Aerial vehicle system

• US 9,975,632 B2
• Filed: 04/08/2016
• Issued: 05/22/2018
• Est. Priority Date: 04/08/2016
• Status: Active Grant

• Current Assignee: Drona, LLC
• Original Assignee: Drona, LLC
• Inventors: Alegria, Loren
• Primary Examiner(s): Jeanglaude, Gertrude Arthur
• Application Number:
  US15/095,011
• Publication Number:
  US 20170291704A1
• Time in Patent Office: 774 Days
• Field of Search: 701 2, 701 13, 701 14, 701 15, 701 36, 244 30
• CPC Class Codes: B64C 39/022 Tethered aircraft
• CPC Class Codes: B64C 39/024 of the remote controlled vehicle type, i.e. RPV
• CPC Class Codes: B64D 47/08 Arrangements of cameras
• CPC Class Codes: B64U 10/13 Flying platforms
• CPC Class Codes: B64U 10/60 Tethered aircraft
• CPC Class Codes: B64U 20/30 for safety, e.g. with frangible components rotor guards B64U30/299
• CPC Class Codes: B64U 20/65 Composite materials
• CPC Class Codes: B64U 2101/30 for imaging, photography or videography
• CPC Class Codes: B64U 2101/60 for transporting passengers; for transporting goods other than weapons
• CPC Class Codes: B64U 2101/64 for parcel delivery or retrieval
• CPC Class Codes: B64U 2201/10 autonomous, i.e. by navigating independently from ground or air stations, e.g. by using inertial navigation systems [INS]
• CPC Class Codes: B64U 2201/102 adapted for flying in formations
• CPC Class Codes: B64U 50/19 using electrically powered motors
• CPC Class Codes: B64U 50/34 In-flight charging photovoltaics B64U50/31
• CPC Class Codes: G01C 21/005 with correlation of navigation data from several sources, e.g. map or contour matching G01C21/30 takes precedence
• CPC Class Codes: G01C 21/1652 with ranging devices, e.g. LIDAR or RADAR
• CPC Class Codes: G01C 21/1654 with electromagnetic compass
• CPC Class Codes: G01C 21/1656 with passive imaging devices, e.g. cameras
• CPC Class Codes: G01S 13/933 of aircraft or spacecraft
• CPC Class Codes: G01S 15/02 using reflection of acoustic waves G01S15/66 takes precedence
• CPC Class Codes: G01S 17/933 : of aircraft or spacecraft
• CPC Class Codes: G01S 19/15 : Aircraft landing systems
• CPC Class Codes: G01S 5/16 : using electromagnetic waves other than radio waves
• CPC Class Codes: G01S 5/163 : Determination of attitude using inertial means G01C9/00; control of attitude G05D1/49
• CPC Class Codes: G05D 1/0866 : specially adapted to captive aircraft
• 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 5/0013 : with a ground station
• CPC Class Codes: G08G 5/0039 : Modification of a flight plan
• CPC Class Codes: G08G 5/0043 : Traffic management of multiple aircrafts from the ground G08G5/003 takes precedence; data processing specially designed for resource management, e.g. scheduling or allocating time, human or machine resources G06Q10/06
• CPC Class Codes: G08G 5/0069 : specially adapted for an unmanned aircraft
• CPC Class Codes: G08G 5/0086 : for monitoring terrain radar or analogous systems specially adapted for terrain avoidance G01S13/935
• CPC Class Codes: G08G 5/045 : Navigation or guidance aids, e.g. determination of anti-collision manoeuvers radar or analogous systems specially adapted for anti-collision between aircraft G01S13/933

Abstract

A system is provided for maneuvering a payload in an air space constrained by one or more obstacles, and may include first and second aerial vehicles coupled by a tether to a ground station. Sensor systems and processors in the ground station and aerial vehicles may track obstacles and the tether'"'"'s and the vehicles'"'"' positions and attitude to maneuver the payload and the tether to carry out a mission. The sensor system may include airborne cameras providing data for a scene reconstruction process and simultaneous mapping of obstacles and localization of aerial vehicles relative to the obstacles. The aerial vehicles may include a frame formed substantially of a composite material for preventing contact of the rotors with the tether segments.

