Balloon trajectory control system

• US 6,402,090 B1
• Filed: 06/29/1998
• Issued: 06/11/2002
• Est. Priority Date: 06/29/1998
• Status: Expired due to Term

• Current Assignee: Global Aerospace Corporation
• Original Assignee: Global Aerospace Corporation
• Inventors: Aaron, Kim Maynard
• Primary Examiner(s): ELDRED, JOHN W
• Application Number:
  US09/106,563
• Time in Patent Office: 1,443 Days
• Field of Search: 244/24, 244/27, 244/31, 244/32, 244/30
• US Class Current: 244/24
• CPC Class Codes: B64B 1/00 Lighter-than-air aircraft

Abstract

A device to provide control of the trajectory of a lighter than air vehicle, such as a balloon, is provided. A lifting device, such as a wing on end, is suspended on a tether well below the balloon to take advantage of the natural variation in winds at different altitudes. The wing can generate a horizontal lift force that can be directed over a wide range of angles. This force is transmitted to the balloon by the tether. Due to this force, the balloon'"'"'s path is altered depending on the relative sizes of the balloon and the wing. A relatively small amount of power is needed to control the system, possibly with a rudder. As the energy of the wind provides most of the force, the wind'"'"'s energy does most of the work. The balloon is able to avoid hazards, to reach desired targets, to select convenient landing zones, and to provide other operational advantages. As a result, fewer flights must be terminated early due to an inability to control the trajectory, and it is easier to obtain permission to launch since a planned flight path can be achieved within a greater range of conditions.

Claims

1. A trajectory-control device for a lighter-than-air system, comprising:

a frame;

a lift-generating device mounted on the frame;

a flap mounted on the frame; and

a tether, the tether having a first end connected to the frame and a second end for connecting the trajectory-control device to the lighter-than-air system, wherein the trajectory-control device passively generates force on the lighter-than-air system from airflow differences between the lighter-than-air system and the lift-generating device.

2. A trajectory-control device as claimed in claim 1, wherein the lift-generating device includes a sail.

3. A trajectory-control device as claimed in claim 1, wherein the lift-generating device includes a wing.

4. A trajectory-control device as claimed in claim 1, wherein the lift-generating device includes a body of a whirligig arrangement.

5. A trajectory-control device as claimed in claim 1, wherein the tether includes a cable.

6. A trajectory-control device as claimed in claim 1, wherein the frame includes a boom that connects the lift-generating device and the flap.

7. A trajectory-control device as claimed in claim 6, further comprising a counterweight mounted on the boom, wherein the counterweight adjusts a center of mass of the trajectory-control device.

8. A trajectory-control device as claimed in claim 1, further comprising:

an actuator connected to the flap for adjusting a relative orientation of the flap; and

a control system for commanding the actuator.

9. A trajectory-control device as claimed in claim 1, wherein the tether has an extended length of at least 0.5 km.

10. A trajectory-control device as claimed in claim 1, wherein the tether has an extended length that is sufficiently large for controlling a trajectory of the lighter-than-air system.

11. A trajectory-control device for a lighter-than-air system, comprising:

a frame;

a lift-generating device mounted on the frame;

a flap mounted on the frame;

an actuator connected to the flap for adjusting a relative orientation of the flap;

a control system for commanding the actuator; and

a tether, the tether having a first end connected to the frame and a second end for connecting the trajectory-control device to the lighter-than-air system, and the tether having an extended length of at least 0.5 km, wherein the trajectory-control device passively generates force on the lighter-than-air system from airflow differences between the lighter-than-air system and the lift-generating device.

12. A trajectory-control device for a lighter-than-air system, comprising:

a frame;

a lift-generating device mounted on the frame;

a flap mounted on the frame;

an actuator connected to the flap for adjusting a relative orientation of the flap;

a control system for commanding the actuator; and

a tether, the tether having a first end connected to the frame and a second end for connecting the trajectory-control device to the lighter-than-air system, wherein the trajectory-control device passively generates force on the lighter-than-air system from airflow differences between the lighter-than-air system and the lift-generating device, and the tether has an extended length that is sufficiently large for controlling a trajectory of the lighter-than-air system.

