Suspended load stability systems and methods

• US 10,479,503 B2
• Filed: 01/15/2019
• Issued: 11/19/2019
• Est. Priority Date: 02/08/2018
• Status: Active Grant

• Current Assignee: Vita Inclinata IP Holdings LLC
• Original Assignee: Vita Inclinata Technologies, Inc.
• Inventors: Sikora, Derek, Carr, Caleb B., Goodrich, Logan
• Primary Examiner(s): Badawi, Medhat
• Application Number:
  US16/247,791
• Publication Number:
  US 20190241267A1
• Time in Patent Office: 308 Days
• CPC Class Codes: B64C 17/00 Aircraft stabilisation not otherwise provided for
• CPC Class Codes: B64D 1/08 the articles being load-carrying devices
• CPC Class Codes: B64D 1/22 Taking-up articles from earth's surface
• CPC Class Codes: B64D 9/00 Equipment for handling freight; Equipment for facilitating passenger embarkation or the like emergency equipment B64D17/00, B64D19/00, B64D25/00; structures integral with fuselage to facilitate loading, fuselage floors specially adapted for freight, steps mounted on and retractable within aircraft B64C; ground installations B64F
• CPC Class Codes: B66D 1/485 electrical
• CPC Class Codes: G05D 1/0858 specially adapted for vertical take-off of aircraft
• CPC Class Codes: G05D 1/10 Simultaneous control of position or course in three dimensions G05D1/12 takes precedence
• CPC Class Codes: H04W 4/026 using orientation information, e.g. compass

Abstract

Load stability systems and methods for stabilizing swinging motions of suspended loads. The load stability systems include a fully automated, self-powered device that employs thrust to counteract and control lateral and rotational motion of an external load. The device is a temporary installment on the load, cable, or boom, and is agnostic to the platform from which it is suspended.

Claims

1. A load stability system apparatus for stabilizing a load suspended via a cable from above, the apparatus comprising:

a center module comprising;

an attachment point for the cable, configured to allow rotation of the cable relative to the apparatus such that a twist or rotational motion of the cable is decoupled from an orientation of the apparatus and the apparatus in operation is orientable to any direction around an upright axis between the cable and the load;

an attachment point for the load, configured to suspend the load in operation below the load stability system apparatus;

a tensile structural element along the upright axis between the attachment point for the cable and the attachment point for the load,

wherein an upper surface of the tensile structural element is coupled to the attachment point for the cable and a lower surface of the tensile structural element is coupled to the attachment point for the load; and

a thruster mounting structure connected to the tensile structural element, configured to mount an even number of thrusters to the center module in a fixed position,

wherein the fixed position comprises pairs of thrusters arranged on opposite sides of the center module across the upright axis, aligned in parallel and facing a common direction;

a power supply;

a sensor array comprising;

an inertial measurement system;

an orientation measurement system; and

an absolute position measurement system;

a wireless transceiver;

a thruster controller;

two or more thrusters connected to the thruster mounting structure and controlled by the thruster controller; and

a processor operably connected to the sensor array, the wireless transceiver, and the thruster controller;

wherein the processor is configured to;

determine a motion of the load, the motion including any of a pendulum awing, a conical pendulum swing, and a twisting or rotational motion, based on the sensor array measurement systems;

orient the apparatus to a thrust application vector, by controlling thrust provided by the at least one of the thrusters in the pairs of thrusters mounted on opposite sides of the center module, such that the common direction that at least one of the pairs of thrusters faces coincides with the thrust application vector; and

apply thrust along the thrust application vector to autonomously counteract the motion of the load, by controlling at least the pair of thrusters aligned with the thrust application vector.

2. The load stability system apparatus of claim 1, wherein the two or more thrusters comprise unidirectional or bidirectional ducted fans.

3. The load stability system apparatus of claim 1, further comprising a thruster mount mechanism wherein the two or more thrusters are toollessly detachable from the center module.

4. The load stability system apparatus of claim 1, wherein the attachment point for the cable comprises one or more of a hoist ring or a hook.

5. The load stability system apparatus of claim 1, wherein the power supply comprises one or more batteries.

6. The load stability system apparatus of claim 5, further comprising a charging station configured to electrically connect to the apparatus to charge the one or more batteries and to physically receive and secure the apparatus.

