Method of actively controlling winch swing via modulated uptake and release

• US 9,981,834 B2
• Filed: 07/28/2016
• Issued: 05/29/2018
• Est. Priority Date: 05/19/2014
• Status: Active Grant

• Current Assignee: Wing Aviation LLC (Alphabet Inc.)
• Original Assignee: X Development LLC (Alphabet Inc.)
• Inventors: Bialkowski, Joshua John, Roberts, John, Bachrach, Abraham
• Primary Examiner(s): Sanderson, Joseph W
• Application Number:
  US15/222,150
• Publication Number:
  US 20160332851A1
• Time in Patent Office: 670 Days
• CPC Class Codes: B64D 1/22 Taking-up articles from earth's surface
• 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 2101/67 the UAVs comprising tethers for lowering the goods
• 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 2201/20 Remote controls
• CPC Class Codes: B64U 50/38 by wireless transmission
• CPC Class Codes: B66C 13/06 for minimising or preventing longitudinal or transverse swinging of loads
• CPC Class Codes: B66D 1/485 electrical
• CPC Class Codes: G05D 1/0858 specially adapted for vertical take-off of aircraft

Abstract

An unmanned aerial vehicle (UAV) including a winch system, wherein the winch system includes a winch line having a first end that is secured to the payload, and wherein the winch system is controllable to vary the rate of descent of the payload, an inertial measurement unit positioned on the payload or on the first end of the winch line, wherein the inertial measurement unit is configured to measure oscillations of the payload, and a control system configured to (a) receive data from the IMU, (b) determine oscillations of the payload based on the data received from the IMU, and (c) operate the winch system to vary the deployment rate of the winch line so to damp oscillations of the payload.

Claims

1. A method of controlling the oscillations of a payload during descent from an unmanned aerial vehicle (UAV) comprising a winch system positioned on the aerial vehicle, the winch system including a winch line secured to the payload and to the winch system, an inertial measurement unit positioned on the payload or an end of the winch line, and a control system positioned on the UAV, comprising the steps of:

operating the control system to control the rate of descent of the payload in response to measurements received from the inertial measurement unit; and

operating the control system to unwind the winch line when the payload moves towards a bottom of a swing.

2. The method of claim 1, further including the step of operating the control system to stop or slow the rate at which the winch line is unwound when the payload moves from the bottom of the swing towards a top of the swing.

3. The method of claim 1, further including the step of operating the control system to wind the winch line in when the payload moves from a bottom of the swing towards a top of the swing.

4. The method of claim 1, further including the step of reversing the direction of winch line travel twice during a period of oscillation of the payload.

5. The method of claim 1, further including the step of determining an oscillation frequency of the line, and matching a switching frequency of the line to the oscillation frequency of the line, wherein the winch alternates between winding and unwinding the line at the switching frequency.

6. The method of claim 1, further comprising determining a phase of line oscillation, and matching a switching phase of the line to the phase of line oscillation.

7. The method of claim 1, wherein the inertial measurement unit is configured to determine a period of oscillation of the payload during the descent of the payload;

and further including the step of winding in the winch line at a first pair of separate points during the period of oscillation of the payload, and the step of unwinding the winch line at a second pair of separate points during the period of oscillation of the payload.

8. The method of claim 1, further including the step of operating the control system to unwind the winch line when the inertial measurement unit moves towards the bottom of the swing.

9. The method of claim 1, further including the step of operating the control system to reduce or stop the rate the winch line is wound in when the inertial measurement unit moves towards the bottom of the swing.

10. The method of claim 1, further including the step of translating the position of the UAV in response to measurements received from the inertial measurement unit.

11. A method of controlling the oscillations of a payload during ascent to an unmanned aerial vehicle (UAV) comprising a winch system positioned on the aerial vehicle, the winch system including a winch line secured to the payload and to the winch system, an inertial measurement unit positioned on the payload or an end of the winch line, and a control system positioned on the UAV, comprising the steps of:

operating the control system to control the rate of ascent of the payload in response to measurements received from the inertial measurement unit; and

operating the control system to wind in the winch line when the payload moves from a bottom of a swing toward a top of the swing;

wherein the winch system is controllable to vary the rate of ascent of the payload; and

the control system configured to control oscillations of the payload during ascent by operating the winch system to control the rate of ascent of the payload in response to measurements received from the inertial measurement unit.

12. The method of claim 11, wherein the control system is further configured to control oscillations of the payload during ascent by unwinding the winch line when the payload moves towards the bottom of the swing.

13. The method of claim 11, wherein the control system is further configured to control oscillations of the payload during ascent by reducing or stopping the rate the winch line is wound in when the payload moves towards the bottom of the swing.

14. The method of claim 11, wherein the inertial measurement unit is configured to determine a period of oscillation of the inertial measurement unit during ascent of the inertial measurement unit.

15. The method of claim 11, wherein the control system is configured to wind in the winch line at a first rate at a first pair of separate points during a period of oscillation of the inertial measurement unit, and wind in the winch line at a second lower rate at a second pair of separate points during the period of oscillation of the inertial measurement unit.

16. The method of claim 11, wherein the control system is configured to wind in the winch line at a rate proportional to a velocity of the payload as the payload moves from a bottom of a swing towards the top of the swing.

17. The method of claim 11, wherein the control system is configured to unwind the winch line at two separate points during a period of oscillation of the inertial measurement unit.

18. The method of claim 11, wherein the control system is further configured to control oscillations of the payload by translating the position of the UAV in response to measurements received from the inertial measurement unit.

19. The method of claim 11, wherein the control system is configured to reverse the direction of winch line travel twice during a period of oscillation of the payload.