred communications attribute.

14. The computer program product of claim 13 wherein said first computer instruction means further includes a fifth computer instruction means for reading a current position of the aircraft.

15. The computer program product of claim 13 wherein said fourth computer instruction means selects a preferred communications channel.

16. The computer program product of claim 13 wherein said first computer instruction means further includes a fifth computer instruction means for identifying a current service area located within said current service volume.

17. A communications apparatus for effecting airborne communications comprising:

an input for receiving a message to be transmitted from an aircraft;

a logic device for identifying a preferred communications attribute to be utilized in transmitting said message as a function of;

a service volume; and

at least one of a VHF frequency preference and a channel preference; and

a router for effecting airborne communications according to said preferred communications attribute.

18. The communications apparatus of claim 17 wherein said logic device comprises a computer readable medium.

19. The communications apparatus of claim 18 wherein said computer readable medium comprises a PCMCIA card.

20. The communications apparatus of claim 17 wherein said logic device comprises a programmable logic device.

21. The communications apparatus of claim 17 wherein said input is coupled to receive a position information of the aircraft and wherein said preferred communications attribute is determined according to said position information.

22. The communications apparatus of claim 17 further comprising a controller useful for controlling display of communications information on a cockpit display.

23. The communications apparatus of claim 17 wherein said apparatus comprises a CMU.

24. The communications apparatus of claim 17 wherein said apparatus comprises an Air Traffic Service Unit (ATSU).

25. The communications apparatus of claim 17 wherein said apparatus comprises a Data Management Unit (DMU).