7. The load stability system apparatus of claim 1, wherein the power supply comprises a wired power connection.

8. The load stability system apparatus of claim 1, further comprising a housing around the center module.

9. The load stability system apparatus of claim 1, wherein the sensor array inertial measurement system comprises at least one accelerometer or gyroscope, the sensor array orientation measurement system comprises at least one magnetometer or compass, and the sensor array absolute position measurement system comprises a Global Positioning System (GPS) sensor.

10. The load stability system apparatus of claim 1, wherein the sensor array further comprises at least one of a proximity sensor or light detection and ranging (LIDAR) system, an infrared (IR) or optical sensor, a gravitational sensor, a strain sensor, a rotational encoder or thruster speed sensor, or a shutdown pin presence sensor.

11. The load stability system apparatus of claim 1, further comprising a remote positional unit external to the apparatus, located at a position that is fixed relative to the location from which the cable is suspended or a target location, wherein the remote positional unit includes a positional transceiver configured to communicate with the wireless transceiver and provide a positional reference to the apparatus.

12. The load stability system apparatus of claim 1, further comprising external status indicator lights configured to indicate one or more of a position of the apparatus, an orientation of the apparatus, a distance from obstacles, a height above ground, a signal quality of the wireless transceiver, a mode or command state of the processor, an inertial behavior of the load, an energy capacity or available power of the power supply, a work load or power consumption of the two or more thrusters, the thrust from each thruster, a motion or direction of thrust of the apparatus, and a recommended direction for an operator to maneuver a platform suspending the load.

13. The load stability system apparatus of claim 1, further comprising a user-operable button or switch on the apparatus to initialize or shut down the apparatus and an emergency shutdown mechanism comprising a removable pin.

14. The load stability system apparatus of claim 1, further comprising a remote interactive display comprising a display processor, a screen, an input device, and a display transceiver configured to communicate with the wireless transceiver, wherein the remote interactive display is configured to:

receive data wirelessly from the load stability system apparatus via the display transceiver;

display, via the screen, indicators of one or more of a position of the apparatus, an orientation of the apparatus, a distance from obstacles, a height above ground, a signal quality of the wireless transceiver, a mode or command state of the processor, an inertial behavior of the load, an energy capacity or available power of the power supply, a work load or power consumption of the two or more thrusters, the thrust from each thruster, a motion or direction of thrust of the apparatus, and a recommended direction for an operator to maneuver a platform suspending the load; and

provide user control, via the input device, to set one or more of the mode or command state of the processor, a target position for the apparatus, and activation of an emergency shut off.

15. The load stability system apparatus of claim 1, wherein the apparatus comprises a self-contained, self-powered, closed-loop stabilization system that continuously counteracts a pendulum-like swing of the suspended load.

16. A method, performed by an autonomous load stability system apparatus suspended by a cable, to counteract a swinging of a load suspended below the load stability system apparatus,

wherein the load stability system apparatus includes a center module (comprising an attachment point for the cable, configured to allow rotation of the cable relative to the apparatus such that a twist or rotational motion of the cable is decoupled from an orientation of the apparatus and the apparatus in operation is orientable to any direction around an upright axis between the cable and the load, an attachment point for the load, configured to suspend the load in operation below the load stability system apparatus, a tensile structural element along the upright axis between the attachment point for the cable and the attachment point for the load, wherein an upper surface of the tensile structural element is coupled to the attachment point for the cable and a lower surface of the tensile structural element is coupled to the attachment point for the load, and a thruster mounting structure connected to the tensile structural element, configured to mount an even number of thrusters to the center module in a fixed position, wherein the fixed position comprises pairs of thrusters arranged on opposite sides of the center module across the upright axis, aligned in parallel and facing a common direction), a power supply, a sensor array (comprising an inertial measurement system, an orientation measurement system;

and an absolute position measurement system), a wireless transceiver, a thruster controller, a processor (operably connected to the sensor array, the wireless transceiver, and the thruster controller), and two or more thrusters connected to the thruster mounting structure and controlled by the thruster controller,

the method comprising;

receiving an activation signal;

obtaining, by the sensor array, information describing the position, orientation, and movement of the load stability system apparatus;

identifying a target location of the load stability system apparatus;

determining, by the processor, a thrust application vector to move the load stability system apparatus to the identified target location, based on the obtained information describing the position, orientation, and movement of the load stability system apparatus;

rotating the load stability system apparatus by controlling thrust from at least one of the two or more thrusters to align the common direction that at least one of the pairs of thrusters faces with the thrust application vector; and

applying thrust, by at least the pair of thrusters aligned with the thrust application vector, to counteract the swinging of the load.

