Aircraft control system for reaching a waypoint at a required time of arrival

• US 6,507,782 B1
• Filed: 05/14/2001
• Issued: 01/14/2003
• Est. Priority Date: 05/14/2001
• Status: Expired due to Term

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Jackson, Michael R., Rumbo, Jim R., OʼLaughlin, Brian E.
• Primary Examiner(s): Cuchlinski, Jr., William A.
• Assistant Examiner(s): Marc-Coleman, Marthe Y.
• Application Number:
  US09/855,861
• Time in Patent Office: 610 Days
• Field of Search: 701/123, 701/121, 701/204, 244/182
• US Class Current: 701/121
• CPC Class Codes: G05D 1/0005 with arrangements to save energy
• CPC Class Codes: G05D 1/0202 specially adapted to aircraft

Abstract

The instant invention provides a system and method for controlling the flight of an aircraft to meet an RTA. The system comprises a speed profile generator that communicates with a trajectory generator to produce a speed profile signal that enables the aircraft to reach a waypoint substantially at a predetermined time. In the system of the instant invention, the speed profile generator receives a nominal speed command signal, a time error signal and a sensitivity signal. Based on these inputs, the speed profile generator produces a speed profile signal. The trajectory generator receives the speed profile signal and a required time of arrival signal. Based on these signals, the trajectory generator produces a time error signal and a sensitivity signal. This sensitivity signal represents the sensitivity of the time error signal to changes in the speed profile signal.

Claims

1. A system for controlling the flight of an aircraft to enable the aircraft to reach a waypoint substantially at a predetermined time, the system comprising a speed profile generator in communication with a trajectory generator;

said speed profile generator configured to receive a nominal speed command signal, a time error signal and a sensitivity signal and to produce a speed profile signal in response to said nominal speed command signal, said time error signal and said sensitivity signal;

said trajectory generator configured to receive said speed profile signal and a required time of arrival signal to produce a time error signal and a sensitivity signal in response to said speed profile signal and said required time of arrival signal, said sensitivity signal representing the sensitivity of said time error signal to changes in said speed profile signal.

2. The system of claim 1 wherein said trajectory generator is configured to receive an atmospheric condition signal and produce said time error signal in response to said atmospheric condition signal.

3. The system of claim 1 wherein said trajectory generator is configured to receive an atmospheric condition signal and produce said sensitivity signal in response to said atmospheric condition signal.

4. The system of claim 1 further comprising a descent path planner in communication with said trajectory generator.

5. The system of claim 4 wherein said descent path planner modifies said speed profile signal to enable the aircraft to descend with an engine throttle setting greater than idle.

6. The system of claim 5 wherein said speed profile signal enables the aircraft to decelerate with an engine throttle setting greater than idle.

7. The system of claim 1 wherein said trajectory generator includes a descent path planner.

8. The system of claim 1 wherein said speed profile signal includes a climb phase segment.

9. The system of claim 8 wherein said speed profile signal is configured to enable the aircraft to reach a waypoint substantially at a predetermined time during the climb phase.

10. The system of claim 9 wherein the speed profile signal is modified while the aircraft'"'"'s position is increasing in altitude.

11. The system of claim 1 wherein said speed profile signal includes a descent phase segment.

12. The system of claim 11 wherein said speed profile signal is configured to enable the aircraft to reach a waypoint substantially at a predetermined time while the aircraft'"'"'s position is decreasing in altitude.

13. The system of claim 12 wherein the speed profile signal is modified while the aircraft'"'"'s position is decreasing in altitude.

14. The system of claim 1 wherein said trajectory generator detects a variation in said sensitivity signal and produces a variability signal in response to said variation.

15. The system of claim 14 wherein said speed profile generator is configured to receive said variability signal and produce said speed profile signal in response to said variability signal.

16. The system of claim 1 wherein said speed profile generator comprises a speed adjustment generator in communication with a speed adjuster, said speed adjustment generator configured to receive said time error signal and said sensitivity signal and produce a speed adjustment signal in response to said time error signal and said sensitivity signal, said speed adjuster configured to receive said speed adjustment signal and a nominal speed command signal and produce said speed profile signal in response to said speed adjustment signal and said nominal speed command signal.

17. The system of claim 16 wherein said trajectory generator detects a variation in said sensitivity signal and produces a variability signal in response to said variation.

18. The system of claim 17 wherein said speed profile generator is configured to receive said variability signal and produce said speed profile signal in response to said variability signal.

