Method and system of controlling a flight of an aircraft subjected to a required time of arrival constraint

Patent metadata

Field	Value
Publication number	US-10049585-B2
Application number	US-201615192238-A
Country	US
Kind code	B2
Filing date	Jun 24, 2016
Priority date	Jun 26, 2015
Publication date	Aug 14, 2018
Grant date	Aug 14, 2018

Abstract

Example systems and methods for controlling a flight of an aircraft subjected to a required time of arrival constraint at a target waypoint and to an additional flight criterion are disclosed herein. An example method includes calculating combinations of cruise speed and descent speed for estimated times of arrival (ETAs) at the target waypoint and determining a subset of the combinations that introduce substantially a same amount of time change in the ETA when changing the corresponding cruise speed to a cruise speed limit as when changing the corresponding descent speed to a descent speed limit. The example method also includes selecting a combination of the subset of the combinations having an ETA substantially equal to the RTA and modifying at least one of a cruise speed or a descent speed of the aircraft based on the selected combination.

First claim

What is claimed is:

1. A method of controlling a flight of an aircraft subjected to a required time of arrival (RTA) constraint at a target waypoint, the method comprising:
calculating, using an estimated time of arrival (ETA) determiner, during flight, combinations of cruise speed and descent speed for estimated times of arrival (ETAs) at the target waypoint;
determining, using a criterion determiner, a subset of the combinations that introduce substantially a same amount of time change in the ETA when changing the corresponding cruise speed to a cruise speed limit, while maintaining the descent speed constant, as when changing the corresponding descent speed to a descent speed limit while maintaining the cruise speed constant;
selecting, using a selector, a combination of the subset of the combinations having an ETA substantially equal to the RTA; and
modifying at least one of a cruise speed or a descent speed of the aircraft based on the selected combination.

2. The method of claim 1 , wherein the cruise speed limit includes a minimum cruise speed and the descent speed limit includes a minimum descent speed, and wherein determining the subset of the combinations includes determining a first set of combinations that introduce a same amount of time delay when the corresponding cruise speed is reduced to the minimum cruise speed as when the corresponding descent speed is reduced to the minimum descent speed.

3. The method of claim 2 , wherein the cruise speed limit includes a maximum cruise speed and the descent speed limit includes a maximum descent speed, and wherein determining the subset of the combinations includes determining a second set of combinations that introduce a same amount of time anticipation when the corresponding cruise speed is increased to the maximum cruise speed as when the corresponding descent speed is increased to the maximum descent speed.

4. The method of claim 3 , wherein the subset of the combinations further includes a third set of combinations having a cruise speed equal to an average of the minimum cruise speed and the maximum cruise speed.

5. The method of claim 1 , wherein the cruise speed limit and the descent speed limit are based on at least one of a cruise altitude of the aircraft or a weight of the aircraft.

6. The method of claim 1 , wherein the cruise speed limit and the descent speed limit are based on an aircraft spacing requirement.

7. The method of claim 1 , wherein the combinations are based on at least one of a weight of the aircraft, a cruise altitude of the aircraft, a flight plan, an initial position or a weather condition.

8. A system to control a flight of an aircraft subjected to a required time of arrival (RTA) constraint at a target waypoint, the system comprising:
an estimated time of arrival (ETA) determiner to calculate, during flight, combinations of cruise speed and descent speed for estimated times of arrival (ETAs) at the target waypoint;
a criterion determiner to determine a subset of the combinations that introduce substantially a same amount of time change in the ETA when changing the corresponding cruise speed to a cruise speed limit, while maintaining the descent speed constant, as when changing the corresponding descent speed to a descent speed limit, while maintaining the cruise speed constant;
a selector to select a combination of the subset of the combinations having an ETA substantially equal to the RTA; and
a speed profile generator to generate a signal that modifies at least one of a cruise speed or a descent speed of the aircraft based on the selected combination.

9. The system of claim 8 , wherein the cruise speed limit includes a minimum cruise speed and the descent speed limit includes a minimum descent speed, and the subset of the combinations includes a first set of combinations that introduce a same amount of time delay when the corresponding cruise speed is reduced to the minimum cruise speed as when the corresponding descent speed is reduced to the minimum descent speed.

10. The system of claim 9 , wherein the cruise speed limit includes a maximum cruise speed and the descent speed limit includes a maximum descent speed, and the subset of the combinations includes a second set of combinations that introduce a same amount of time anticipation when the corresponding cruise speed is increased to the maximum cruise speed as when the corresponding descent speed is increased to the maximum descent speed.

11. The system of claim 10 , wherein the subset of the combinations further includes a third set of combinations having a cruise speed equal to an average of the minimum cruise speed and the maximum cruise speed.

12. The system of claim 8 , wherein the cruise speed limit and the descent speed limit are based on at least one of a cruise altitude of the aircraft or a weight of the aircraft.

13. The system of claim 8 , wherein the cruise speed limit and the descent speed limit are based on an aircraft spacing requirement.

14. A tangible computer readable storage medium comprising instructions that, when executed, cause a machine to at least:
calculate, during flight, combinations of cruise speed and descent speed for estimated times of arrival (ETAs) of an aircraft at a target waypoint;
determine a subset of the combinations that introduce substantially a same amount of time change in the ETA when changing the corresponding cruise speed to a cruise speed limit, while maintaining the descent speed constant, as when changing the corresponding descent speed to a descent speed limit, while maintaining the cruise speed constant;
select a combination of the subset of the combinations having an ETA substantially equal to a required time of arrival (RTA) constraint; and
modify at least one of a cruise speed or a descent speed of the aircraft based on the selected combination.

15. The tangible computer readable storage medium of claim 14 , wherein the cruise speed limit includes a minimum cruise speed and the descent speed limit includes a minimum descent speed, and the subset of the combinations includes a first set of combinations that introduce a same amount of time delay when the corresponding cruise speed is reduced to the minimum cruise speed as when the corresponding descent speed is reduced to the minimum descent speed.

16. The tangible computer readable storage medium of claim 15 , wherein the cruise speed limit includes a maximum cruise speed and the descent speed limit includes a maximum descent speed, and the subset of the combinations includes a second set of combinations that introduce a same amount of time anticipation when the corresponding cruise speed is increased to the maximum cruise speed as when the corresponding descent speed is increased to the maximum descent speed.

17. The tangible computer readable storage medium of claim 16 , wherein the subset of the combinations further includes a third set of combinations having a cruise speed equal to an average of the minimum cruise speed and the maximum cruise speed.

18. The tangible computer readable storage medium of claim 14 , wherein the cruise speed limit and the descent speed limit are based on at least one of a cruise altitude of the aircraft or a weight of the aircraft.

19. The tangible computer readable storage medium of claim 14 , wherein the cruise speed limit and the descent speed limit are based on an aircraft spacing requirement.

20. The tangible computer readable storage medium of claim 14 , wherein the combinations are based on at least one of a weight of the aircraft, a

Assignees

• Boeing Co

Inventors

• Garrido López David

Classifications

• G08G5/0039 Primary

  Physics · mapped topic

• G05D1/101 Primary

  specially adapted for aircraft · CPC title

• G05D1/0676

  specially adapted for landing · CPC title

• G08G5/34

  for flight plan modification · CPC title