Claims

1. A system for maneuvering a payload in an air space constrained by one or more obstacles, the system comprising:

a first aerial vehicle defining a plurality of flight characteristics and having a processor for handling data about the flight characteristics of the first aerial vehicle;

a second aerial vehicle configured to carry the payload, the second aerial vehicle defining a plurality of flight characteristics and having a processor for handling data about the flight characteristics of the second aerial vehicle;

a first sensor system carried by one of the first and second aerial vehicles, the sensor system coupled to the processor in the one of the first and second aerial vehicles that is carrying the first sensor system, the sensor configured to gather data about obstacles in the air space and to develop data about flight characteristics of at least one of the first and second aerial vehicles, the sensor system configured to provide the data to the processor to which the sensor system is coupled;

a ground station having a flight control processor configured to maintain a first dataset about obstacles in the air space and a second dataset about flight characteristics of the first and second aerial vehicles;

a first tether segment coupling the ground station to the first aerial vehicle;

a second tether segment coupling the second aerial vehicle to the first aerial vehicle.

2. The system of claim 1 wherein the first sensor system includes an obstacle sensor selected from the group of a camera-based sensor, a laser-based sensor, a radar-based sensor, a LIDAR-based sensor, and an acoustic-based sensor.

3. The system of claim 2 wherein the first sensor system further includes a position sensor selected from the group of a GPS unit, an inertial navigation unit, an inertial measurement unit, and a barometer.

4. The system of claim 2 wherein the first sensor system further includes an attitude sensor selected from the group of a magnetometer, an accelerometer, and a sun sensor.

5. The system of claim 1 further comprising:

a second sensor system carried by the other one of the first and second aerial vehicles, the second sensor system including a sensor selected from the group of an obstacle sensor, a position sensor, and an attitude sensor, the second sensor system providing data about flight characteristics of the aerial vehicle by which it is carried to the processor in the aerial vehicle.

6. The system of claim 5 wherein at least one of the first and second sensor systems includes an array of four cameras carried by the aerial vehicle.

7. The system of claim 6 wherein the four cameras are located at four maximally separated positions on the aerial vehicle.

8. The system of claim 6 wherein the processor on the aerial vehicle with the sensor system with the four cameras receives data from the cameras and processes the data using a scene reconstruction process.

9. The system of claim 5 wherein the processors in the aerial vehicles and the ground station provide simultaneous mapping of obstacles and localization of aerial vehicles relative to the obstacles.

10. The system of claim 1 wherein the data gathered by the first sensor system about obstacles includes data about fixed obstacles.

11. The system of claim 1 wherein the data gathered by the first sensor system about obstacles includes data about moving obstacles.

12. The system of claim 11 wherein the data gathered by the first sensor system about moving obstacles includes data about the other aerial vehicle.

13. The system of claim 1 wherein the first tether segment provides a path for power from the ground station to the first aerial vehicle.

14. The system of claim 1 wherein the second tether segment provides a path for power from the first aerial vehicle to the second aerial vehicle.

15. The system of claim 1 wherein the tether segments provide a path for data transmission between the ground station and the aerial vehicles.

16. The system of claim 1 wherein at least one of the aerial vehicles has a wireless link to the ground station for data transmission between the ground station and the aerial vehicle.

17. The system of claim 1 wherein at least one of the aerial vehicles further includes a plurality of spaced-apart rotors, the rotors configured to spin about a substantially vertical axis during flight of the aerial vehicle, the aerial vehicle further including a frame with a structure for preventing contact of the rotors with the tether segments.

