SYSTEM AND METHOD FOR GROUND PROXIMITY WARNING WITH ENHANCED OBSTACLE DEPICTION

• US 20060238402A1
• Filed: 04/21/2005
• Published: 10/26/2006
• Est. Priority Date: 04/21/2005
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Khatwa, Ratan
• Granted Patent: US 7,330,147 B2
• Time in Patent Office: Days
• US Class Current: 342/29
• CPC Class Codes: G01C 23/005 Flight directors indicating arrangements specially adapted for rotary gyroscopes G01C19/32

Abstract

Systems and methods for displaying ground obstructions on a visual display are disclosed. In an embodiment, a ground proximity warning system includes at least one aircraft sensor system operable to acquire aircraft data and a ground proximity warning computer coupled to the aircraft sensor system to process the aircraft data that generates ground proximity warning data corresponding to a sensed ground obstruction. An indicating system including a visual display device then presents an image of a visual symbol corresponding to the sensed ground obstruction. At least one of the computer and the visual display device is controllable to selectively display the visual symbol.

Claims

1. A system for an aircraft, comprising:

at least one aircraft sensor system operable to acquire aircraft data;

a ground proximity warning computer coupled to the at least one aircraft sensor system that is operable to process the aircraft data to generate ground proximity warning data corresponding to a distance between a sensed ground obstruction and the aircraft; and

an indicating system including at least one visual display device that is configured to display an image of a visual symbol corresponding to the sensed ground obstruction, wherein at least one of the computer and the visual display device is controllable to selectively display the visual symbol.

2. The system of claim 1, wherein at least one of the computer and the visual display device is further operable to display terrain elevations, and at least one of the computer and the visual display device is controllable to suppress the terrain elevations while displaying the visual symbol.

3. The system of claim 1, wherein the at least one visual display device is further operable to display terrain elevations, and at least one of the computer and the visual display device is controllable to suppress the visual symbol while displaying the terrain elevations.

4. The system of claim 3, wherein at least one of the computer and the visual display device is configured to automatically display a suppressed visual symbol when the corresponding sensed ground obstruction is within a predetermined range of the aircraft.

5. The system of claim 3, wherein at least one of the computer and the visual display device is configured to automatically display a suppressed visual symbol when the corresponding sensed ground obstruction is within a predetermined bearing relative to the aircraft.

6. The system of claim 1, wherein at least one of the computer and the visual display device is configured to selectably alter a range setting for the visual display device, further wherein at least one visual symbol is suppressed or an alternate visual symbol is displayed when a predetermined range value is selected.

7. The system of claim 6, wherein the predetermined range value is at least about ten nautical miles.

9. The system of claim 1, wherein the visual symbol includes a first portion and a second portion, and further wherein at least one of the computer and the visual display device is controllable to display the first portion while suppressing the second portion.

8. (canceled)

10. A method comprising:

displaying terrain elevations on a visual display device;

displaying at least one visual symbol corresponding to a sensed ground obstruction on the visual display device; and

controllably altering the visual display device to display a selected one of the terrain elevations and the at least one visual symbol.

11. The method of claim 10, wherein controllably altering the visual display device further comprises displaying the terrain elevations and suppressing the at least one visual symbol.

12. The method of claim 10, wherein controllably altering the visual display device further comprises displaying the at least one visual symbol and suppressing the terrain elevations.

13. The method of claim 10, wherein controllably altering the visual display device further comprises controlling a selected one of a ground proximity warning computer and an indicating system coupled to the computer to alter the visual display device.

14. A method of display management for an aircraft ground proximity warning system, comprising:

generating terrain elevations and visual symbols corresponding to sensed ground obstructions that are configured to be displayed on a visual display device;

displaying the terrain elevations on a display device;

detecting a selected ground obstruction that is within a predetermined zone that extends outwardly from the aircraft; and

displaying the generated symbol corresponding to the selected ground obstruction on the display device.

15. The method of claim 14, wherein generating terrain elevations and visual symbols further comprises generating the terrain elevations and visual symbols in at least one of a ground proximity warning computer and an indicating system coupled to the ground proximity warning computer.

16. The method of claim 14, wherein the display device includes a terrain awareness display (TAD).

17. The method of claim 14, wherein detecting a selected ground obstruction further comprises detecting the selected ground obstruction is within a predetermined range and bearing relative to the aircraft.

18. The method of claim 14, wherein detecting a selected ground obstruction further comprises detecting the ground obstruction is less than a predetermined distance from the aircraft.

19. The method of claim 18, wherein detecting the ground obstruction is less than the predetermined distance from the aircraft further comprises determining one of a vertical distance between a portion of the detected ground obstruction and the aircraft, and determining a slant range between the obstacle and the aircraft.

20. A method of display management for an aircraft ground proximity warning system, comprising:

displaying terrain elevations on a visual display device;

displaying a plurality of visual symbols corresponding to sensed ground obstructions on the visual display device;

selecting a range setting for the visual display device; and

if the range setting is less than a predetermined value, altering display of the number of previously displayed visual symbols, and if the range setting is greater than or equal to the predetermined value.

21. The method of claim 20, wherein selecting a range setting further comprises altering a range setting in at least one of a ground proximity warning computer and an indicating system coupled to the ground proximity warning computer.

22. The method of claim 20, wherein the visual display device includes a terrain awareness display (TAD).

23. A method of display management for an aircraft ground proximity warning system, comprising:

displaying at least one visual symbol corresponding to a sensed ground obstruction on a visual display device, the visual symbol having a first portion and a second portion; and

selecting a display mode for the visual display device, wherein a first display mode is operable to display the first portion and the second portion of the visual symbol, and a second display mode is operable to display the first portion of the visual symbol while suppressing the second portion.

24. The method of claim 24, further comprising selecting a display range, and if the selected display range is less that a predetermined range value, displaying the first and the second portion, and if the display range is greater than a predetermined range value, displaying the first portion only.

25. The method of claim 24, wherein displaying at least one visual symbol further comprises displaying an ICAO symbol.

26. The method of claim 24, wherein displaying an ICAO symbol further comprises displaying a chevron portion of the symbol when operating in the first display mode, and suppressing the chevron portion when operating in the second display mode.