Autonomous station keeping system for formation flight

• US 7,024,309 B2
• Filed: 08/28/2003
• Issued: 04/04/2006
• Est. Priority Date: 08/28/2003
• Status: Expired due to Fees

• Current Assignee: The Boeing Co.
• Original Assignee: United States Of America As Represented By The Secretary Of The Air Force
• Inventors: Doane, Paul M.
• Primary Examiner(s): Chin, Gary
• Application Number:
  US10/650,606
• Publication Number:
  US 20050055143A1
• Time in Patent Office: 950 Days
• Field of Search: 701/3, 701/120, 701/301, 342/29, 342/30, 342/31, 342/32, 340/961
• US Class Current: 701/301
• CPC Class Codes: B64C 13/18 using automatic pilot
• CPC Class Codes: B64C 13/20 using radiated signals
• CPC Class Codes: G01S 13/933 of aircraft or spacecraft
• CPC Class Codes: G01S 19/49 whereby the further system is an inertial position system, e.g. loosely-coupled
• CPC Class Codes: G01S 5/0072 Transmission between mobile stations, e.g. anti-collision systems
• CPC Class Codes: G05D 1/104 involving a plurality of aircrafts, e.g. formation flying traffic control systems for aircraft G08G5/00
• CPC Class Codes: G08G 5/0008 with other aircraft

Abstract

A system for autonomously keeping an aircraft'"'"'s station in a formation flight of a plurality of aircraft includes a navigation system configured to determine a position of an aircraft. A data link is configured to allow the aircraft to communicate data with at least one other aircraft in the formation flight of the plurality of aircraft. A sensor is configured to detect a presence of another aircraft within a predetermined distance of the aircraft. A processor is configured to provide control signals to the aircraft'"'"'s autoflight system to keep the aircraft at a predetermined station relative to the other of the plurality of aircraft in the formation flight.

Claims

1. A system for autonomously keeping an aircraft'"'"'s station in a formation flight of a plurality of aircraft, the system comprising:

a navigation system configured to determine a position of the aircraft;

a data link configured to allow the aircraft to communicate data with at least one other aircraft in a formation flight of a plurality of aircraft;

a sensor configured to sense position of the at least one other aircraft within a predetermined distance of the aircraft; and

a processor configured to provide control signals to keep the aircraft at a predetermined station relative to the at least one other of the plurality of aircraft in the formation flight based upon the sensed position of the at least one other aircraft, the processor including;

a first component configured to generate first control signals for performing a collision avoidance maneuver when the position of the aircraft is within a first predetermined threshold from the at least one other aircraft in the formation; and

a second component configured to generate second control signals for performing a collision deconfliction maneuver when the position of the aircraft is within a second predetermined threshold from the at least one other aircraft in the formation, the second predetermined threshold being greater than the first predetermined threshold.

2. The system of claim 1, wherein the navigation system includes an embedded GPS inertial navigation system.

3. The system of claim 2, wherein position uncertainty of the navigation system is within around 30 meters.

4. The system of claim 2, wherein position uncertainty of the navigation system is within around 1 meter.

5. The system of claim 4, wherein the navigation system is configured to process PY GPS signals.

6. The system of claim 1, wherein the data link includes Link 16.

7. The system of claim 1, wherein the data link includes ARC 210 data link.

8. The system of claim 1, wherein the data link includes a millimeter wave radar.

9. The system of claim 1, wherein the data communicated includes a flight plan of the aircraft.

10. The system of claim 1, wherein the sensor includes a millimeter wave radar.

11. The system of claim 10, wherein the predetermined distance is around 10 miles.

12. The system of claim 1, wherein the predetermined station is within around 1,000 feet of at least one other aircraft in the formation.

13. The system of claim 1, wherein the collision avoidance maneuver includes at least one of changing altitude of the aircraft in an opposite direction from changing altitude of the at least one other aircraft and turning away from the at least one other aircraft.

14. The system of claim 1, wherein the first predetermined threshold includes a time period in a range of around 1 second to around 2 seconds before a collision becomes unavoidable.

