Cockpit display systems and methods for generating navigation displays including landing diversion symbology

Patent metadata

Field	Value
Publication number	US-9646503-B2
Application number	US-201514619849-A
Country	US
Kind code	B2
Filing date	Feb 11, 2015
Priority date	Feb 11, 2015
Publication date	May 9, 2017
Grant date	May 9, 2017

Abstract

Cockpit display systems and methods for generating navigation displays including landing diversion symbology are provided. In one embodiment, the cockpit display system includes a cockpit monitor and a controller coupled to the cockpit monitor. The controller is configured to assess the current feasibility of landing at one or more diversion airports in a range of an aircraft on which the cockpit display system is deployed. The controller is further configured to assign each diversion airport to one of a plurality of predetermined landing feasibility categories, and generate a horizontal navigation display on the cockpit monitor including symbology representative of the feasibility category assigned to one or more of the diversion airports.

First claim

What is claimed is:

1. A cockpit display system for deployment onboard an aircraft, the cockpit display system comprising:
a cockpit monitor; and
a controller coupled to the cockpit display system and configured to:
assess the current feasibility of landing at a first landing option in range of the aircraft;
assign the first landing option to one of a plurality of predetermined landing feasibility categories; and
generate a vertical navigation display on the cockpit monitor including symbology representative of the feasibility category assigned to the first landing option;

wherein the controller generates the vertical navigation display to further include: (i) an ideal trajectory profile for the first landing option, (ii) a predicted trajectory profile intersecting the ideal trajectory profile, and (iii) one or more visual cues marking at least one point at which a drag device of the aircraft should be deployed to follow the predicted trajectory profile to an intersection point with the ideal trajectory profile.

2. The cockpit display system of claim 1 wherein the controller is further configured to generate the predicted trajectory profile as a coded color graphic having a color indicative of the feasibility category assigned to the first landing option.

3. The cockpit display system of claim 1 wherein the symbology comprises a color coded icons, the color of the color coded icons distinguishing between the plurality of predetermined landing feasibility categories.

4. The cockpit display system of claim 3 wherein the plurality of predetermined landing feasibility categories comprise a high feasibility landing category, a moderate feasibility landing category, and a low feasibility landing category represented by a green color coded icon, an amber color coded icon, and a red color coded icon, respectively.

5. The cockpit display system of claim 1 wherein the first landing option is a designated airport at which the aircraft is scheduled to land.

6. The cockpit display system of claim 5 wherein the plurality of landing feasibility categories include a low feasibility landing category, and wherein the method further comprises:
if the designated airport is assigned to the low feasibility landing category, generating additional symbology on the navigation display indicating the location of one or more diversion airports.

7. A method carried-out by a cockpit display system of an aircraft, the cockpit display system including a controller and a cockpit monitor operably coupled to the controller, the method comprising:
at the controller, assessing the current feasibility of landing at a first landing option in a range of the aircraft;
at the controller, assigning the first landing option to one of a plurality of predetermined landing feasibility categories; and
generating a vertical navigation display on the cockpit monitor including symbology representative of the predetermined landing feasibility category assigned to the first landing option and further including graphics representing: (i) an ideal trajectory profile for the first landing option, and (ii) a predicted trajectory profile of the aircraft intersecting the ideal trajectory profile.

8. The method of claim 7 wherein generating comprises further producing, on the vertical navigation display, visual cues marking at least one point at which a drag device of the aircraft should be deployed to follow the predicted trajectory profile to an intersection point with the ideal trajectory profile.

9. The method of claim 7 further comprising:
at the controller, assessing the current feasibility of landing at a second landing option in the range of the aircraft;
at the controller, assigning the second landing option to one of the plurality of predetermined landing feasibility categories; and
generating a horizontal navigation display including symbology representative of the predetermined feasibility category assigned to both the first landing option and the second landing option.

10. The method of claim 7 further comprising:
producing a horizontal navigation display including symbology representative of the predetermined feasibility category assigned to the first landing option; and
generating the vertical navigation display on the cockpit monitor in response to receipt of input data selecting the first landing option from the horizontal navigation display.

11. The method of claim 7 wherein the symbology comprises an icon, which is color coded in accordance with the predetermined landing feasibility category assigned to the first landing option.

12. The method of claim 7 wherein the cockpit display system further comprises a datalink subsystem coupled to the controller, and wherein the method further comprises sending data to an Air Traffic Controller via the datalink subsystem identifying the predetermined landing feasibility category assigned to the first landing option by the controller.

13. The method of claim 7 wherein assessing comprises evaluating, at the controller, an estimated operational workload required to carry-out a successful landing at the first landing option.

14. The method of claim 7 wherein generating comprises producing, on the cockpit monitor, the predicted trajectory profile to comprise a coded color graphic having a color indicative of the predetermined feasibility category assigned to the first landing option.

15. The method of claim 7 further comprising selecting the first landing option to correspond with a designated airport at which the aircraft is scheduled to land.

16. The method of claim 7 further comprising generating the graphics representative of the predicted trajectory profile in a warning color when the controller assesses the first landing option as unfeasible.

Assignees

• Honeywell Int Inc

Inventors

• Kawalkar Amit Nishikant
• Chaubey Rajesh
• Mohan Rajeev

Classifications

• G08G5/00

  Traffic control systems for aircraft · CPC title

• G01C23/00 Primary

  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 title

• G01C23/005

  Flight directors (indicating arrangements specially adapted for rotary gyroscopes G01C19/32) · CPC title

• G08G5/0056 Primary

  Physics · mapped topic

• G08G5/0021

  Physics · mapped topic