13. A trajectory-control device for a lighter-than-air system, comprising:

a lift-generating device;

a flap mounted on the lift-generating device; and

a tether, the tether having a first end connected to the lift-generating device and a second end for connecting the trajectory-control device to the lighter-than-air system, wherein the trajectory-control device passively generates force on the lighter-than-air system from airflow differences between the lighter-than-air system and the lift-generating device.

14. A trajectory-control device as claimed in claim 13, wherein the lift-generating device includes a body of a whirligig arrangement.

15. A trajectory-control device as claimed in claim 13, wherein the tether includes a cable.

16. A trajectory-control device as claimed in claim 13, further comprising:

an actuator connected to the flap for adjusting a relative orientation of the flap; and

a control system for commanding the actuator.

17. A trajectory-control device as claimed in claim 13, wherein the tether has an extended length of at least 0.5 km.

18. A trajectory-control device as claimed in claim 13, wherein the tether has an extended length that is sufficiently large for controlling a trajectory of the lighter-than-air system.

19. A trajectory-control device for a lighter-than-air system, comprising:

means for generating lift from air velocity differences; and

means for connecting the lift-generating means to the lighter-than-air system, wherein the connecting means is non-rigid, and the trajectory-control device passively generates force on the lighter-than-air system from airflow differences between the lighter-than-air system and the lift-generating means.

20. A trajectory-control device according to claim 19, wherein

the lift-generating means includes means for controlling a lift force generated by the lift-generating means.

21. A trajectory-control device according to claim 19, wherein the connecting means has an extended length of at least 0.5 km.

22. A trajectory-control device according to claim 19, wherein the connecting means has an extended length that is sufficiently large for controlling a trajectory of the lighter-than-air system.

23. An aircraft comprising a lighter-than-air system and a trajectory-control device, the trajectory-control comprising:

a frame;

a lift-generating device mounted on the frame;

a flap mounted on the frame; and

a tether, the tether having a first end connected to the frame and a second end connected to the lighter-than-air system, wherein the trajectory-control device passively generates force on the lighter-than-air system from airflow differences between the lighter-than-air system and the lift-generating device.

24. An aircraft as claimed in claim 23, wherein the lift-generating device includes a sail.

25. An aircraft as claimed in claim 23, wherein the lift-generating device includes a wing.

26. An aircraft as claimed in claim 23, wherein the lift-generating device includes a body of a whirligig arrangement.

27. An aircraft as claimed in claim 23, wherein the tether includes a cable.

28. An aircraft as claimed in claim 23, wherein the frame includes a boom that connects the lift-generating device and the flap.

29. An aircraft as claimed in claim 28, wherein

the lift-generating device further comprises a counterweight mounted on the boom so that the counterweight adjusts a center of mass of the trajectory-control device.

30. An aircraft as claimed in claim 23, wherein the trajectory-control device further comprises:

an actuator connected to the flap for adjusting a relative orientation of the flap; and

a control system for commanding the actuator.

31. An aircraft as claimed in claim 23, wherein the tether has an extended length of at least 0.5 km.

32. An aircraft as claimed in claim 23, wherein the tether has an extended length that is sufficiently large for controlling a trajectory of the lighter-than-air system.

33. An aircraft comprising a lighter-than-air system and a trajectory-control device, the trajectory-control device comprising:

a frame;

a lift-generating device mounted on the frame;

a flap mounted on the frame;

an actuator connected to the flap for adjusting a relative orientation of the flap;

a control system for commanding the actuator; and

a tether, the tether having a first end connected to the frame and a second end connected to the lighter-than-air system, and the tether having an extended length of at least 0.5 km, wherein the trajectory-control device passively generates force on the lighter-than-air system from airflow differences between the lighter-than-air system and the lift-generating device.

34. An aircraft comprising a lighter-than-air system and a trajectory-control device, the trajectory-control device comprising:

a frame;

a lift-generating device mounted on the frame;

a flap mounted on the frame;

an actuator connected to the flap for adjusting a relative orientation of the flap;

a control system for commanding the actuator; and

a tether, the tether having a first end connected to the frame and a second end connected to the lighter-than-air system, wherein the trajectory-control device passively generates force on the lighter-than-air system from airflow differences between the lighter-than-air system and the lift-generating device, and the tether has an extended length that is sufficiently large for controlling a trajectory of the lighter-than-air system.