15. The system of claim 1, wherein the first predetermined threshold includes a distance of around 150 feet.

16. The system of claim 1, wherein the collision deconfliction maneuver includes at least one of changing altitude of the aircraft in an opposite direction from changing altitude of the at least one other aircraft and turning away from the at least one other aircraft and changing speed of the aircraft opposite changing speed of the at least one other aircraft.

17. The system of claim 1, wherein the second predetermined threshold includes a time period of around 30 seconds before a collision becomes unavoidable.

18. A system for autonomously keeping aircraft'"'"'s station in a formation flight of a plurality of aircraft, the system comprising:

an embedded GPS inertial navigation system configured to determine a position of the aircraft;

a data link configured to allow the aircraft to communicate data with at least one other aircraft in a formation flight of a plurality of aircraft;

a millimeter wave radar system configured to sense position of the at least one other aircraft within a predetermined distance of the aircraft; and

a processor configured to provide control signals to keep the aircraft at a predetermined station relative to the at least one other of the plurality of aircraft in the formation flight based upon the sensed position of the at least one other aircraft, the processor including;

a first component configured to generate first control signals for performing a collision avoidance maneuver when the position of the aircraft is within a first predetermined threshold from the at least one other aircraft in the formation; and

a second component configured to generate second control signals for performing a collision deconfliction maneuver when the position of the aircraft is within a second predetermined threshold from the at least one other aircraft in the formation, the second predetermined threshold being greater than the first predetermined threshold.

19. The system of claim 18, wherein position uncertainty of the navigation system is within around 30 meters.

20. The system of claim 18, wherein position uncertainty of the navigation system is within around 1 meter.

21. The system of claim 18, wherein the navigation system is configured to process PY GPS signals.

22. The system of claim 18, wherein the data link includes Link 16.

23. The system of claim 18, wherein the data link includes ARC 210 data link.

24. The system of claim 18, wherein the data link includes millimeter wave radar.

25. The system of claim 18, wherein the data communicate includes a flight plan of the aircraft.

26. The system of claim 18, wherein the predetermined station is within around 1,000 feet of other aircraft in the formation.

27. The system of claim 18, wherein the predetermined distance is around 10 miles.

28. The system of claim 18, wherein the collision avoidance maneuver includes at least one of changing altitude of the aircraft in an opposite direction from changing altitude of the at least one other aircraft and turning away from the at least one other aircraft.

29. The system of claim 18, wherein the first predetermined threshold includes a time period in a range of around 1 second to around 2 seconds before a collision becomes unavoidable.

30. The system of claim 18, wherein the first predetermined threshold includes a distance of around 150 feet.

31. The system of claim 18, wherein the collision deconfliction maneuver includes at least one of changing altitude of the aircraft in an opposite direction from changing altitude of the at least one other aircraft and turning away from the at least one other aircraft and changing speed of the aircraft opposite changing speed of the at least one other aircraft.

32. The system of claim 18, wherein the second predetermined threshold includes a time period of around 30 seconds before a collision becomes unavoidable.

33. A method of automatically keeping a predetermined station of an aircraft flying in a formation flight of a plurality of aircraft, the method comprising:

transmitting a flight plan of an aircraft flying in a formation flight of a plurality of aircraft, the aircraft having a predetermined station in the formation flight relative to other aircraft in the formation flight;

determining position of the aircraft;

sensing positions of the other aircraft in the formation;

comparing the position of the aircraft with the positions of the other aircraft in the formation;

automatically adjusting the position of the aircraft relative to positions of the other aircraft flying in the formation flight such that the predetermined station of the aircraft is maintained;

performing a collision avoidance maneuver when the position of the aircraft is within a first predetermined threshold from the other aircraft in the formation; and

performing a collision deconfliction maneuver when the position of the aircraft is within a second predetermined threshold from the other aircraft in the formation, the second predetermined threshold being greater than the first predetermined threshold.

34. The method of claim 33, wherein the automatically adjusting the position includes adjusting at least one of course and speed and altitude of the aircraft.

35. The method of claim 33, wherein the predetermined station is at least around 1,000 feet from the other aircraft in the formation.