17. The method of claim 16, wherein the obtaining, identifying, determining, rotating, and applying thrust are performed continuously.

18. The method of claim 16, wherein the identifying a target location of the load stability system apparatus is based on a mode or command state, and receiving the activation signal comprises receiving, by the wireless transceiver, a user selection of the mode or command state comprising one of:

maintaining a position relative to a fixed or moving point from which the cable is suspended;

holding a current position;

moving to a designated coordinate location or a point above the designated coordinate location; and

following an external target not connected to the suspended load.

19. The method of claim 18, further comprising displaying, on one or more external status indicator lights on the load stability system apparatus or on a remote interactive display in wireless communication with the wireless transceiver, an indication of the current mode or command state of the load stability system apparatus.

20. The method of claim 16, wherein the two or more thrusters are mounted in a fixed orientation relative to the load stability system apparatus, and wherein the rotating at least one of the two or more thrusters to align with the thrust application vector comprises rotating the load stability system apparatus.

21. The method of claim 16, wherein determining, by the processor, a thrust application vector to move the load stability system apparatus to the identified target location, based on the obtained information describing the position, orientation, and movement of the load stability system apparatus comprises using a non-linear state estimator to project near-term future motion of the load stability system apparatus and calculating a dynamic thrust response to the projected near-term future motion of the load stability system apparatus.

22. The method of claim 16, further comprising:

obtaining, by the sensor array, information describing an obstacle in a path of projected or potential movement of the load stability system apparatus; and

wherein determining, by the processor, a thrust application vector to move the load stability system apparatus to the identified target location, based on the obtained information describing the position, orientation, and movement of the load stability system apparatus comprises determining an adjusted vector to steer the load stability system apparatus and the load clear of the obstacle.

23. The method of claim 16, wherein the obtaining, identifying, determining, rotating, and applying thrust cause the load stability system apparatus to autonomously counteract the swinging of the load including any of a pendulum swing, a conical pendulum swing, and a twisting or rotational motion.

24. The method of claim 16, wherein the load stability system apparatus is agnostic of a platform from which the cable is suspended, such that the load stability system apparatus does not control the platform from which the cable is suspended.

25. An autonomous load stability system apparatus that is suspended by a cable, the load stability system apparatus comprising a non-transitory computer-readable storage medium having stored thereon instructions that, when executed by a processor in the load stability system apparatus, configure the processor to control the load stability system apparatus to counteract a swinging of a load suspended below the load stability system apparatus,

wherein the load stability system apparatus includes a center module (comprising an attachment point for the cable, configured to allow rotation of the cable relative to the apparatus such that a twist or rotational motion of the cable is decoupled from an orientation of the apparatus and the apparatus in operation is orientable to any direction around an upright axis between the cable and the load, an attachment point for the load, configured to suspend the load in operation below the load stability system apparatus, a tensile structural element along the upright axis between the attachment point for the cable and the attachment point for the load, wherein an upper surface of the tensile structural element is coupled to the attachment point for the cable and a lower surface of the tensile structural element is coupled to the attachment point for the load, and a thruster mounting structure connected to the tensile structural element, configured to mount an even number of thrusters to the center module in a fixed position, wherein the fixed position comprises pairs of thrusters arranged on opposite sides of the center module across the upright axis, aligned in parallel and facing a common direction), a power supply, a sensor array (comprising an inertial measurement system, an orientation measurement system;

and an absolute position measurement system), a wireless transceiver, a thruster controller, the processor (operably connected to the sensor array, the wireless transceiver, and the thruster controller), and two or more thrusters connected to the thruster mounting structure and controlled by the thruster controller,

