Dynamically modifiable parameters in required time of arrival (RTA) regions of an assigned flight path

Patent metadata

Field	Value
Publication number	US-11587447-B2
Application number	US-202017098561-A
Country	US
Kind code	B2
Filing date	Nov 16, 2020
Priority date	Jan 23, 2020
Publication date	Feb 21, 2023
Grant date	Feb 21, 2023

Abstract

Systems and methods provide dynamically modifiable parameters in required time of arrival (RTA) speed regions of an assigned flight path of an aircraft. The system includes a vertical situation display (VSD) rendering thereon a vertical flight profile of the assigned flight path. A control module is coupled to the display system and configured to: demark the vertical flight profile with a plurality of RTA speed regions related to an initial speed profile; render an RTA speed band graphic having demarked sections vertically representing a speed minimum and speed maximum for an respective RTA speed region, the RTA speed band graphic representing a normalized speed range between zero and a maximum value for each respective RTA speed region. The control module accepts user modifications and updates the RTA speed band graphic and the current speed profile to reflect user input.

First claim

What is claimed is:

1. A processor-implemented method providing dynamically modifiable parameters in required time of arrival (RTA) speed regions of an assigned flight path, comprising:
rendering a vertical flight profile of the assigned flight path on a vertical situation display (VSD);

demarking the vertical flight profile with a plurality of RTA speed regions associated with a speed profile based on a received RTA;
rendering, on the VSD, an RTA speed band graphic that extends horizontally from a start of climb speed to a start of approach speed, the RTA speed band graphic having demarked sections that vertically represent a speed minimum and speed maximum associated with a current speed profile, the speed minimum and speed maximum referred to as a speed range, and a vertical spread for the RTA speed band graphic representing a normalized speed range between zero and a maximum value for each respective RTA speed region;
prompting a user for user input to edit an RTA speed region of the plurality of RTA speed regions, the user input being for each of (i) edit a priority order for the RTA speed region, (ii) edit a beginning and an ending of an RTA speed region, and (iii) select an RTA speed region for a speed range modification; and
in response to receiving the user input, modifying the RTA speed band graphic and the current speed profile to reflect the user input, whereby the aircraft is controlled using the modified current speed profile.

2. The method of claim 1 ,
wherein the user input includes decreasing a magnitude of a speed range for a selected RTA speed region; and
wherein modifying the RTA speed band graphic includes rendering a decreased magnitude speed range for the selected RTA speed region.

3. The method of claim 1 ,
wherein the user input includes increasing a magnitude of a speed range for a selected RTA speed region; and
wherein modifying the RTA speed band graphic includes rendering an increased magnitude speed range for the selected RTA speed region.

4. The method of claim 1 , further comprising rendering the RTA speed band graphic as a thickened portion along the X axis of the VSD.

5. The method of claim 1 , further comprising rendering the RTA speed band graphic as a thickened portion of the vertical flight profile.

6. The method of claim 1 , further comprising rendering the RTA speed band graphic as aligned above, but separate from, the vertical flight profile.

7. The method of claim 1 , wherein the user input includes disabling RTA speed control for the RTA speed region.

8. A system providing dynamically modifiable parameters in required time of arrival (RTA) speed regions of an assigned flight path, comprising:
a vertical situation display (VSD) rendering thereon rendering a vertical flight profile of the assigned flight path; and
a processor programmed to:
demark the vertical flight profile with a plurality of RTA speed regions associated with a speed profile based on a received RTA;
render, on the VSD, an RTA speed band graphic that extends horizontally from a start of climb speeds to a start of approach speeds, the RTA speed band graphic having demarked sections that vertically represent a speed minimum and speed maximum associated with a current speed profile, the speed minimum and speed maximum referred to as a speed range, and a vertical spread for the RTA speed band graphic representing a normalized speed range between zero and a maximum value for each respective RTA speed region;
prompt a user for user input to edit an RTA speed region of the plurality of RTA speed regions, the user input being for each of (i) edit a priority order for the RTA speed region, and (ii) select an RTA speed region for a speed range modification;
receive user input for an RTA speed region; and
modify the RTA speed band graphic and the current speed profile to reflect the user input, whereby the aircraft is controlled using the modified current speed profile.

9. The system of claim 8 , wherein the user input includes a pilot defined start point and end point for the RTA speed region.

10. The system of claim 9 , wherein the user input includes disabling RTA speed control for the RTA speed region.

11. The system of claim 10 , wherein the processor is further programmed to render the RTA speed band graphic as aligned above, but separate from, the vertical flight profile.

12. The system of claim 10 , wherein the processor is further programmed to render the RTA speed band graphic as a thickened portion along the X axis of the VSD.

13. The system of claim 10 , wherein the processor is further programmed to render the RTA speed band graphic as a thickened portion of the vertical flight profile.

14. The system of claim 11 ,
wherein the user input includes decreasing a magnitude of a speed range for a selected RTA speed region; and
wherein the processor is further programmed to modify the RTA speed band graphic by rendering a decreased magnitude speed range for the selected RTA speed region.

15. The system of claim 14 ,
wherein the user input includes increasing a magnitude of a speed range for a selected RTA speed region; and
wherein the processor is further programmed to modify the RTA speed band graphic by rendering an increased magnitude speed range for the selected RTA speed region.

16. A flight guidance system providing dynamically modifiable parameters in required time of arrival (RTA) speed regions of an assigned flight path of an aircraft, comprising:
a display system with a vertical situation display (VSD) rendering thereon a vertical flight profile of the assigned flight path; and
a control module coupled to the display system and configured to:

demark the vertical flight profile with a plurality of RTA speed regions related to an initial speed profile that is a function of an RTA;
render, on the display system, an RTA speed band graphic having demarked sections vertically aligned with the plurality of RTA speed regions, each demarked section vertically representing a speed minimum and speed maximum for an respective RTA speed region, the speed minimum and speed maximum referred to as a speed range, and a vertical spread for the RTA speed band graphic representing a normalized speed range between zero and a maximum value for each respective RTA speed region;
receive user input for an RTA speed region for at least editing a priority order for the RTA speed region; and
modify the RTA speed band graphic and the current speed profile to reflect the user input, whereby the aircraft is controlled using the modified current speed profile.

17. The flight guidance system of claim 16 , wherein the controller is configured to accept user input to edit a beginning and an ending of an RTA speed region.

18. The flight guidance system of claim 17 , wherein the controller is configured to accept user input to select an RTA speed region for a speed range modification.

19. The flight guidance system of claim 18 , wherein the controller is further configured to accept user input for disabling RTA speed control for the RTA speed region.

Assignees

• Honeywell Int Inc

Inventors

• Ramachandra Sripathi
• Jackson Michael
• Howe-Veenstra Ryan

Classifications

• G08G5/76

  for monitoring atmospheric conditions · CPC title

• G08G5/55

  for a single aircraft · CPC title

• G08G5/50

  Navigation or guidance aids · CPC title

• G08G5/21 Primary

  located onboard the aircraft · CPC title

• G08G5/54

  for approach or landing · CPC title