Autonomous Environmental Control System and Method For Post-Capture and Pre-Launch Management of an Unmanned Air Vehicle

• US 20060249622A1
• Filed: 05/04/2005
• Published: 11/09/2006
• Est. Priority Date: 05/04/2005
• Status: Abandoned Application

• Current Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Original Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Inventors: Steele, Daniel W.
• Application Number:
  US10/908,255
• Publication Number:
  US 20060249622A1
• Time in Patent Office: Days
• US Class Current: 244/115
• CPC Class Codes: B64F 1/02 for arresting aircraft, e.g. nets or cables
• CPC Class Codes: B64F 1/04 for launching aircraft
• CPC Class Codes: B64U 70/00 Launching, take-off or landing arrangements
• CPC Class Codes: B64U 70/30 for capturing UAVs in flight by ground or sea-based arresting gear, e.g. by a cable or a net
• CPC Class Codes: B64U 70/92 Portable platforms
• CPC Class Codes: B64U 80/70 in containers B64U80/60 takes precedence

Abstract

An embodiment of the invention is directed to a system for controlling and managing a small unmanned air vehicle (UAV) between capture and launch of the UAV. The system includes an enclosure that provides environmental protection and isolation for multiple small UAVs in assembled and/or partially disassembled states. Control and management of the UAVs includes reorientation of a captured UAV from a landing platform and secure hand-off to the enclosure, decontamination, de-fueling, ingress to the enclosure, downloading of mission payload, UAV disassembly, stowage, retrieval and reassembly of the UAV, mission uploading, egress of the UAV from the enclosure, fueling, engine testing and launch readiness. An exemplary system includes two or more robots controlled by a multiple robot controller for autonomously carrying out the functions described above. A modular, compact, portable and autonomous system of UAV control and management is described.

Claims

1. A system for autonomously controlling and managing a small unmanned air vehicle (UAV) between a capture and a launch of the UAV, comprising:

an enclosure;

a) means for accessing a captured UAV;

b) means for ingress of the captured UAV to the enclosure;

c) means for at least one of i) disassembling the UAV within the enclosure, ii) storing the UAV within the enclosure, and iii) retrieving the UAV from storage within the enclosure;

d) means for egress of the UAV from within the enclosure; and

e) means for readying the UAV for launch.

2. The system of claim 1, further comprising at least one multiple robot control means for controlling at least two robotic components of means (a-e) from a single control point.

3. The system of claim 1, wherein the means for disassembling the UAV includes means for at least partially disassembling the UAV.

4. The system of claim 1, wherein the means for storing the UAV within the enclosure includes means for storing the disassembled parts of the UAV.

5. The system of claim 1, wherein the means for retrieving the UAV from within the enclosure includes means for reassembling the UAV.

6. The system of claim 1, further comprising means for at least one of decontaminating and defueling the captured UAV.

7. The system of claim 6, wherein the at least one of the decontamination means and the defueling means are external to the enclosure.

8. The system of claim 1, further comprising means for downloading a payload from the captured UAV.

9. The system of claim 1, further comprising means for uploading a mission instruction for the UAV prior to launching the UAV.

10. The system of claim 1, further comprising means for at least one of fueling the UAV and making an engine test of the UAV, prior to launching the UAV.

11. The system of claim 1, wherein the enclosure includes a space for storing a plurality of disassembled UAVs.

12. The system of claim 11, wherein the space can accommodate 50 or more disassembled UAVs.

13. The system of claim 1, further comprising means for at least one of launching a UAV and capturing an in-flight UAV.

14. The system of claim 1, wherein the means (a-e) are fully automated.

15. The system of claim 14, comprising a common controller programmed to coordinate the operation of means (a-e).

16. The system of claim 1, wherein the system is a modular system.

17. The system of claim 16, wherein the system is a portable system.

18. The system of claim 1, wherein the system provides at least one of a launch cycle and a capture cycle having a cycle time of equal to or less than two minutes.

19. The system of claim 1, wherein the enclosure incorporates an environmentally sealable entry/exit.

20. The system of claim 1, wherein the system is adapted for operation on a ship-based host platform.

21. The system of claim 1, wherein the system is adapted for operation on a land-based host platform.

22. The system of claim 1, wherein the system is a self-propelled, land-based platform.

23. A system for autonomously controlling and managing a small unmanned air vehicle (UAV) between a capture and a launch of the UAV, comprising:

an enclosure;

at least a first robot and a second robot operationally interfaced to the enclosure and programmed and controlled to perform at least two of;

i) access a captured UAV, ii) retrieve the accessed UAV into the enclosure, iii) disassemble the UAV within the enclosure, iv) store the UAV within the enclosure, v) retrieve the UAV from storage within the enclosure, and vi) prepare the UAV for launch; and

at least one multiple robot controller programmed to control the at least first and second robots from a single control point.

24. The system of claim 23, wherein at least one of the at least first and second robots is programmed to partially disassemble the UAV within the enclosure.

25. The system of claim 23, wherein at least one of the at least first and second robots is programmed to store the disassembled parts of the UAV.

26. The system of claim 23, wherein the enclosure includes a plurality of modular compartments for stowage of a plurality of disassembled UAVs.

27. The system of claim 23, wherein at least one of the at least first and second robots is programmed to reassemble the disassembled parts of the UAV.

28. The system of claim 23, further comprising means for at least one of decontaminating and defueling the captured UAV.

29. The system of claim 28, comprising a UAV washing station.

30. The system of claim 28, comprising a UAV fueling station.

31. The system of claim 28, wherein the at least one of the decontamination means and the defueling means are external to the enclosure.

32. The system of claim 23, further comprising means for downloading a payload from the captured UAV.

33. The system of claim 23, further comprising means for uploading a mission instruction for the UAV prior to launching the UAV.

34. The system of claim 23, further comprising means for at least one of fueling the UAV and making an engine test of the UAV, prior to launching the UAV.

35. The system of claim 23, wherein the enclosure includes a space for storing a plurality of disassembled UAVs.

36. The system of claim 23, wherein the system is a portable system.

37. The system of claim 23, wherein the system provides at least one of a launch cycle and a capture cycle having a cycle time of equal to or less than two minutes.

38. The system of claim 23, wherein the enclosure incorporates an environmentally sealable entry/exit.

39. The system of claim 23, wherein the system is adapted for operation on a ship-based host platform.

40. The system of claim 23, wherein the system is adapted for operation on a land-based host platform.

41. The system of claim 23, wherein the system is a self-propelled, land-based platform.