18. A tethered aerial vehicle system comprising:

a ground station;

an aerial vehicle including a plurality of spaced-apart rotors, each rotor configured to spin about a substantially vertical axis during flight of the aerial vehicle, wherein the substantially vertical axes are spaced apart from one another;

a tether segment coupling the ground station to the aerial vehicle;

the aerial vehicle further including a frame with a structure for preventing contact of the rotors with the tether segment, the frame defining a plurality of corners and a plurality of substantially straight outer edges interconnecting the corners, and wherein each rotor is located adjacent a corner.

19. The system of claim 18 wherein the structure for preventing contact of the rotors with the tether segment includes a stand-off joint coupled between the tether segment and the aerial vehicle.

20. The system of claim 18 wherein the frame defines a planform that is substantially quadrilateral and surrounds the rotors to prevent contact of the rotors with the tether segment.

21. The system of claim 20 wherein the planform includes a slot.

22. The system of claim 21 wherein the frame includes a stand-off joint coupled between the tether segment and the aerial vehicle, and further wherein the stand-off joint is pivotally coupled to the aerial vehicle for movement through the slot.

23. The system of claim 18 wherein the frame includes a band defining an outline of a planform having a substantially quadrilateral shape.

24. The system of claim 23 wherein the band is formed substantially of a composite material.

25. The system of claim 24 wherein the substantially composite material includes an aramid-epoxy composite.

26. A system for maneuvering a payload in an air space constrained by one or more obstacles, the system comprising:

a first aerial vehicle defining a plurality of flight characteristics and having a processor for handling data about the flight characteristics of the first aerial vehicle;

a second aerial vehicle configured to carry the payload, the second aerial vehicle defining a plurality of flight characteristics and having a processor for handling data about the flight characteristics of the second aerial vehicle;

a first sensor system carried by one of the first and second aerial vehicles, the sensor system coupled to the processor in the one of the first and second aerial vehicles that is carrying the first sensor system, the sensor configured to gather data about obstacles in the air space and to develop data about flight characteristics of at least one of the first and second aerial vehicles, the sensor system configured to provide the data to the processor to which the sensor system is coupled;

a ground station having a flight control processor configured to maintain a first dataset about obstacles in the air space and a second dataset about flight characteristics of the first and second aerial vehicles;

a first tether segment coupling the ground station to the first aerial vehicle;

a second tether segment coupling the second aerial vehicle to the first aerial vehicle; and

wherein at least one of the aerial vehicles further includes a plurality of spaced-apart rotors, the rotors configured to spin about a substantially vertical axis during flight of the aerial vehicle, the aerial vehicle further including a frame with a structure for preventing contact of the rotors with the tether segments.

27. The system of claim 26 further comprising:

a second sensor system carried by the other one of the first and second aerial vehicles, the second sensor system including a sensor selected from the group of an obstacle sensor, a position sensor, and an attitude sensor, the second sensor system providing data about flight characteristics of the aerial vehicle by which it is carried to the processor in the aerial vehicle.

28. The system of claim 27 wherein the processors in the aerial vehicles and the ground station provide simultaneous mapping of obstacles and localization of aerial vehicles relative to the obstacles.

29. The system of claim 26 wherein the tether segments provide a path for power from the ground station to the aerial vehicles.

30. The system of claim 29 wherein the tether segments provide a path for data transmission between the ground station and the aerial vehicles.

31. The system of claim 29 wherein at least one of aerial vehicles has a wireless link to the ground station for data transmission between the ground station and the aerial vehicle.

32. The system of claim 26 wherein the structure for preventing contact of the rotors with the tether segment includes a stand-off joint coupled between the tether segment and the aerial vehicle.

33. The system of claim 26 wherein the frame defines a planform that is substantially quadrilateral and surrounds the rotors to prevent contact of the rotors with the tether segment.

34. The system of claim 33 wherein the planform includes a slot.

35. The system of claim 34 wherein the frame includes a stand-off joint coupled between the tether segment and the aerial vehicle, and further wherein the stand-off joint is pivotally coupled to the aerial vehicle for movement through the slot.

