System and method of assisted aerial navigation

• US 8,698,655 B2
• Filed: 10/03/2011
• Issued: 04/15/2014
• Est. Priority Date: 03/17/2008
• Status: Active Grant

• Current Assignee: Garmin International, Inc. (Garmin Limited)
• Original Assignee: Garmin International, Inc. (Garmin Limited)
• Inventors: Flanigan, Daniel Keegan, Flatland, Jay R., James, Merlin R., Schlef, Eric D.
• Primary Examiner(s): Swarthout, Brent
• Application Number:
  US13/251,912
• Publication Number:
  US 20120022727A1
• Time in Patent Office: 925 Days
• Field of Search: 340/972, 340/973, 340/974, 340/975, 340/976, 340/980, 701/9, 701/14, 701/16
• US Class Current: 340/972
• CPC Class Codes: G01C 23/005 Flight directors indicating arrangements specially adapted for rotary gyroscopes G01C19/32
• CPC Class Codes: G01S 19/15 Aircraft landing systems
• CPC Class Codes: G01S 19/48 by combining or switching between position solutions derived from the satellite radio beacon positioning system and position solutions derived from a further system

Abstract

A system and method of providing aerial navigation for an aircraft comprises presenting an enlarged virtual runway for an identified runway on a display, where the virtual area of the virtual runway remains substantially constant as the aircraft approaches the runway.

Claims

1. An aerial navigation system for an aircraft, said system comprising:

a user interface including a display;

a global positioning component operable to receive global positioning system signals and determine a current geographic location of the aircraft using the received signals;

a database including geographic coordinate information for a plurality of runways; and

a processing system operable to;

identify at least one of the runways using at least the current geographic location of the aircraft;

define a virtual runway around the identified runway, the virtual runway having a virtual area greater than the area of the identified runway defined by the geographic coordinate information stored within the database; and

control the display to present a visual indication of the virtual runway and the indentified runway, wherein the virtual area of the virtual runway remains substantially constant as the aircraft approaches the runway;

wherein the visual indication of the identified runway increases in size as the aircraft approaches the runway.

2. The system of claim 1, wherein the processing system is further operable to control the display to present a visual indication of the identified runway within the visual indication of the virtual runway.

3. The system of claim 1, wherein the visual indication of the identified runway approaches the size of the visual indication of the virtual runway as the aircraft approaches the runway.

4. The system of claim 3, wherein the processing system replaces the visual indication of the virtual runway with the visual indication of the identified runway at a geographic location in proximity to the identified runway.

6. The system of claim 1, wherein the database further includes terrain data including terrain coordinate information, the processing system being further operable to control the display to present a visual indication of the terrain data corresponding to the current geographic location of the aircraft.

5. An aerial navigation system for an aircraft, said system comprising:

a user interface including a display;

a global positioning component operable to receive global positioning system signals and determine a current geographic location of the aircraft using the received signals;

a database including geographic coordinate information for a plurality of runways; and

a processing system operable to;

identify at least one of the runways using at least the current geographic location of the aircraft;

define a virtual runway around the identified runway, the virtual runway having a virtual area greater than the area of the identified runway defined by the geographic coordinate information stored within the database; and

control the display to present a visual indication of the virtual runway and the indentified runway, wherein the virtual area of the virtual runway remains substantially constant as the aircraft approaches the runway;

wherein the visual indication of the virtual runway includes virtual runway numbers having a virtual area greater than the area of the identified runway defined by the geographic coordinate information stored within the database.

17. The system of claim 5, wherein the processing system is further operable to control the display to present a visual indication of the identified runway within the visual indication of the virtual runway.

18. The system of claim 17, wherein the visual indication of the identified runway approaches the size of the visual indication of the virtual runway as the aircraft approaches the runway.

19. The system of claim 18, wherein the processing system replaces the visual indication of the virtual runway with the visual indication of the identified runway at a geographic location in proximity to the identified runway.

20. The system of claim 5, wherein the database further includes terrain data including terrain coordinate information, the processing system being further operable to control the display to present a visual indication of the terrain data corresponding to the current geographic location of the aircraft.

