Method and system displaying crosswind correction for approach to a runway

• US 8,392,039 B2
• Filed: 05/29/2008
• Issued: 03/05/2013
• Est. Priority Date: 05/29/2008
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: He, Gang, Wyatt, Ivan Sandy
• Primary Examiner(s): Tran, Khoi
• Assistant Examiner(s): HOLLOWAY, JASON R
• Application Number:
  US12/129,495
• Publication Number:
  US 20090326744A1
• Time in Patent Office: 1,741 Days
• Field of Search: 701/3, 701/4, 701/10, 701/14, 701 16- 18, 340/967, 340/968, 340971-976, 340/979, 340/980, 340/966, 244/75.1, 244/76.R, 244/174, 244/175, 244/181, 244/182, 244/194, 244/195, 345/428, 345/581, 345/589, 345/600, 345/698, 345/12, 345/20, 345/63
• US Class Current: 701/14
• 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

Abstract

An aircraft display system (100) for illustrating a suggested crab angle has a processor (104) adapted to receive data representative of a desired ground tract (214) and representative of a ground tract deviation, and is configured upon receipt of these data to supply a ground tract rendering display command. A display device (116) coupled to receive the ground tract image rendering display commands is operable to render an icon (222) representative of the desired aircraft heading to maintain the desired ground tract (214). The method of how to maneuver an aircraft to correct for crosswind includes determining (306) a difference between a current ground track (224) and a current heading (218), determining a desired heading to maintain the desired ground track (214) based on the difference, and rendering on a display an aircraft icon (222) that is representative of the desired heading.

Claims

1. A method of illustrating how to maneuver an aircraft to correct for crosswind, comprising:

determining a difference between a current ground track and a current heading;

identifying a desired ground track;

calculating, in response to the determining and identifying steps, a desired heading required to maintain the desired ground track;

applying a gain factor to the desired heading resulting in a modified heading proportional to the difference between current track and desired heading; and

rendering on a display the current ground track, current heading, and an aircraft icon that is representative of the modified heading, the aircraft icon having a format different from the current ground track.

2. The method of claim 1 wherein the rendering step comprises rendering the aircraft icon comprising one of a plurality of formats as determined by the magnitude of the difference between the current track and the desired heading.

3. The method of claim 2 wherein the rendering step comprises rendering the aircraft icon comprising a format selected from one of the formats consisting of at least two colors and at least two sizes.

4. The method of claim 1 wherein the rendering step comprises a user selecting the conditions to enable the aircraft icon that is representative of the modified heading.

5. The method of claim 1 wherein rendering step comprises rendering the aircraft icon comprising displaying the modified heading as determined by aircraft dynamic characteristics.

6. The method of claim 1 wherein the rendering step comprises displaying the aircraft icon with respect to the desired ground track as determined by one of an ILS navigation aid, a ground based navigational system, a GPS navigation aid, a flight management system, and an inertial navigation system.

7. The method of claim 1 further comprising rendering a lateral deviation icon for indicating angular deviations form a desired course line.

8. The method of claim 1 further comprising rendering a lateral deviation icon indicating linear deviations from the desired ground track.

9. The method of claim 7 wherein the rendering a lateral deviation step comprises rendering a lateral deviation icon comprising one of a plurality of formats as determined by the magnitude of the desired heading.

10. The method of claim 9 wherein the rendering a lateral deviation step comprises rendering the aircraft icon comprising a format selected from one of the formats consisting of at least two colors, at least two sizes, and at least two positions.

11. The method of claim 1 further comprising rendering a lateral deviation icon indicating the direction in which a runway is positioned in relation to a heading indicated by the aircraft icon.

12. A method of displaying an icon representative of a desired aircraft crab angle to compensate for a crosswind, comprising:

determining a current ground track;

determining a current heading;

determining a difference between the current ground track and the current heading;

determining a desired ground track;

determining, in response to the desired ground track and difference between the current ground track and the current heading, a desired heading reflective of the desired aircraft crab angle required to maintain the desired ground track;

applying a gain factor to the desired heading resulting in a modified heading when the difference between the desired heading and the desired ground track is less than a threshold; and

rendering on a display an aircraft icon that is representative of the modified heading, the aircraft icon having a format different than a displayed desired ground track.

13. The method of claim 12 wherein the rendering step comprises rendering the aircraft icon comprising one of a plurality of formats as determined by the magnitude of the desired heading.

14. The method of claim 12 wherein the rendering step comprises rendering the aircraft icon comprising a format selected from one of the formats consisting of at least two colors and at least two sizes.

15. The method of claim 12 further comprising rendering a lateral deviation icon for indicating angular deviations form a desired course line.

16. The method of claim 14 wherein the rendering a lateral deviation icon step comprises rendering a lateral deviation icon comprising one of a plurality of formats as determined by the magnitude of the desired heading.

17. An aircraft display system comprising:

a processor adapted to receive data representative of a desired ground track, a current heading and data representative of a current ground track deviation, and configured upon receipt of these data to determine a desired heading required to maintain the desired ground track, and to apply a gain factor to the desired heading resulting in a modified heading when the difference between the desired heading and the desired ground track is less than a threshold, and supply a ground track rendering display command and a modified heading display command; and

a display device coupled to receive the ground track image rendering display command and the modified heading display command and operable to render an icon representative of the modified heading to maintain the desired ground track.