36. A system for maneuvering a payload in an air space constrained by one or more obstacles, the system comprising:

an aerial vehicle defining an airframe and configured to carry the payload, the aerial vehicle having a processor for handling data about the flight characteristics of the aerial vehicle;

a sensor system carried by the aerial vehicle, the sensor system coupled to the processor in the aerial vehicle, the sensor system including a plurality of cameras pointing outward from the airframe, the cameras configured to gather data about obstacles in the air space and to provide the data to the processor,

and further wherein the processor receives the data from the cameras and processes the data using a scene reconstruction process.

37. The system of claim 36 wherein the scene reconstruction process includes a stereophotogrammetry process.

38. The system of claim 36 wherein the scene reconstruction process includes an optical flow process.

39. The system of claim 36 further comprising a ground station and a tether coupling the ground station to the aerial vehicle.

40. The system of claim 39 wherein the tether provides a path for power from the ground station to the aerial vehicle.

41. The system of claim 39 wherein the tether provides a path for data transmission between the ground station and the aerial vehicle.

42. The system of claim 39 wherein the aerial vehicle has a wireless link to the ground station for data transmission between the ground station and the aerial vehicle.

43. The system of claim 36 further comprising a ground station, a second aerial vehicle, and first and second tether segments coupling the ground station and the aerial vehicles.

44. The system of claim 36 wherein the processor uses a stereophotogrammetry process and an optical flow process to process the data from the cameras.

45. The system of claim 44 wherein the processor uses a key frame bundle adjustment in calculating at least one vector to at least one obstacle.

46. The system of claim 45 wherein the processor uses the key frame bundle adjustment to calculate a trajectory of the aerial vehicle.

47. The system of claim 36 wherein the sensor system further includes a position sensor selected from the group of a GPS unit, an inertial navigation unit, an inertial measurement unit, and a barometer, the position sensor providing data to the processor.

48. The system of claim 47 wherein the processor uses an extended Kalman filter to integrate data from the position sensor with data from the cameras.

49. The system of claim 36 wherein the sensor system further includes an attitude sensor selected from the group of a magnetometer, an accelerometer, and a sun sensor, the attitude sensor providing data to the processor.

50. The system of claim 49 wherein the processor uses an extended Kalman filter to integrate data from the attitude sensor with data from the cameras.

51. The system of claim 36 wherein the processor in the aerial vehicle provides simultaneous mapping of obstacles and localization of the aerial vehicle relative to the obstacles.

52. The system of claim 36 wherein the processor in the aerial vehicle includes more than one processing units.

53. The system of claim 52 wherein the processing units in the aerial vehicle include a camera processing unit for processing data from each of the cameras.

54. The system of claim 53 wherein the processing units in the aerial vehicle include a processing unit for integrating data from the camera processing units to calculate a navigation solution of the aerial vehicle.

55. The system of claim 53 wherein the camera processing units in the aerial vehicle include at least one graphical processing unit.

56. The system of claim 36 wherein each camera pointing outward from the airframe of the aerial vehicle defines a field of view, and wherein the fields of view of at least two cameras are overlapping.

57. The system of claim 56 wherein the plurality of cameras includes at least three cameras pointing outward from the airframe of the vehicle.

58. The system of claim 56 wherein the plurality of cameras includes at least four cameras pointing outward from the airframe of the vehicle.

59. The system of claim 56 wherein the airframe frame defines a planform that is substantially quadrilateral, the planform having four corners, and wherein one of the four cameras is located adjacent each corner of the planform.

60. A tethered aerial vehicle system comprising:

a ground station;

an aerial vehicle including a plurality of spaced-apart rotors, the rotors configured to spin about a substantially vertical axis during flight of the aerial vehicle, the aerial vehicle further including a frame;

a stand-off joint coupled to the frame of the aerial vehicle;

a tether segment coupled between the ground station and the stand-off joint.

