AUTONOMOUS DOCKING SYSTEM FOR AN UNMANNED AERIAL VEHICLE

Abstract

There is disclosed an autonomous docking system for aerial delivery of a payload from a ground station. The system may comprise an unmanned aerial vehicle (UAV) having one or more motors for powered flight and a pyramidal bottom surface opening downward to terminate in a base perimeter. A cargo pod may be included to carry the payload and may have a pyramidal top surface complementary to the pyramidal bottom surface of the UAV. The system may further include a latching system for locking the UAV to the cargo pod and one or more steering components for approaching the cargo to within a steering accuracy. The UAV may be configured to dock by steering downward until the base perimeter slidably contacts the pyramidal top surface of the cargo pod for gravity-aligning the UAV in azimuth and laterally. The system may be further defined by a capture radius of the base perimeter being greater than a lateral component of the steering accuracy.

Claims

1. An autonomous docking system for unmanned aerial delivery of a payload from a ground station, the docking system comprising: an unmanned aerial vehicle (UAV) having one or more motors for powered flight and a pyramidal bottom surface opening downward to terminate in a base perimeter; a cargo pod configured to carry the payload and having a pyramidal top surface complementary to the pyramidal bottom surface of the UAV; a latching system for locking the UAV to the cargo pod when docked; one or more steering components disposable on the UAV for approaching the cargo pod at the ground station to within a steering accuracy; and where the UAV is configured to dock by steering downward until the base perimeter slidably contacts the pyramidal top surface of the cargo pod for gravity-aligning the UAV in azimuth and laterally, where a capture radius of the base perimeter is greater than a lateral component of the steering accuracy.

2. The docking system of claim 1, wherein: the latching system comprises one or more of electro-mechanical or magnetic latches on the UAV and complementary latch receptacles on the cargo pod.

3. The docking system of claim 2, wherein: each latch receptacle is a hard pin mounted to a side of the cargo pod.

4. The docking system of claim 2, wherein: the latches are electro-permanent magnetic (EPM) devices switchable in polarity by a temporary current.

5. The docking system of claim 1, wherein: the steering components are one or more of LIDAR, GPS, infrared, inertial, and photographic components.

6. The docking system of claim 1, wherein: the bottom and the top pyramidal surfaces each have 4 sides and the steering accuracy includes an azimuthal component of less than 45 degrees of error.

7. The docking system of claim 1, further comprising: a mating rack attachable to the UAV for providing the pyramidal bottom surface.

8. The docking system of claim 7, wherein: the rack is disposed with one or more electro-mechanical or magnetic latches of the latching system.

9. The docking system of claim 1, further comprising: a main battery on the UAV for powering the one or more motors, an auxiliary battery on the cargo pod, and one or more power transfer contacts on the pyramidal top surface for sending power from the auxiliary battery to the UAV while docked.

10. The docking system of claim 1, further comprising: a docking sensor to indicate correct alignment and mating with the pod, the sensor configurable to enable the latching system.

11. The docking system of claim 1, further comprising: a cargo bay inside the cargo pod for housing the payload.

12. The docking system of claim 11, further comprising: an access door on the cargo pod for locking the cargo bay and discouraging

13. The docking system of claim 1, wherein: the cargo pod includes a pod bottom surface conforming to the pyramidal bottom surface of the UAV, and including another latching system, the pod bottom surface and the additional latching system for capturing the ground station, the ground station having a pyramidal top surface for gravity-aligning to the cargo pod.

14. The docking system of claim 13, wherein: the ground station is one or more of another cargo pod, a parking location for customer delivery, and a docking station for powering or recharging the UAV.

15. An autonomous docking system for securely storing a payload deliverable by an unmanned aerial vehicle (UAV) having a battery for powered flight, the docking system comprising: a cargo pod for carrying the payload and hoistable by the UAV, the cargo pod having a pyramidal bottom surface opening downward to terminate in a base perimeter; a docking station securable to a ground location and having a pyramidal top surface complementary to the pyramidal bottom surface of the cargo pod; a latching system for locking the cargo pod to the docking station; one or more steering components on the UAV for approaching the docking station to within a steering accuracy; and where the hoisted cargo pod is configured to dock by steering the UAV downward until the base perimeter of the cargo pod slidably contacts the pyramidal top surface of the docking station for gravity-aligning the cargo pod in azimuth and laterally, where a capture radius of the base perimeter is greater than a lateral component of the steering accuracy.

