Enhanced instrument procedure visualization

• US 9,702,726 B2
• Filed: 11/16/2015
• Issued: 07/11/2017
• Est. Priority Date: 11/16/2015
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: McCullough, Sue, Turner, Nathan Shaughn, Gorsky, John-Paul, Acuna, Vincent, Crouch, Steven, Dairman, Charles
• Primary Examiner(s): Tarcza, Thomas
• Assistant Examiner(s): BERNS, MICHAEL ANDREW
• Application Number:
  US14/942,051
• Publication Number:
  US 20170138759A1
• Time in Patent Office: 603 Days
• CPC Class Codes: B64D 43/02 for indicating aircraft speed or stalling conditions
• CPC Class Codes: G01C 23/005 Flight directors indicating arrangements specially adapted for rotary gyroscopes G01C19/32
• CPC Class Codes: G08G 5/0021 located in the aircraft
• CPC Class Codes: G08G 5/0047 Navigation or guidance aids for a single aircraft details of equipment G08G5/0017
• CPC Class Codes: G08G 5/0052 for cruising combined instruments indicating more than one navigational value G01C23/00
• CPC Class Codes: G08G 5/025 Navigation or guidance aids radar or analogous systems specially adapted for landing purposes G01S13/913

Abstract

A system and method for providing the information contained in instrument procedure charts in a more intuitive and easier to comprehend manner is provided. The provided enhanced instrument procedure visualization system displays a dynamic three-dimensional view of a selected instrument procedure, and incorporates time-relevant information from weather and traffic sources. The provided enhanced instrument procedure visualization system further allows a pilot to scroll forward and backward in time to review and study the complete instrument procedure.

Claims

1. A method for displaying an instrument procedure on a three-dimensional display element, the method comprising;

at a controller,

receiving a user selected destination and a user selected instrument procedure;

receiving current position and current orientation information for a vehicle;

processing the user selected destination, user selected instrument procedure, current position and current orientation to determine a vehicle path;

processing the vehicle path and the selected instrument procedure, to generate a three-dimensional map comprising the vehicle path and a volume surrounding the vehicle path, wherein the volume (i) is selected from among the set including (a) a predetermined amount of elapsed time around the vehicle at a predetermined traveling speed, and (b) predetermined distances around the vehicle, and (ii) comprises one or more features associated with the selected instrument procedure; and

commanding the three-dimensional display element to dynamically render the three-dimensional map as a three-dimensional dynamic synthetic vision image.

2. The method of claim 1, wherein the vehicle is an aircraft, the vehicle path is a flight path, the selected destination is an airport, and the step of receiving current position and orientation for a vehicle comprises receiving respective aircraft direction, aircraft attitude, aircraft speed, and aircraft altitude.

3. The method of claim 2, wherein the three-dimensional display element comprises a synthetic vision display element.

4. The method of claim 2, further comprising:

overlaying, on the three-dimensional dynamic synthetic vision image, a banner with text boxes providing optional layers;

receiving a first user selected optional layer; and

rendering, on the three-dimensional map, a feature associated with the first user selected optional layer, responsive to the user selection.

5. The method of claim 4, further comprising:

receiving a second user selected optional layer;

rendering, on the three-dimensional map, a feature associated with the second user selected optional layer; and

removing, from the three-dimensional map, the feature associated with the first user selected optional layer in response to receiving a user de-selection of the first user selected optional layer.

6. The method of claim 4, wherein the optional layers are selected from among the set including waypoint list, frequencies, traffic, weather, notice to airmen (NOTAMs), attitude and heading reference system (AHRS), and procedure chart.

7. A display system for displaying an instrument procedure for a vehicle, the system comprising;

a three-dimensional display element;

a database comprising flight plan information, terrain information, frequency information, chart information, weather information, and airspace information; and

a controller coupled to the three-dimensional display element, a source of a selected destination, a source of a selected instrument procedure, a source of a current position and a current orientation, and the database, and configured to;

determine a vehicle path based on the selected destination, the selected instrument procedure, and the current position and the current orientation; and

generate a dynamic three-dimensional map comprising a volume surrounding the vehicle path, wherein the volume (i) comprises a feature associated with the selected instrument procedure, and (ii) moves forward or backward in time responsive to user input;

command the three-dimensional display element to dynamically render the three-dimensional map as a synthetic vision image.

8. The system of claim 7, wherein the vehicle is an aircraft, the vehicle path is a flight path, the selected destination is an airport, and the controller is further configured to receive aircraft direction, aircraft attitude, aircraft speed, and aircraft altitude.

9. The system of claim 8, wherein the three-dimensional display element comprises a synthetic vision display element.

10. The system of claim 8, wherein the controller is further configured to:

command the three-dimensional display element to display a banner with text boxes providing optional layers;

receive a first user selected optional layer; and

render on the three-dimensional map, a feature associated with the first user selected optional layer.

11. The system of claim 10, wherein the controller is further configured to:

receive a second user selected optional layer; and

render, on the three-dimensional map, a feature associated with the second user selected optional layer.

12. The system of claim 11, wherein the optional layers are selected from among the set including waypoint list, frequencies, traffic, weather, notice to airmen (NOTAMs), attitude and heading reference system (AHRS), and procedure chart.

13. A method for displaying aircraft information on a three-dimensional synthetic vision display element, the method comprising:

at a controller,

receiving an instrument procedure;

receiving a selected destination;

receiving a current position and a current orientation for an aircraft;

processing the user selected destination, the current position and the current orientation to determine a vehicle path; and

processing the vehicle path and the instrument procedure to generate (i) three-dimensional map comprising the vehicle path and a volume surrounding the vehicle path, and (ii) a plurality of text boxes indicating optional layers for display; and

dynamically rendering, on the three-dimensional synthetic vision display element, the three-dimensional map and the plurality of text boxes.

14. The method of claim 13, further comprising:

rendering a feature associated with the selected instrument procedure within the three-dimensional map.

15. The method of claim 14, wherein the vehicle is an aircraft, the vehicle path is a flight path, the selected destination is an airport, and the step of receiving current position and current orientation for a vehicle comprises receiving respective aircraft direction, aircraft attitude, aircraft speed, and aircraft altitude.

16. The method of claim 15, further comprising:

receiving a first user selected optional layer; and

rendering, on the three-dimensional map, a feature associated with the first user selected optional layer.

17. The method of claim 16, further comprising:

receiving a second user selected optional layer; and

rendering, on the three-dimensional map, a feature associated with the second user selected optional layer.

18. The method of claim 17, further comprising removing, from the three-dimensional map, the feature associated with the first user selected optional layer in response to receiving a user de-selection of the first user selected optional layer.

19. The method of claim 18, wherein the optional layers are selected from among the set including waypoint list, frequencies, traffic, weather, notice to airmen (NOTAMs), attitude and heading reference system (AHRS), and procedure chart.

20. The method of claim 13, further comprising, dynamically moving the three-dimensional map forward or backward in time responsive to user input.