Unmanned aertial vehicle with rotatable net assembly

1. A drone comprising:

a drone chassis extending along a plane;

a plurality of motors attached to the drone chassis;

a plurality of propellers coupled to the plurality of motors; and

a net assembly mounted to the drone chassis, the net assembly including:

a net enclosure that is mounted laterally with respect to the drone chassis and is rotatably mounted such that an outward facing opening of the enclosure is rotatable about an axis of rotation that is parallel to the plane of the drone chassis.

2. The drone of claim 1 further comprising a rotation mechanism configured to rotate the net enclosure with respect to the plane of the drone chassis.

3. The drone of claim 2 wherein the rotation mechanism includes:

a rod extending between arms of the drone chassis, the rod is statically attached to the net enclosure and rotatably attached to the drone chassis; and

a motor coupled to the rod to control rotation of the rod and net enclosure with respect to the drone chassis.

4. The drone of claim 3 wherein the motor is mounted in a central portion of the drone chassis and is coupled to the rod by a belt extending about a wheel that is attached to and concentric with the rod.

5. The drone of claim 1 wherein the enclosure is mounted such that the plane of the drone chassis extends through the enclosure.

6. The drone of claim 1 wherein the outward facing opening of the enclosure is oriented along a primary direction of travel of the drone.

7. The drone of claim 1 wherein the enclosure includes:

a central portion that extends parallel to the axis of rotation between a first end and a second end and is substantially crescent shaped in cross section along a plane perpendicular to the axis of rotation; and

first and second wing portions that extend outward from the first end and the second end of the central portion at an oblique angle to the central portion.

8. The drone of claim 7 wherein the central portion and the first and second wing portions include a frame and enclosure netting attached to the frame.

9. The drone of claim 8 wherein the net assembly further comprises an entanglement net attached to the first and second wing portions, the entanglement net extending across the outward facing opening.

10. The drone of claim 8 wherein the enclosure netting is formed of strands of monofilament nylon having a first spacing and first tension and the entanglement net is formed of strands of monofilament nylon having a second spacing that is greater than the first spacing and second tension that is less than the first tension.

11. A method of intercepting a target drone with a counter-unmanned aerial vehicle (C-UAV) drone comprising:

piloting the C-UAV drone with a net assembly towards the target drone, the net assembly having an opening along a primary direction of travel of the C-UAV;

rotating the net assembly with respect to the C-UAV drone to align the net assembly with the target drone while the C-UAV is flying towards the target drone; and

intercepting the target drone with the net assembly by aligning the opening with the target drone while the C-UAV is flying such that the target drone enters the opening.

12. The method of claim 11 wherein, when the C-UAV is flying towards the target drone it has negative pitch and rotating the net assembly at least partially counteracts the negative pitch of the C-UAV.

13. The method of claim 11 wherein the net assembly further includes an entanglement net extending across the opening and intercepting the target drone includes entangling the target drone in the entanglement net.

14. The method of claim 11 wherein the C-UAV includes a chassis extending along a plane and rotating the net assembly with respect to the C-UAV includes using a motor attached to the chassis to rotate the net assembly about an axis of rotation that extends parallel to the plane.

15. The method of claim 11 further comprising:

detecting interception of the target drone by one or more of a strain gauge, a camera, or an optical sensor;

determining information regarding the target drone from signals from the one or more of a strain gauge, a camera, or an optical sensor; and

modifying flying parameters of the C-UAV drone according to the information regarding the target drone.

16. A Counter-Unmanned Aerial Vehicle (C-UAV) quadcopter comprising:

a quadcopter chassis extending along a plane, the quadcopter chassis having a first arm, a second arm, a third arm, and a fourth arm forming an X-shape in cross section along the plane;

a first motor, a second motor, a third motor, and a fourth motor respectively attached to the first, second, third, and fourth arms of the quadcopter chassis;

a first propeller, a second propeller, a third propeller, and a fourth propeller coupled to the respective first, second, third, and fourth motors;

a net assembly rotatably attached to ends of the first and second arms of the quadcopter chassis; and

a motor attached to the quadcopter chassis, the motor coupled to the net assembly to rotate the net assembly with respect to the plane of the quadcopter chassis.

17. The C-UAV quadcopter of claim 16 wherein the net assembly includes:

a central portion that extends parallel to an axis of rotation of the net assembly between a first end and a second end and is substantially crescent shaped in cross section along a plane perpendicular to the axis of rotation;

first and second wing portions that extend outward from the first and second ends of the central portion at an oblique angle to the central portion; and

an entanglement net attached to the first and second wing portions, the entanglement net extending parallel to the central portion and in front of the central portion along a primary direction of travel of the C-UAV.

18. The C-UAV quadcopter of claim 16 further comprising:

one or more strain gauges or optical sensors attached to components of the net assembly to detect presence of a target drone in the net assembly;

one or more cameras mounted to the net assembly for First Person View (FPV) operation of the C-UAV for intercepting the target drone; and

control circuits configured to receive outputs of the one or more strain gauges or optical sensors and outputs of the one or more cameras and to adjust flying parameters of the C-UAV quadcopter in response to the outputs.

19. The C-UAV quadcopter of claim 18 wherein the control circuits are further configured to determine pitch of the C-UAV and control the motor to rotate the net assembly to counteract the pitch such that the net assembly is substantially aligned for interception of a target drone.