36. The method of claim 33, wherein the position of the aircraft is determined within a position uncertainty of around 30 meters.

37. The method of claim 33, wherein the position of the aircraft is determined within a position uncertainty of around 1 meter.

38. The method of claim 33, wherein the other aircraft are sensed at distances of at least around 10 miles from the aircraft.

39. The method of claim 33, wherein the performing the collision avoidance maneuver includes at least one of changing altitude of the aircraft in an opposite direction from changing altitude of the other aircraft and turning away from the other aircraft.

40. The method of claim 33, wherein the first predetermined threshold includes a time period in a range of around 1 second to around 2 seconds before a collision becomes unavoidable.

41. The method of claim 33, wherein the first predetermined threshold includes a distance of around 150 feet.

42. The method of claim 33, wherein the performing the collision deconfliction maneuver includes at least one of changing altitude of the aircraft in an opposite direction from changing altitude of the other aircraft and turning away from the other aircraft and changing speed of the aircraft opposite changing speed of the other aircraft.

43. The method of claim 33, wherein the second predetermined threshold includes a time period of around 30 seconds before a collision becomes unavoidable.

44. An aircraft comprising:

a fuselage;

a pair of wings;

a plurality of flight control surfaces;

at least one engine;

an autoflight system; and

a system for autonomously keeping the aircraft'"'"'s station in a formation flight of a plurality of aircraft, the system including;

a navigation system configured to determine a position of the aircraft;

a data link configured to allow the aircraft to communicate data with at least one other aircraft in a formation flight of a plurality of aircraft;

a sensor configured to sense position of the at least one other aircraft within a predetermined distance of the aircraft; and

a processor configured to provide control signals to the autoflight system to keep the aircraft at a predetermined station relative to the other of the plurality of aircraft in the formation flight based upon the sensed position of the at least one other aircraft, the processor including;

a first component configured to generate first control signals for performing a collision avoidance maneuver when the position of the aircraft is within a first predetermined threshold from the at least one other aircraft in the formation; and

a second component configured to generate second control signals for performing a collision deconfliction maneuver when the position of the aircraft is within a second predetermined threshold from the at least one other aircraft in the formation, the second predetermined threshold being greater than the first predetermined threshold.

45. The aircraft of claim 44, wherein the navigation system includes an embedded GPS inertial navigation system.

46. The aircraft of claim 45, wherein position uncertainty of the navigation system is within around 30 meters.

47. The aircraft of claim 45, wherein position uncertainty of the navigation system is within around 1 meter.

48. The aircraft of claim 47, wherein the navigation system is configured to process PY GPS signals.

49. The aircraft of claim 44, wherein the data link includes Link 16.

50. The aircraft of claim 44, wherein the data link includes an ARC 210 data link.

51. The aircraft of claim 44, wherein the data link includes a millimeter wave radar.

52. The aircraft of claim 44, wherein the data communicated includes a flight plan of the aircraft.

53. The aircraft of claim 44, wherein the sensor includes a millimeter wave radar.

54. The aircraft of claim 53, wherein the predetermined distance is around 10 miles.

55. The aircraft of claim 44, wherein the predetermined station is within around 1,000 feet of at least one other aircraft in the formation.

56. The aircraft of claim 44, wherein the collision avoidance maneuver includes at least one of changing altitude of the aircraft in opposite direction from changing altitude of the least one other aircraft and turning away from the at least one other aircraft.

57. The system of claim 44, wherein the first predetermined threshold includes a time period in a range of around 1 second to around 2 seconds before a collision becomes unavoidable.

58. The system of claim 44, wherein the first predetermined threshold includes a distance of around 150 feet.

59. The aircraft of claim 44, wherein the collision deconfliction maneuver includes at least one of changing altitude of the aircraft in an opposite direction from changing altitude of the at least one other aircraft and turning away from the at least one other aircraft and changing speed of the aircraft opposite changing speed of the at least one other aircraft.

60. The aircraft of claim 44, wherein the second predetermined threshold includes a time period of around 30 seconds before a collision becomes unavoidable.