61. The system of claim 60 wherein the frame defines a planform that is substantially quadrilateral and surrounds the rotors to prevent contact of the rotors with the tether segment.

62. The system of claim 61 wherein the planform includes a slot.

63. The system of claim 62 wherein the stand-off joint is pivotally movable through the slot.

64. The system of claim 60 wherein the stand-off joint provides a substantially rigid interconnect between the frame of the aerial vehicle and the tether segment.

65. The system of claim 60 wherein the stand-off joint provides a semi-rigid interconnect between the frame of the aerial vehicle and the tether segment.

66. The system of claim 60 wherein the stand-off joint is coupled to the frame of the aerial vehicle by a universal joint.

67. The system of claim 66 wherein the universal joint is formed by a pair of pivot joints, each pivot joint defining an axis, wherein the axes of the pivot joints are substantially orthogonal.

68. The system of claim 66 wherein the universal joint is formed by a pair of eyebolts.

69. The system of claim 66 wherein the universal joint includes a tube formed of a composite material, and further including a bushing mounted for rotational motion around the tube.

70. An aerial vehicle system comprising:

an aerial vehicle including a plurality of spaced-apart rotors, the rotors configured to spin about a substantially vertical axis during flight of the aerial vehicle, the aerial vehicle further including a frame;

a stand-off joint coupled to the frame of the aerial vehicle, the stand-off joint defining a proximal end adjacent the frame and a distal end; and

a payload coupled to the stand-off joint adjacent the distal end.

71. The system of claim 70 further comprising a tether segment and a ground station, the tether segment coupled between the ground station and the stand-off joint.

72. The system of claim 70 wherein the payload includes a camera.

73. A system for maneuvering a payload in an air space constrained by one or more obstacles, the system comprising:

an aerial vehicle defining an airframe and configured to carry the payload, the aerial vehicle defining a plurality of flight characteristics and having a processor for handling data about the flight characteristics of the aerial vehicle;

a sensor system carried by the aerial vehicle, the sensor system coupled to the processor in the aerial vehicle, the sensor system configured to gather data about obstacles in the air space and to provide the data to the processor in the aerial vehicle, and wherein the processor in the aerial vehicle calculates a cost function based on the flight characteristics of the aerial vehicle and the obstacles in the air space;

a ground station having a flight control processor;

a tether coupling the ground station to the aerial vehicle,

and wherein the aerial vehicle communicates with the ground station, the processor in the aerial vehicle providing the cost function to the flight control processor in the ground station and further wherein the flight control processor is configured to optimize the cost function for control of the aerial vehicle.

74. A system for maneuvering a payload in an air space constrained by one or more obstacles, the system comprising:

a first aerial vehicle defining a plurality of flight characteristics and having a processor for handling data about the flight characteristics of the first aerial vehicle;

a second aerial vehicle configured to carry the payload, the second aerial vehicle defining a plurality of flight characteristics and having a processor for handling data about the flight characteristics of the second aerial vehicle;

a ground station having a flight control processor configured to maintain a first dataset about obstacles in the air space and a second dataset about flight characteristics of the first and second aerial vehicles;

a first tether segment coupling the ground station to the first aerial vehicle;

a second tether segment coupling the second aerial vehicle to the first aerial vehicle;

a first sensor system carried by one of the first and second aerial vehicles, the sensor system coupled to the processor in the one of the first and second aerial vehicles that is carrying the first sensor system, the sensor configured to gather data about obstacles in the air space and to develop data about flight characteristics of at least one of the first and second aerial vehicles, the sensor system configured to provide the data to the processor to which the sensor system is coupled, and wherein the processor calculates a cost function based on the flight characteristics of the aerial vehicle and the obstacles in the air space and provides the cost function to the flight control processor in the ground station, and further wherein the flight control processor is configured to optimize the cost function for control of at least one of the aerial vehicles.