16. The docking system of claim 15, further comprising: configuring the docking station with electrical power and configuring the docking system with a power transfer means for routing the electrical power to the cargo pod for powering the UAV or recharge the battery.

17. The docking system of claim 16, wherein: the electrical power is one or more of an auxiliary battery of the docking station and a land-based electrical grid, and wherein the power transfer means includes one or more power transfer contacts on the pyramidal top surface of the docking station.

18. The docking system of claim 15, wherein: the docking station is another cargo pod for stacking and locking two cargo pads to the ground location.

19. The docking system of claim 15, wherein: the latching system comprises one or more of electro-mechanical or electro-permanent magnetic (EPM) devices disposed on the cargo pod and complementary latch receptacles disposed on the docking station.

20. The docking system of claim 15, wherein: the bottom and the top pyramidal surfaces each have 4 sides and the steering accuracy includes an azimuthal component of less than 45 degrees of error.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0010] Non-limiting and non-exhaustive embodiments of the present invention, including the preferred embodiment, are described with reference to the following figures, wherein like reference numerals refer to like parts throughout the various views unless otherwise specified. Illustrative embodiments of the invention are illustrated in the drawings, in which:

[0011] FIG. 1 illustrates a perspective view of mating components for an autonomous docking system for an unmanned aerial vehicle, in accordance with an embodiment of the present disclosure.

[0012] FIG. 2 illustrates a perspective view of the mated components for an autonomous docking system for an unmanned aerial vehicle, in accordance with an embodiment of the present disclosure.

[0013] FIG. 3 illustrates a side view of a UAV with the mated components for an autonomous docking system for an unmanned aerial vehicle, in accordance with an embodiment of the present disclosure.

[0014] FIG. 4 illustrates a cutaway view of a cargo pod for an autonomous docking system for an unmanned aerial vehicle, in accordance with an embodiment of the present disclosure.

[0015] FIG. 5 illustrates a perspective view of a pyramidal top surface of the cargo pod for an autonomous docking system for an unmanned aerial vehicle, in accordance with an embodiment of the present disclosure.

[0016] FIG. 6 illustrates a top view of the cargo pod for an autonomous docking system for an unmanned aerial vehicle, in accordance with an embodiment of the present disclosure.

[0017] FIG. 7 illustrates a perspective view of internal components of the cargo pod for an autonomous docking system for an unmanned aerial vehicle, in accordance with an embodiment of the present disclosure.

[0018] FIG. 8 illustrates a cutaway view of two stacked cargo pods for an autonomous docking system for an unmanned aerial vehicle, in accordance with an embodiment of the present disclosure.

DETAILED DESCRIPTION

[0019] Embodiments are described more fully below in sufficient detail to enable those skilled in the art to practice the system and method. However, embodiments may be implemented in many different forms and should not be construed as being limited to the embodiments set forth herein. The following detailed description is, therefore, not to be taken in a limiting sense.

[0020] When elements are referred to as being “connected” or “coupled,” the elements can be directly connected or coupled together or one or more intervening elements may also be present. In contrast, when elements are referred to as being “directly connected” or “directly coupled,” there are no intervening elements present.

[0021] As may be appreciated, based on the disclosure, there exists a need in the art for an aerial delivery system whose aerial vehicles can autonomously align with and capture a package within a service area of the delivery system. Additionally, there exists a need in the art for powering or refueling the vehicle in the field (service area). Further, there exists a need in the art for locking the package to a secure ground location in order to prevent theft of the package. Also, there exists a need in the art to maximally utilize the available fuel during the return flight so as to minimize the number of flights required each day. Finally, there exists a need in the art for adapting multiple non-standard vehicle designs to a standardized docking system.

[0022] Referring to FIGS. 1-8, in an embodiment, an autonomous docking system 10 is described for unmanned aerial delivery of a payload 14 (FIG. 8) from a ground station (not shown). The docking system 10 may include an unmanned aerial vehicle (UAV) 20 (FIG. 3) having one or more motors 21 for powered flight and a pyramidal bottom surface 22 opening downward to terminate in a base perimeter 24 with a capture radius 25 (FIG. 6). The UAV 20 may include a 3-axis maneuvering system for maintaining a level attitude during hovering and flying, and may also include a main battery (not shown) for powering the one or more motors 21. An itinerary of the aerial delivery system, centralized at a warehouse, may direct and coordinate a flight plan for the UAV 20 (among a fleet of UAVs) across the service area.