wherein the instructions comprise;

receiving an activation signal, wherein the activation signal includes a user selection of a mode or command state comprising one of;

maintaining a position relative to a fixed or moving point from which the cable is suspended;

holding a current position;

moving to a designated coordinate location or a point above the designated coordinate location; and

following an external target not connected to the suspended load;

obtaining, by the sensor array, information describing the position, orientation, and movement of the load stability system apparatus;

identifying a target location of the load stability system apparatus, based on the mode or command state;

determining, by the processor, a thrust application vector to move the load stability system apparatus to the identified target location, based on the obtained information describing the position, orientation, and movement of the load stability system apparatus;

rotating the load stability system apparatus by controlling thrust from at least one of the two or more thrusters to align the common direction that the at least one of the pairs of thrusters faces with the thrust application vector; and

applying thrust, by at least the pair of thrusters aligned with the thrust application vector, to counteract the swinging of the load.

26. The autonomous load stability system apparatus of claim 25, wherein the obtaining, identifying, determining, rotating, and applying thrust cause the load stability system apparatus to autonomously counteract the swinging of the load including any of a pendulum swing, a conical pendulum swing, and a twisting or rotational motion.

27. A method of counteracting a motion of a suspended load, the method comprising:

attaching a load stability system apparatus to a cable for suspending the load, wherein the load stability system apparatus includes a center module (comprising an attachment point for the cable, configured to allow rotation of the cable relative to the apparatus such that a twist or rotational motion of the cable is decoupled from an orientation of the apparatus and the apparatus in operation is orientable to any direction around an upright axis between the cable and the load, an attachment point for the load, configured to suspend the load in operation below the load stability system apparatus, a tensile structural element along the upright axis between the attachment point for the cable and the attachment point for the load, wherein an upper surface of the tensile structural element is coupled to the attachment point for the cable and a lower surface of the tensile structural element is coupled to the attachment point for the load, and a thruster mounting structure connected to the tensile structural element, configured to mount an even number of thrusters to the center module in a fixed position, wherein the fixed position comprises pairs of thrusters arranged on opposite sides of the center module across the upright axis, aligned in parallel and facing a common direction), a power supply, a sensor array (comprising an inertial measurement system, an orientation measurement system; and

an absolute position measurement system), a wireless transceiver, a thruster controller, a processor (operably connected to the sensor array, the wireless transceiver, and the thruster controller), and two or more thrusters connected to the thruster mounting structure and controlled by the thruster controller, wherein the processor is configured to;

determine a motion of the load, the motion including any of a pendulum swing, a conical pendulum swing, and a twisting or rotational motion, based on the sensor array measurement systems;

orient the apparatus to a thrust application vector, by controlling thrust provided by the at least one of the thrusters in the pairs of thrusters mounted on opposite sides of the center module, such that the common direction that at least one of the pairs of thrusters faces coincides with the thrust application vector; and

apply thrust along the thrust application vector to autonomously counteract the motion of the load, by controlling at least the pair of thrusters aligned with the thrust application vector,

activating a mode or command state of the load stability system apparatus comprising one of;

maintaining a position relative to a fixed or moving point from which the cable is suspended;

holding a current position;

moving to a designated coordinate location or a point above the designated coordinate location; and

following an external target not connected to the suspended load; and

causing a motion of the suspended load inconsistent with the activated mode or command state of the load stability system apparatus,

such that the thrust applied by the load stability system apparatus along the thrust application vector autonomously counteracts the motion of the suspended load.

28. The method of claim 27, wherein the load stability system apparatus autonomously:

obtains, by the sensor array, information describing the position, orientation, and movement of the load stability system apparatus;

identifies a target location of the load stability system apparatus, based on the mode or command state;

determines, by the processor, the thrust application vector to move the load stability system apparatus to the identified target location, based on the obtained information describing the position, orientation, and movement of the load stability system apparatus;

rotates the load stability system apparatus by controlling thrust from at least one of the two or more thrusters to align the common direction that at least one of the pairs of thrusters faces with the thrust application vector; and

applies thrust, by at least the pair of thrusters aligned with the thrust application vector, to counteract the swinging of the load.