Stabilized UAV recovery system

• US 8,172,177 B2
• Filed: 06/01/2009
• Issued: 05/08/2012
• Est. Priority Date: 06/02/2008
• Status: Active Grant

• Current Assignee: Advanced Technology & Research Corp., David Lupi-Atr
• Original Assignee: Advanced Technology & Research Corp.
• Inventors: Hui, Eric Chi-Kai, Umbreit, Merrill Keith, Lovell, Gibert H.
• Primary Examiner(s): Swiatek, Rob
• Assistant Examiner(s): Xavier, Valentina
• Application Number:
  US12/455,323
• Publication Number:
  US 20090294584A1
• Time in Patent Office: 1,072 Days
• Field of Search: 244/110.C, 244/110.E, 244/110.F, 244/115, 244/63, 244/135.A
• US Class Current: 244/110.F
• CPC Class Codes: B63B 27/10 of cranes
• CPC Class Codes: B64C 39/024 of the remote controlled vehicle type, i.e. RPV
• CPC Class Codes: B64U 10/25 Fixed-wing aircraft VTOL aircraft B64U10/20
• 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 70/93 for use on a land or nautical vehicle
• CPC Class Codes: B64U 80/84 Waterborne vehicles

Abstract

A stabilized UAV recovery system is disclosed. In the illustrative embodiment for UAV recovery over water, the system includes ship-based elements and UAV-based elements. The ship-based elements include a robot arm that holds a capture mechanism over the side of the ship while compensating for wave-induced ship motion. The UAV-based elements include a hook mounted to the top of the UAV fuselage. With the capture mechanism held stable from the perspective of a UAV approaching from behind or in front of the mechanism, the UAV is flown under it, snagging an arresting line with the hook. With continued forward motion of the UAV, the arresting line pulls out of a winch drum that is coupled to a brake, bringing the UAV to rest.

Claims

1. An apparatus for airborne capture of an unmanned aerial vehicle (UAV) on a ship, the apparatus comprising the following:

a UAV capture mechanism with two attached posts between which a horizontally disposed portion of arresting line is held prior to UAV capture;

a robot arm wherein a free end of the robot arm is attached to the said capture mechanism and the base of the robot arm is mounted to the ship and wherein said robot is capable of compensating for wave-induced ship motion, thereby holding said capture mechanism stable for approaching UAV; and

an arresting hook mounted to said UAV that snags said horizontally disposed portion of arresting line when said UAV reaches said capture mechanism;

wherein the capture mechanism comprises the following;

a fixed length loop of arresting line that includes the horizontally disposed portion of arresting line;

an open length of arresting line, one end of which is attached to the said loop;

a rotating winch drum about which said open length of arresting line is wrapped;

a brake that can apply a resistive torque to said winch drum;

a motor that can rotate said winch drum; and

attachments at the ends of the posts that hold the said loop prior to UAV capture and allow said loop to be pulled free from said posts by an arresting hook of an approaching UAV.

2. The apparatus of claim 1 wherein the robot arm has a serial kinematic structure with four actuated revolute joints wherein the robot base is attached to the deck of ship;

the axis of the first joint, which couples the base to the first moving link, is perpendicular to the deck; and

the axes of the second, third, and fourth joints are parallel to each other and perpendicular to the axis of the first joint.

3. The apparatus of claim 1 further comprising the following two sensing devices:

a UAV sensing device that provides a real-time estimate of the position of the UAV relative to the capture mechanism and a ship motion sensing device that provides a real-time estimate of the ship position in an inertial reference frame.

4. The apparatus of claim 3 further comprising a processor that receives the signals of said UAV sensing device and the signals of said ship motion sensor and that sends flight path commands to the UAV and that sends actuator commands to the actuators of the robot arm and capture mechanism.

5. The apparatus of claim 2 wherein the angle of the first revolute joint can be positioned such that the second joint axis is substantially parallel to expected flight path direction just prior to capture.

10. The apparatus of claim 1 used on a ground vehicle or stationary ground site rather than a ship.

6. A method for airborne capture of a UAV comprising the following:

directing the UAV, which has an attached arresting hook, to a horizontally disposed portion of arresting line held by attachment devices at the ends of two posts of the capture mechanism wherein said capture mechanism is held by a robot arm that compensates for ship wave-induced motion such that said capture mechanism is a stable target for said approaching UAV;

after said arresting hook makes contact with the said horizontally disposed portion of arresting line, coupling said arresting hook to said horizontally disposed portion of arresting line wherein said arresting line is first pulled free of said attachment devices by said arresting hook, is momentarily slack, and then becomes taut, snaring the hook;

pulling arresting line off of the winch drum as the UAV continues its forward motion while the rotary brake that is coupled to said winch drum provides braking torque to the said winch drum thus decelerating said UAV until it is at rest; and

suspending said UAV with the arresting line below the capture mechanism with said brake preventing rotation of said winch drum.

7. The method of claim 6 wherein, prior to UAV capture, the sensed ship motion is input to the processor and the processor calculates and outputs the proper commands to the actuators of the robot arm such that the capture mechanism is a stable target for the approaching UAV.

8. The method of claim 6 wherein, prior to UAV capture, the sensed UAV position is input to the processor and the processor calculates and outputs the proper commands to the capture mechanism revolute joint actuator such that the vertical height of the portion of the horizontally disposed arresting line between the posts of the capture mechanism matches the vertical height of the arresting hook in the final seconds before capture.

9. The method of claim 6 wherein, after UAV capture, the following operations are performed:

the brake that is coupled to the winch drum is disengaged, the motor that is coupled to the winch drum rotates said winch drum thus hoisting said UAV up to the capture mechanism, and the said brake is re-engaged;

the actuators of the robot arm are commanded to stop thus turning off ship motion compensation;

said robot arm then moves said UAV to a location on the deck of the ship.