[0023] Continuing with FIGS. 1-8, in various embodiments, the docking system 10 may include a cargo pod 30 configured to carry the payload 14. The cargo pod 30 may include a pyramidal top surface 32 complementary to the pyramidal bottom surface 22 of the UAV 20 for facilitating an alignment and capture of cargo pod 30 by UAV 20. The cargo pod 30 may house a cargo bay 34 lockable by an access door 35 for carrying and securing, respectively, payload 14. The access door 35 may include a locking means 35a, thereby discouraging theft (FIG. 3). The payload 14 may comprise one or more packages slated for delivery to one or more customers in the service area (FIG. 8). Aerodynamic front 52 of the pod 30 may reduce drag and/or generate lift when pointed in a direction of flight. The cargo pod 30 may include internal components 37 for coordinating with the UAV 20 and/or managing the payload 14 (FIGS. 4, 7, 8). For example, one of the components 37 may be an auxiliary battery 38.

[0024] Continuing with FIGS. 1-8, in various embodiments, both of the pyramidal surfaces 22 and 32 may identically be 3-sided, and may preferably be 4-sided. The top surface 32 may slope upward to form intersecting radial edges 54 (FIGS. 5-6) and may terminate at a flat central portion 56 substantially smaller than the base perimeter 24 of bottom surface 22. For example, the central portion 56 of the cargo pod 30 may be approximately half the size of the base perimeter 24 of the UAV 20.

[0025] Referring now to FIGS. 1-3 and 5-7, in various embodiments, the docking system may further comprise a latching system for automatically locking the UAV 20 to the cargo pod 30 when docked. The latching system may include one or more electro-mechanical or magnetic latches 46 (FIGS. 1-2) connectable to the UAV 20 and complementary latch receptacles 36 (FIGS. 1, 3, 6-7) disposed on the cargo pod 30. The latch system may engage once aligned contact has been made between UAV 20 and pod 30. Latch receptacle 36 may be a hard pin mounted to a side 31 of the cargo pod 30 and passing through receptacle opening 36a in the bottom surface 32. Latch 46 may electronically rotate to secure the hard pin 36 to the UAV 20. The latch 46 may also be an electro-permanent magnetic (EPM) device switchable in polarity by a temporary current.

[0026] Referring now to FIGS. 1-3, in various embodiments, a mating rack 26 may provide the pyramidal bottom surface 22 and be attachable to the UAV 20, where the UAV 20 may not itself be configured to provide the pyramidal bottom surface 22. Beneficially, the docking system 10 may thereby be adaptable to aerial vehicles not standardized to provide the bottom surface 22. In the embodiment of FIGS. 1-3, the rack 26 may be disposed with the one or more latches 46 of the latching system for securing the UAV 20 to complementary receptacles 36. In another embodiment, latches 46 may be disposed on or near the base perimeter 24 of the bottom pyramidal surface 22.

[0027] The docking system 10 may include a pyramidal bottom surface 22 (FIG. 5) separate from the rack 26 and UAV 10, the separate bottom surface 22 being directly fastenable to the rack 26 or to the UAV 20. In an embodiment not shown, the mating rack 26 may itself be formed to present aspects of the pyramidal bottom surface 22 critical to mating with pyramidal top surface 32, such as presenting the intersecting radial edges 54. Rack 26 may be made of metal, plastic, or other materials, and may also be referred to as the pod rack unit (PRU). Alternatively, the one or more latches 46 may be disposed on the cargo pod 30 and the complementary receptacles 36 may be disposed directly on the UAV 20 or on the mating rack 26.

[0028] Referring again to FIGS. 1-8, the autonomous docking system 10 may include one or more steering components (not shown) housed in the UAV 20 for approaching the cargo pod 30 at the ground station to within a steering accuracy. The steering components may include one or more of LIDAR, GPS, infrared, inertial, and photographic components for navigating the flight plan, approaching a customer location for delivery, and/or docking at the ground station. The UAV 20 may be configured to dock with the cargo pod 30 by steering downward until the base perimeter 24 slidably contacts the pyramidal top surface 32 of the cargo pod 30 for gravity-aligning the UAV 20 in azimuth and laterally. A capture radius 25 of the base perimeter 24 may be greater than a lateral component of the steering accuracy for capturing the pod 30.

