SYSTEM AND METHOD FOR DISPLAYING VERTICAL REFERENCE ON A ROTORCRAFT SYSTEM

• US 20150259075A1
• Filed: 03/17/2014
• Published: 09/17/2015
• Est. Priority Date: 03/17/2014
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Case, Timothy John, Meeker, John
• Granted Patent: US 9,340,282 B2
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: B64C 27/00 Rotorcraft; Rotors peculiar thereto
• CPC Class Codes: G01C 23/00 Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration
• CPC Class Codes: G01C 5/005 altimeters for aircraft G01C5/02, G01C5/06 take precedence

Abstract

A method and system for maintaining visual vertical reference on a rotorcraft display during rotorcraft landing is provided. The method generates vertical poles and positions them on the rotorcraft display such that vertical reference as well as roll information may be quickly and easily comprehended by a pilot.

Claims

1. A method for providing visual vertical guidance during rotorcraft landing, the method comprising:

displaying a landing point;

displaying a first pole having a first, static, predetermined height at a first predetermined location with respect to the landing point;

displaying a second pole having a second, static, predetermined height at a second predetermined location with respect to the landing point;

obtaining terrain and elevation data;

obtaining rotorcraft position data;

dividing the first pole into equal first pole sections of a predetermined size;

dividing the second pole into equal second pole sections of the predetermined size;

rendering the first pole and the second pole in visually distinguishable pole sections indicative of rotorcraft position above the terrain; and

altering the visually distinguishable pole sections to indicate rotorcraft roll.

6. The method of claim 1, wherein the step of displaying a first pole further comprises positioning the first pole at a location substantially consistent with 300 degrees on a circle representative of a landing zone, and wherein the step of displaying a second pole further comprises positioning the second pole at a location substantially consistent with 60 degrees on the circle representative of the landing zone.

8. The method of claim 1, wherein the step of displaying a landing point further comprises displaying a substantially circular line of a predetermined diameter surrounding the landing point.

9. The method of claim 1, further comprising:

selectively changing the first predetermined location and the second predetermined location according to the rotorcraft position.

2. (canceled)

3. (canceled)

4. (canceled)

5. (canceled)

7. (canceled)

10. A system for providing visual vertical guidance during rotorcraft landing, the system comprising:

a first source of terrain and elevation data;

a second source of rotorcraft position data;

a user input device providing a landing point;

a display system; and

a processor coupled to the first source, the second source, the user input device, and the display system, the processor configured to;

obtain the landing point;

create at least two vertical reference poles of a predetermined height;

generate symbology on the display graphically representative of a composite image of (i) the terrain and elevation proximate to the landing point, and (ii) the at least two vertical reference poles;

positioned at separate predetermined locations, and rendered in visually distinguishable sections representative of rotorcraft position above the terrain; and

alter the visually distinguishable sections of the at least two vertical reference poles to indicate direction and magnitude of rotorcraft roll.

11. The system of claim 10, wherein the processor is further configured to selectively position the at least two vertical reference poles with respect to the landing point.

14. The system of claim 10, wherein the processor is further configured to selectively change the first predetermined location and the second predetermined location according to the rotorcraft position.

12. (canceled)

13. (canceled)

15. A method for providing visual vertical guidance during rotorcraft landing, the method comprising:

obtaining terrain data;

obtaining a landing point;

obtaining rotorcraft position data;

displaying a substantially circular line of a predetermined diameter surrounding the landing point;

displaying a first pole at a first predetermined location on the circular line; and

displaying a second pole at a second predetermined location on the circular line;

rendering the first pole and the second pole in visually distinguishable pole sections indicative of rotorcraft position above the terrain.

16. The method of claim 15, wherein displaying a first pole further comprises displaying a first pole of a first predetermined height;

and wherein displaying a second pole further comprises displaying a second pole of a second predetermined height.

18. The method of claim 15, further comprising rendering the first pole and the second pole in visually distinguishable pole sections indicative of rotorcraft roll.

19. The method of claim 15, further comprising:

selectively changing the first predetermined location and the second predetermined location according to the rotorcraft position.

20. The method of claim 18, further comprising rendering the pole sections visually distinguishable by color.

17. (canceled)