35. An aircraft comprising a lighter-than-air system and a trajectory-control device, the trajectory-control device comprising:

a lift-generating device;

a flap mounted on the lift-generating device; and

a tether, the tether having a first end connected to the lift-generating device and a second end connected to the lighter-than-air system, wherein the trajectory-control device passively generates force on the lighter-than-air system from airflow differences between the lighter-than-air system and the lift-generating device.

36. An aircraft as claimed in claim 35, wherein the lift-generating device includes a body of a whirligig arrangement.

37. An aircraft as claimed in claim 35, wherein the tether includes a cable.

38. An aircraft as claimed in claim 35, further comprising:

an actuator connected to the flap for adjusting a relative orientation of the flap; and

a control system for commanding the actuator.

39. An aircraft as claimed in claim 35, wherein the tether has an extended length of at least 0.5 km.

40. An aircraft as claimed in claim 35, wherein the tether has an extended length that is sufficiently large for controlling a trajectory of the lighter-than-air system.

41. A method for trajectory control of a lighter-than-air system, comprising:

connecting a lift-generating device to the lighter-than-air system with a tether;

connecting a flap to the lift-generating device, wherein a relative orientation of the flap controls force on the lighter-than-air system that is passively generated from airflow differences between the lighter-than-air system and the lift-generating device; and

adjusting the relative orientation of the flap.

42. A method as claimed in claim 41, wherein the lift-generating device includes a sail.

43. A method as claimed in claim 41, wherein the lift-generating device includes a wing.

44. A method as claimed in claim 41, wherein the lift-generating device includes a body of a whirligig arrangement.

45. A method as claimed in claim 41, further comprising:

extending the tether so that the tether has an extended length of at least 0.5 km.

46. A method as claimed in claim 41, further comprising:

extending the tether so that the tether has an extended length that is sufficiently large for controlling a trajectory of the lighter-than-air system.

47. A trajectory-control device for a lighter-than-air system, comprising:

a lift-generating device; and

a tether, the tether having a first end connected to the lift-generating device and a second end for connecting the trajectory-control device to the lighter-than-air system, wherein the trajectory-control device passively generates force on the lighter-than-air system from airflow differences between the lighter-than-air system and the lift-generating device.

48. A trajectory-control device as claimed in claim 47, wherein the lift-generating device includes a body of a whirligig arrangement.

49. A trajectory-control device as claimed in claim 47, wherein the tether includes a cable.

50. A trajectory-control device as claimed in claim 47, wherein the tether has an extended length of at least 0.5 km.

51. A trajectory-control device as claimed in claim 47, wherein the tether has an extended length that is sufficiently large for controlling a trajectory of the lighter-than-air system.

52. An aircraft comprising a lighter-than-air system and a trajectory-control device, the trajectory-control device comprising:

a lift-generating device; and

a tether, the tether having a first end connected to the lift-generating device and a second end connected to the lighter-than-air system, wherein the trajectory-control device passively generates force on the lighter-than-air system from airflow differences between the lighter-than-air system and the lift-generating device.

53. An aircraft as claimed in claim 52, wherein the lift-generating device includes a body of a whirligig arrangement.

54. An aircraft as claimed in claim 52, wherein the tether includes a cable.

55. An aircraft as claimed in claim 52, wherein the tether has an extended length of at least 0.5 km.

56. An aircraft as claimed in claim 52, wherein the tether has an extended length that is sufficiently large for controlling a trajectory of the lighter-than-air system.

57. A method for trajectory control of a lighter-than-air system, comprising:

connecting a lift-generating device to the lighter-than-air system with a tether for passively generating force on the lighter-than-air system from airflow differences between the lighter-than-air system and the lift-generating device.

58. A method as claimed in claim 57, wherein the lift-generating device includes a sail.

59. A method as claimed in claim 57, wherein the lift-generating device includes a wing.

60. A method as claimed in claim 57, wherein the lift-generating device includes a body of a whirligig arrangement.

61. A method as claimed in claim 57, further comprising:

extending the tether so that the tether has an extended length of at least 0.5 km.

62. A method as claimed in claim 57, further comprising:

extending the tether so that the tether has an extended length that is sufficiently large for controlling a trajectory of the lighter-than-air system.