[0029] For example, during a docking maneuver, the UAV 20 may descend toward the cargo pod 30 until the base perimeter 24 of the bottom surface 22 contacts the intersecting radial edges 54 of the top surface 32, whereupon gravity may slidably rotate the UAV 20 ‘downhill’ along the radial edges 54 to center the UAV 20 laterally and align it azimuthally. The 3-axis maneuvering system (not shown) may be configured to compensate for uneven slidable contact with the pyramidal top surface 32 in order to keep the UAV 20 level while allowing gravity descent. The docking system may include a docking sensor (not shown) to indicate correct alignment and mating and which may then enable the latching system. For example, the docking sensor may trigger a latch control line 47 to engage the latching system (FIGS. 1-2). The docking sensor may include any electrical, mechanical, or proximity means disposed on the UAV 20 or the pod 30 for indicating intimate contact therebetween.

[0030] Still with FIGS. 1-8, in various embodiments, the pyramidal bottom 32 and the top 22 surfaces may each be 4-sided and the steering accuracy may therefore have an azimuthal component of less than 45 degrees of error in order to reliably dock. Although the steering accuracy may be sufficient for identifying and navigating to a landing target placed at the customer location within a foot or several inches, this accuracy alone may not be adequate for reliably docking with the pod 30. Beneficially, configuring both the UAV 20 and the pod 30 with complementary pyramidal surfaces and the latching system may provide for an autonomous docking capability executable in the field without human intervention.

[0031] Referring to FIGS. 1-2, 4, and 7-8, the docking system 10 may include one or more power transfer contacts 39 on the pyramidal top surface 32 for sending power from the auxiliary battery 38 to the UAV 20 or its main battery while docked. The power contacts 39 may be spring-loaded copper pads disposed on the pyramidal top surface 32 of the cargo pod 30 and may be configured to electrically mate with complementary transfer contacts (not shown) on the UAV 20. In one embodiment, there may be four contacts 39 disposed on the top surface 32, as shown in FIGS. 1-2 and 6-8. Beneficially, providing the aerial delivery system with a capacity to dock with a cargo pod 30 in the field may provide an opportunity to autonomously refuel the UAV 20 for additional customer deliveries or for the return flight to the central warehouse.

[0032] Referring now to FIGS. 1, 3 and 8, in additional embodiments, the docking system 10 may further comprise a pod bottom surface 33 (FIG. 8) on the cargo pod 30 and which conforms to the pyramidal bottom surface 22 of the UAV for docking with and stacking onto another cargo pod. Another latching system may be included in system 10 for locking the two cargo pods 30 together for storage at the ground station. The ground station may be a docking station (not shown) for securing one or more stacked cargo pods 30 to the ground. The docking station may include a dock top surface for capturing the pod bottom surface 33 or the UAVs bottom surface 22. The dock top surface may be configured to conform to the pyramidal top surface 32 of the cargo pod 30.

[0033] Continuing, the docking station may also be configured with electrical power and a power transfer means for routing the electrical power to the one or more stacked cargo pods for charging the main battery or charging the auxiliary batteries 38 of the stacked pods. The power transfer means may include one or more power transfer contacts 39 on the dock top surface for sending the electrical power to the stacked pods 30 or the UAV 20. The electrical power may be provided by an auxiliary battery of the docking station or by a land-based electrical grid.

[0034] The one or more steering components of the UAV 20 may be configured for approaching the docking station to within the steering accuracy of the UAV 20. The UAV 20 may be configured to steer downward until the base perimeter 24 of the lowest of the one or more stacked cargo pods 30 slidably contacts the dock top surface for gravity-aligning the cargo pods 30 in azimuth and laterally, where a capture radius 25 of the base perimeter 24 is greater than a lateral component of the steering accuracy.

[0035] The bottom surface of the cargo pod may be equipped with the complementary power transfer contacts for transferring power from the power transfer contacts on the docking station or another cargo pod. Alternatively, the docking station may employ induction charging for transferring power to the cargo pod or UAV captured above it and without using exposed metal contacts. Beneficially, the described pyramidal surfaces 22 and 32, latching systems, and power transfer contacts 39 may provide a docking system 10 that enables the autonomous retrieval of one or more cargo pods 30, the field charging of pod 30 and UAV 20, and the secure parking of payloads 14 at ground stations.

[0036] Although the above embodiments have been described in language that is specific to certain structures, elements, compositions, and methodological steps, it is to be understood that the technology defined in the appended claims is not necessarily limited to the specific structures, elements, compositions and/or steps described. Rather, the specific aspects and steps are described as forms of implementing the claimed technology. Since many embodiments of the technology can be practiced without departing from the spirit and scope of the invention, the invention resides in the claims hereinafter appended.