UAV docking system and method

• US 9,561,871 B2
• Filed: 05/07/2014
• Issued: 02/07/2017
• Est. Priority Date: 05/07/2014
• Status: Active Grant

• Current Assignee: Deere & Company
• Original Assignee: Deere & Company
• Inventors: Sugumaran, Ramanathan
• Primary Examiner(s): Dinh, Tien
• Assistant Examiner(s): Fabula, Michael A
• Application Number:
  US14/272,125
• Publication Number:
  US 20160144982A1
• Time in Patent Office: 1,007 Days
• US Class Current: 1/1
• CPC Class Codes: A01D 41/12 Details of combines
• CPC Class Codes: B64C 25/32 characterised by elements which contact the ground or similar surface arrester hooks B64C25/68
• CPC Class Codes: B64C 25/34 wheeled type, e.g. multi-wheeled bogies
• CPC Class Codes: B64C 25/52 Skis or runners
• CPC Class Codes: B64C 39/024 of the remote controlled vehicle type, i.e. RPV
• CPC Class Codes: B64F 1/00 Ground or aircraft-carrier-deck installations specially adapted for captive aircraft B64F3/00
• CPC Class Codes: B64F 1/005 Protective coverings for aircraft not in use
• CPC Class Codes: B64F 1/12 for anchoring aircraft
• CPC Class Codes: B64F 1/36 Other airport installations ground installations for de-icing aircraft B64F5/20
• CPC Class Codes: B64U 10/13 Flying platforms
• CPC Class Codes: B64U 10/14 with four distinct rotor axes, e.g. quadcopters
• CPC Class Codes: B64U 30/20 Rotors; Rotor supports
• CPC Class Codes: B64U 30/21 Rotary wings
• CPC Class Codes: B64U 50/34 In-flight charging photovoltaics B64U50/31
• CPC Class Codes: B64U 70/00 Launching, take-off or landing arrangements
• CPC Class Codes: B64U 70/95 Means for guiding the landing UAV towards the platform, e.g. lighting means
• CPC Class Codes: B64U 80/86 Land vehicles

Abstract

An aerial vehicle docking system includes a landing pad and an aerial vehicle. The landing pad has a concave landing surface and a depression. The aerial vehicle has landing gear and a protrusion. The protrusion is shaped to mate with the depression. The protrusion and the landing gear are positioned on a bottom surface of the aerial vehicle.

Claims

1. An aerial vehicle docking system comprising:

a landing pad having;

a concave landing surface comprising;

a depression; and

an aerial vehicle having;

landing gear;

a protrusion; and

a shoulder comprising;

at least one wheel;

wherein the protrusion is shaped to mate with the depression when the aerial vehicle docks with the landing pad;

wherein the protrusion and landing gear are positioned on a bottom surface of the aerial vehicle;

wherein the shoulder extends outward beyond the perimeter of the protrusion and is positioned above at least a portion of the protrusion; and

wherein the shoulder rests upon the concave landing surface when the protrusion is mated with the depression.

2. The docking system of claim 1, further comprising a cover attached to the landing pad, the cover movable between a first position covering at least a portion of the aerial vehicle when the protrusion is mated with the depression and a second position not covering the aerial vehicle when the protrusion is mated with the depression.

3. The docking system of claim 2, wherein the cover comprises:

a frame,

a sheet, and

a pin, wherein the sheet is attached to the frame and the frame is rotatable about the pin from a first position wherein the sheet is not above the depression to a second position wherein the sheet is above the depression.

4. The docking system of claim 3, wherein the cover is a collapsible awning, the cover is collapsed in the first position, and the cover is uncollapsed in the second position.

5. The docking system of claim 1, wherein the landing gear is positioned on a bottom surface of the protrusion.

6. The docking system of claim 1, wherein the shoulder and the protrusion are elliptically shaped;

and wherein a diameter of the shoulder is greater than the diameter of the protrusion.

7. The docking system of claim 1, wherein the aerial vehicle is a rotary-wing aircraft.

8. The docking system of claim 1, further comprising:

a first magnet included in the aerial vehicle;

a second magnet included in the landing pad, at least a portion of the first magnet overlapping at least a portion of the second magnet when the protrusion is mated with the depression.

9. The docking system of claim 8, wherein the second magnet comprises an electromagnet configured to attract or repel the first magnet in a selectable manner.

10. The docking system of claim 8, wherein the second magnet comprises a permanent magnet configured to attract the first magnet.

11. The docking system of claim 1, further comprising:

a first induction coil included in the aerial vehicle;

a second induction coil included in the landing pad, the first induction coil inductively coupled to the second inductive coil when the protrusion is mated with the depression, and wherein the first induction coil and the second induction coil are configured to transmit power from the landing pad to the aerial vehicle.

12. The docking system of claim 1, further comprising at least one wheel attached to the landing pad and configured to provide rolling support to the landing pad as the landing pad is moved.

13. An aerial vehicle docking system comprising:

a vehicle having;

an operator station in the vehicle; and

a roof;

a landing pad attached to the roof having;

a concave landing surface comprising;

a depression; and

an aerial vehicle having;

landing gear;

a protrusion; and

a shoulder comprising;

at least one wheel;

wherein the protrusion is shaped to mate with the depression when the aerial vehicle docks with the landing pad;

wherein the protrusion and landing gear are positioned on a bottom surface of the aerial vehicle;

wherein the shoulder extends outward beyond the perimeter of the protrusion and is positioned above at least a portion of the protrusion; and

wherein the shoulder rests upon the concave landing surface when the protrusion is mated with the depression.

14. The docking system of claim 13, wherein the landing surface is integrally formed as part of the roof.

15. The docking system of claim 13, wherein the vehicle is an agricultural tractor, harvester, or sprayer.

16. An aerial vehicle docking system comprising:

a landing pad having;

a concave landing surface comprising;

a depression; and

an aerial vehicle having;

landing gear;

a protrusion; and

a shoulder comprising;

at least one skid surface;

wherein the protrusion is shaped to mate with the depression when the aerial vehicle docks with the landing pad;

wherein the protrusion and landing gear are positioned on a bottom surface of the aerial vehicle;

wherein the shoulder extends outward beyond the perimeter of the protrusion and is positioned above at least a portion of the protrusion; and

wherein the shoulder rests upon the concave landing surface when the protrusion is mated with the depression.

17. The docking system of claim 16, wherein the coefficient of friction between the at least one skid surface and the landing surface is less than 0.25.

18. The aerial vehicle docking system according to claim 16 wherein the at least one skid surface comprises one or more skidpads.

19. The docking system of claim 16, further comprising:

a cover attached to the landing pad, the cover movable between a first position covering at least a portion of the aerial vehicle when the protrusion is mated with the depression and a second position not covering the aerial vehicle when the protrusion is mated with the depression.

20. The docking system of claim 19, wherein the cover comprises:

a frame;

a sheet; and

a pin;

wherein the sheet is attached to the frame and the frame is rotatable about the pin from a first position wherein the sheet is not above the depression to a second position wherein the sheet is above the depression.

21. The docking system of claim 19, wherein the cover is a collapsible awning, the cover is collapsed in the first position, and the cover is uncollapsed in the second position.