INTERACTIVE DIALOG DEVICES AND METHODS FOR AN OPERATOR OF AN AIRCRAFT AND A GUIDANCE SYSTEM OF THE AIRCRAFT

• US 20130215023A1
• Filed: 03/15/2013
• Published: 08/22/2013
• Est. Priority Date: 11/29/2011
• Status: Abandoned Application

• Current Assignee: Airbus Operations (European Aeronautic Defence and Space Company EADS NV)
• Original Assignee: Airbus Operations (European Aeronautic Defence and Space Company EADS NV)
• Inventors: Bourret, Thierry, Louise, Pascale, Ollagnon, Claire, Chauveau, Nicolas, Giuliano, Sebastien, Drieux, Sebastien
• Application Number:
  US13/834,401
• Publication Number:
  US 20130215023A1
• Time in Patent Office: Days
• US Class Current: 345/157
• 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: G06F 3/01 Input arrangements or combined input and output arrangements for interaction between user and computer G06F3/16 takes precedence
• CPC Class Codes: G06F 3/013 Eye tracking input arrangements G06F3/015 takes precedence
• CPC Class Codes: G06F 3/0416 Control or interface arrangements specially adapted for digitisers
• CPC Class Codes: G06F 3/0484 for the control of specific functions or operations, e.g. selecting or manipulating an object, an image or a displayed text element, setting a parameter value or selecting a range
• CPC Class Codes: G08G 5/0021 located in the aircraft
• CPC Class Codes: G08G 5/0039 Modification of a flight plan
• CPC Class Codes: G09G 2380/12 Avionics applications

Abstract

Interactive dialog devices and methods can be installed on an aircraft for communication between an operator of the aircraft and a guidance system of the aircraft. A dialog device can include a global screen configured for displaying guidance information related to each of a navigation display, a vertical display, and a primary flight display. The global screen can include at least one graphic object which is produced in the form of an interaction element which represents a control feature that can be grasped and moved by an operator to modify a value of at least one guidance target of the guidance system associated with one or more of the navigation display, the vertical display, or the primary flight display.

Claims

1. A dialog device for an aircraft and guidance system of the aircraft, the dialog device comprising:

a global screen configured for displaying guidance information related to a navigation display, a vertical display, and/or a primary flight display;

wherein the global screen comprises at least one graphic object adapted to display an interaction element that represents a control feature associated with one or more of the navigation display, the vertical display, or the primary flight display; and

wherein the dialog device is adapted for an operator to move the interaction element to modify the control feature.

2. The dialog device of claim 1, wherein the control feature comprises of at least one guidance target of the guidance system associated with one or more of the navigation display, the vertical display, or the primary flight display.

3. The dialog device of claim 1, wherein the global screen is configured such that movement of an interaction element with respect to one of the navigation display, the vertical display, or the primary flight display causes corresponding movement of an interaction element with respect to another of the navigation display, the vertical display, or the primary flight display.

4. The dialog device of claim 1, wherein the global screen is configured such that each of the navigation display, the vertical display, and the primary flight display is selectively sizeable relative to others of the navigation display, the vertical display, and the primary flight display.

5. The dialog device of claim 1, wherein the interaction element is movable to any of a plurality of states which allow different actions to be implemented.

6. The dialog device of claim 5, wherein the interaction element is movable to one or more states which allow implementation of different actions comprising:

modifying a guidance target, which is applied by the guidance system;

modifying a preset guidance, target, which will be applied by the guidance system after validation;

engaging a capture or maintain mode for a selected guidance target;

or engaging a capture or maintain mode for a computed guidance target.

7. The dialog device of claim 5, wherein a transition from one state to another of the interaction element is generated by a corresponding movement thereof.

8. The dialog device of claim 1, wherein the dialog device is adapted for the global screen to generate a dynamic visual feedback on a predicted trajectory associated with the guidance target.

9. The dialog device of claim 8, wherein the global screen automatically displays at least one characteristic point of the predicted trajectory.

10. The dialog device of claim 9, wherein an interaction element is configured for adjusting a position of the characteristic point of the predicted trajectory.

11. The dialog device of claim 1, wherein the global screen comprises a touch screen;

and

wherein the dialog device is adapted for the interaction element to be controlled by direct contact with the touch screen.

12. The dialog device of claim 1, comprising a control device linked to the global screen and configured to control the movement of a cursor on the global screen and to act on the interaction element.

13. The dialog device of claim 12, wherein the control device comprises:

an eye tracker configured to detect a zone of focus of an operator of the aircraft and to select an interaction element contained within a zone of focus; and

a secondary control device linked to the global screen and configured to selectively cause movement of the interaction element so as to modify the control feature.

14. A method for controlling a guidance system of an aircraft, the method comprising:

displaying guidance information related to each of a navigation display, a vertical display, and a primary flight display on a global screen;

selecting at least one interaction element on one of the navigation display, the vertical display, or the primary flight display, wherein the interaction element represents a control feature for a guidance system associated with one or more of the navigation display, the vertical display, or the primary flight display; and

moving the interaction element on one of the navigation display, the vertical display, or the primary flight display to modify the control feature.

15. The method of claim 14, wherein displaying guidance information comprises selectively sizing one of the navigation display, the vertical display, or the primary flight display on the global screen relative to others of the navigation display, the vertical display, and the primary flight display.

16. The method of claim 14, wherein the global screen comprises a touch screen;

and

wherein selecting an interaction element comprises directly contacting the touch screen.

17. The method of claim 14, wherein selecting an interaction element comprises moving a control device linked to the global screen, the control device being configured to control the movement of a cursor on the global screen and to act on the interaction element.

18. The method of claim 17, wherein the control device comprises an eye tracker;

wherein selecting an interaction element comprises detecting a zone of focus of an operator of the aircraft and selecting an interaction element contained within the zone of focus; and

wherein moving the interaction element comprises selectively operating a secondary control device linked to the global screen.

19. The method of claim 14, wherein moving the interaction element of one of the navigation display, the vertical display, or the primary flight display causes corresponding movement of an interaction element with respect to another of the navigation display, the vertical display, or the primary flight display.

20. The method of claim 14, wherein the control feature comprises of at least one guidance target of the guidance system associated with one or more of the navigation display, the vertical display, or the primary flight display.

21. The method of claim 14, wherein moving the interaction element comprises moving the interaction element along a curve of one of the navigation display, the vertical display, or the primary flight display.

22. The method of claim 14, wherein moving the interaction element comprises moving the interaction element to any of a plurality of states which allow different actions to be implemented.

23. The method of claim 22, wherein moving the interaction element comprises moving the interaction element to one or more states which allow implementation of different actions including:

modifying a guidance target, which is applied by the guidance system;

modifying a preset guidance target, which will be applied by the guidance system after validation;

engaging a capture or maintain mode for a selected guidance target;

or engaging a capture or maintain mode for a computed guidance target.