Flight navigation sequencing system and method

• US 20050004745A1
• Filed: 05/15/2003
• Published: 01/06/2005
• Est. Priority Date: 05/15/2003
• Status: Abandoned Application

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Rumbo, Jim R., Hill, Gregory S., Hadley, John C., Bouanani, Adib, Gaier, Chad E.
• Application Number:
  US10/439,390
• Publication Number:
  US 20050004745A1
• Time in Patent Office: Days
• US Class Current: 701/200
• CPC Class Codes: G01C 21/20 Instruments for performing navigational calculations G01C21/24, G01C21/26 take precedence
• CPC Class Codes: G01C 21/22 Plotting boards
• CPC Class Codes: G08G 5/0052 for cruising combined instruments indicating more than one navigational value G01C23/00

Abstract

A flight management system and method is provided that determines segment sequencing during entry into holding patterns and the holding patterns themselves. The flight management system and method monitors the aircraft'"'"'s progress along the active segment of the flight plan to determine what is the appropriate next segment and when to switch control from the active segment to the next segment. The flight management system can determine the appropriate next segment for the aircraft based on a variety of factors. These factors including aircraft position relative to a wayline, the existence of any cross track error, and whether or not the projected aircraft track will intersect an active segment. Preferably, the flight management system evaluates the aircraft state parameters at each wayline crossing to determine which segment is appropriate to control to next. If none of the segments are appropriate, then the control is defaulted to a default segment.

Claims

1. A navigation system for an aircraft, the navigation system comprising:

a sequencing system, the sequencing system evaluating a plurality of segments in a flight plan to determine which of the plurality of segments meets a control criterion, the sequencing system controlling to selected segments from the plurality of segments as the selected segments meet the control criterion.

2. The navigation system of claim 1 wherein the control criterion includes relative orientation of the aircraft.

3. The navigation system of claim 1 wherein the control criterion includes distance to a segment.

4. The navigation system of claim 1 wherein the sequencing system further monitors the aircraft progress along an active segment of a flight plan.

5. The navigation system of claim 1 wherein the sequencing system further determines an inbound delta to a hold orientation, and fixer determines a hold entry type from the inbound delta.

6. The navigation system of claim 1 wherein the sequencing system automatically sequences to a next segment when the aircraft is under control of the navigation system.

7. The navigation system of claim 6 wherein the sequencing system sequences to a most likely next segment when the aircraft is not under active control of the navigation system.

8. The navigation system of claim 1 wherein the sequencing system sequences to a next segment when the aircraft is following the current segment within a specified error distance.

9. The navigation system of claim 8 wherein the sequencing system sequences to the next segment when the aircraft is following the current segment beyond the current specified error distance and the aircraft is on track to intercept the next segment.

10. The navigation system of claim 8 wherein the current specified error distance is equal to a turn radius of a holding pattern.

11. The navigation system of claim 1 wherein the sequencing system locks out used segments while evaluating the plurality of segments in the flight plan.

12. The navigation system of claim 1 wherein the sequencing system determines if the aircraft will intersect one of the plurality of segments by computing an angle between endpoints of the segment.

13. The navigation system of claim 1 wherein the sequencing system determines if the aircraft will intersect one of the plurality of segments by computing an angle that spans a first endpoint of the segment, a second endpoint of the segment, and a tangent line of the segment, and determining if the aircraft heading is within the angle.

14. A navigation system, the navigation system comprising:

a sequencing system, the sequencing system monitoring aircraft progress along an active segment of a flight plan and determining an inbound delta to a hold orientation, the sequencing system determining a hold entry type from the inbound delta, the sequencing system evaluating a plurality of segments in a holding pattern entry algorithm corresponding to the determined hold entry type to determine if the plurality of segments meets a control criterion, the sequencing system controlling to selected segments from the plurality of segments as the selected segments meet the control criterion.

15. The navigation system of claim 14 wherein the sequencing system automatically sequences to a next segment when the aircraft is under control of the navigation system.

16. The navigation system of claim 14 wherein the sequencing system sequences to a most likely next segment when the aircraft is not under active control of the navigation system.

17. The navigation system of claim 14 wherein the sequencing system sequences to a next segment when the aircraft is following the current segment within a specified error distance and when the aircraft crosses a wayline.

18. The navigation system of claim 17 wherein the sequencing system sequences to the next segment when the aircraft is following the current segment beyond the current specified error distance and the aircraft is on track to intercept the next segment.

19. The navigation system of claim 18 wherein the current specified error distance is equal to a turn radius of a holding pattern.

20. The navigation system of claim 14 wherein the sequencing system looks out used segments while evaluating the plurality of segments in the flight plan.

21. The navigation system of claim 14 wherein the sequencing system determines if the aircraft will intersect one of the plurality of segments by computing an angle that spans a first endpoint of the segment, a second endpoint of the segment, and a tangent line of the segment, and determining if the aircraft heading is within the angle.

22. A navigation method for an aircraft, the navigation method comprising the steps of:

a) monitoring progress of the aircraft along an active segment;

b) determining an inbound delta to a hold orientation;

c) determining a hold entry type from the inbound delta;

d) evaluating a plurality of segments in a holding pattern entry algorithm corresponding to the determined hold entry type to determine if the plurality of segments meets a control criterion; and

e) sequencing to selected segments from the plurality of segments as the selected segments meet the control criterion.

23. The method of claim 22 wherein the step of sequencing to the selected segments occurs automatically when the aircraft is under control of the navigation system.

24. The method of claim 22 wherein the step of sequencing to the selected segments comprises sequencing to a most likely next segment when the aircraft is not under active control of the navigation system.

25. The method of claim 22 wherein the step of sequencing to the selected segments comprises sequencing to a next segment when the aircraft is following the current segment within a specified error distance and when the aircraft crosses a wayline.

26. The method of claim 25 wherein the step of sequencing to the selected segments comprises sequencing to the next segment when the aircraft is following the current segment beyond the current specified error distance and the aircraft is on track to intercept the next segment.

27. The method of claim 26 wherein the current specified error distance is equal to a turn radius of a holding pattern.

28. The method of claim 22 wherein the step of evaluating a plurality of segments in a holding pattern entry algorithm comprises locking out used segments while evaluating the plurality of segments in the flight plan.

29. The method of claim 22 wherein the step of evaluating a plurality of segments in a holding pattern entry algorithm comprises determining if the aircraft will intersect one of the plurality of segments by computing an angle between endpoints of the segment.

30. The method of claim 22 wherein the sequencing system determines if the aircraft will intersect one of the plurality of segments by computing an angle that spans a first endpoint of the segment, a second endpoint of the segment, and a tangent line of the segment, and determining if the aircraft heading is within the angle.