7. An aerial navigation system for an aircraft, said system comprising:

a user interface including a display;

a global positioning component operable to receive global positioning system signals and determine a current geographic location of the aircraft using the received signals;

a database including geographic coordinate information for a plurality of runways; and

a processing system operable to;

identify at least one of the runways using at least the current geographic location of the aircraft;

define a virtual runway around the identified runway, the virtual runway having a virtual area greater than the area of the identified runway defined by the geographic coordinate information stored within the database;

at a first location determined by the global positioning component, control the display to present a visual indication of the virtual runway,

at a second location determined by the global positioning component, control the display to additionally present a visual indication of the identified runway within the visual indication of the virtual runway, wherein the second location is closer to the identified runway than the first location, and

at a third location determined by the global positioning component, control the display to increase the size of the visual indication of the identified runway, wherein the third location is closer to the identified runway than the second location,

wherein the virtual area of the displayed virtual runway remains substantially constant at the first location, the second location, and the third location.

8. The system of claim 7, wherein, at a fourth location determined by the global positioning component, the processing system is operable to replace the visual indication of the virtual runway with the visual indication of the identified runway, the fourth location being closer to the identified runway than the third location.

9. The system of claim 7, wherein the visual indication of the virtual runway includes virtual runway numbers having a virtual area greater than the area of the identified runway defined by the geographic coordinate information stored within the database.

10. The system of claim 7, wherein the database further includes terrain data including terrain coordinate information, the processing system being further operable to control the display to present a visual indication of the terrain data corresponding to the current geographic location of the aircraft.

11. A method for displaying a virtual runway on a display of an aerial navigation system positioned within an aircraft, the method comprising:

determining, using a processing system associated with the aerial navigation system, a current geographic location of the aircraft using a global positioning system;

identifying, using the processing system, a runway corresponding to the current geographic location of the aircraft;

defining, using the processing system, a virtual runway around the identified runway, the virtual runway having a virtual area greater than the area of the identified runway as defined by geographic coordinate information stored within a database associated with the aerial navigation system;

presenting, using the processing system, a visual indication of the virtual runway and the indentified runway on a display associated with the aerial navigation system, wherein the virtual area of the virtual runway remains substantially constant as the aircraft approaches the runway;

identifying, using the processing system, movement of the aircraft towards the identified runway using the current geographic location of the aircraft; and

increasing, using the processing system, the size of the visual indication of the identified runway as the aircraft approaches the runway.

12. The method of claim 11, further including presenting, using the processing system, a visual indication of the identified runway within the visual indication of the virtual runway.

13. The method of claim 11, wherein the visual indication of the identified runway approaches the size of the visual indication of the virtual runway as the aircraft approaches the runway.

14. The method of claim 13, further including replacing, using the processing system, the visual indication of the virtual runway with the visual indication of the identified runway at a geographic location in proximity to the identified runway.

16. The method of claim 11, further including:

accessing, using the processing system, a database of terrain data including terrain coordinate information; and

presenting, using the processing system, a visual indication of the terrain data corresponding to the current geographic location of the aircraft.

15. A method for displaying a virtual runway on a display of an aerial navigation system positioned within an aircraft, the method comprising:

determining, using a processing system, a current geographic location of the aircraft using a global positioning system;

identifying, using the processing system, a runway corresponding to the current geographic location of the aircraft;

defining, using the processing system, a virtual runway around the identified runway, the virtual runway having a virtual area greater than the area of the identified runway as defined by geographic coordinate information stored within a database associated with the aerial navigation system;

presenting, using the processing system, a visual indication of the virtual runway and the indentified runway on a display associated with the aerial navigation system, wherein the virtual area of the virtual runway remains substantially constant as the aircraft approaches the runway;

wherein the visual indication of the virtual runway includes virtual runway numbers having a virtual area greater than the area of the identified runway defined by the geographic coordinate information stored within the database.

21. The method of claim 15, further including presenting, using the processing system, a visual indication of the identified runway within the visual indication of the virtual runway.

22. The method of claim 15, wherein the visual indication of the identified runway approaches the size of the visual indication of the virtual runway as the aircraft approaches the runway.

23. The method of claim 22, further including replacing, using the processing system, the visual indication of the virtual runway with the visual indication of the identified runway at a geographic location in proximity to the identified runway.

24. The method of claim 15, further including:

accessing, using the processing system, a database of terrain data including terrain coordinate information; and

presenting, using the processing system, a visual indication of the terrain data corresponding to the current geographic location of the aircraft.