19. The system of claim 16 wherein said trajectory generator produces a minimum speed adjustment signal.

20. The system of claim 16 wherein said trajectory generator produces a maximum speed adjustment signal.

21. The system of claim 16 wherein said speed profile generator detects whether the aircraft is accelerating or decelerating.

22. The system of claim 1 wherein said trajectory generator determines a difference between said speed profile signal and a predetermined limit, and produces said sensitivity signal responsive to said difference.

23. The system of claim 22 wherein said trajectory generator produces a sensitivity signal for acceleration and a sensitivity signal for deceleration.

24. The system of claim 23 wherein said speed profile generator determines the sense of said time error signal and produces a speed profile signal responsive to said sense.

25. The system of claim 23 wherein said trajectory generator produces a first speed profile signal for deceleration and a second speed profile signal for acceleration.

26. The system of claim 25 wherein said trajectory generator produces a plurality of anticipatory sensitivity signals based on comparison of said first speed profile signal and said second speed profile signal to at least one predetermined limit.

27. The system of claim 26 wherein said speed profile generator determines the sense of the time error signal and applies a sensitivity signal in response to said sense and said anticipatory sensitivity signals.

28. The system of claim 1 wherein said speed profile generator determines a difference between said speed profile signal and a predetermined limit and generates a signal in response to said difference.

29. The system of claim 1 wherein said speed profile generator performs reasonableness checks on said sensitivity signal.

30. The system of claim 1 wherein said speed profile signal is based on a refined sensitivity signal.

31. The system of claim 1 wherein said speed profile generator accommodates at least one required time of arrival waypoint.

32. The system of claim 1 wherein said speed profile generator is configured to accommodate a plurality of required time of arrival waypoints.

33. The system of claim 32 wherein said speed profile generator performs a first operation including initializing a status for each waypoint to either an active status or an inactive status and revising said speed profile signal for each waypoint having an active status;

performs a second operation comprising determining whether the status of each waypoint is proper and correcting the status of each improperly statused waypoint; and

performs a third operation comprising repeating said first operation and said second operation until the status of each waypoint is proper.

34. A method of controlling the flight of an aircraft to cause the aircraft to reach a waypoint substantially at a predetermined time, the method comprising:

producing a time error signal in response to a required time of arrival signal and a speed profile signal,

revising said speed profile signal in response to said time error signal,

producing a sensitivity signal in response to said revised speed profile signal, and

further revising said speed profile signal in response to said sensitivity signal,

wherein said further revising said speed profile signal comprises;

estimating a speed adjustment increment,

estimating a sensitivity of said time error signal to said speed adjustment increment, and

determining a refined speed adjustment increment,

wherein said estimating a sensitivity includes determining a variability of said sensitivity.

35. The method of claim 34 wherein said speed profile signal is revised according to a constant true airspeed method.

36. A method of controlling the flight of an aircraft to cause the aircraft to reach a waypoint substantially at a predetermined time, the method comprising:

producing a time error signal in response to a required time of arrival signal and a speed profile signal,

revising said speed profile signal in response to said time error signal,

producing a sensitivity signal in response to said revised speed profile signal, and

further revising said speed profile signal in response to said sensitivity signal,

wherein said speed profile signal is determined according to a percentage airspeed method.

37. A method of controlling the flight of an aircraft to cause the aircraft to reach a waypoint substantially at a predetermined time, the method comprising:

producing a time error signal in response to a required time of arrival signal and a speed profile signal,

revising said speed profile signal in response to said time error signal,

producing a sensitivity signal in response to said revised speed profile signal,

further revising said speed profile signal in response to said sensitivity signal,

detecting variations in said sensitivity signal and

producing a variability signal in response thereto.

38. The method of claim 37 further comprising producing a minimum speed adjustment signal.

39. The method of claim 37 further comprising producing a maximum speed adjustment signal.

40. A method of controlling the flight of an aircraft to cause the aircraft to reach a waypoint substantially at a predetermined time, the method comprising:

producing a time error signal in response to a required time of arrival signal and a speed profile signal,

revising said speed profile signal in response to said time error signal,

producing a sensitivity signal in response to said revised speed profile signal, and

further revising said speed profile signal in response to said sensitivity signal,

wherein said step of revising said speed profile signal includes;

a first operation including initializing a status for each waypoint to either an active status or an inactive status and revising said speed profile signal for each waypoint having an active status,

a second operation comprising determining whether the status of each waypoint is proper and correcting the status of each improperly statused waypoint, and

a third operation comprising repeating said first operation and said second operation until the status of each waypoint is proper.