A drone station according to an embodiment of the present disclosure comprises: a roof allowing a drone to land thereon; a side wall formed to be erected around all sides of the roof from the lower side of the roof; a nozzle which is formed at an edge at which the roof and the side wall meet each other, and sprays an air current upward; a grill formed on the side wall to allow external air to be introduced thereinto; a guide panel disposed inside the grill to guide fluid flow so that fluid flows from the grill to the nozzle; and a rotor disposed inside the guide panel to move fluid from the grill side to the nozzle side through a rotating operation.

Systems and methods include UAVs that serve to assist carrier personnel by reducing the physical demands of the transportation and delivery process. A UAV generally includes a UAV chassis including an upper portion, a plurality of propulsion members configured to provide lift to the UAV chassis, and a parcel carrier configured for being selectively coupled to and removed from the UAV chassis. UAV support mechanisms are utilized to load and unload parcel carriers to the UAV chassis, and the UAV lands on and takes off from the UAV support mechanism to deliver parcels to a serviceable point. The UAV includes computing entities that interface with different systems and computing entities to send and receive various types of information.

An autonomous remote device for deployment in an area, comprising: a mechanism for launching the device airborne from a first of a plurality of locations; a mechanism for navigating the device when airborne to a second of the plurality of locations; and a mechanism for landing the device at the second of the plurality of locations.

The present disclosure provides a control method of a UAV, a control device of a UAV, and a computer-readable storage medium, and relates to the technical field of UAVs. The control method of a UAV includes: determining a deviation between a vertical mapping point on the ground and a landing point of the UAV, the deviation comprising a deviation in a horizontal axis direction of a camera coordinate system and a deviation in a vertical axis direction of the camera coordinate system; and generating speed control amounts of the UAV in the horizontal axis direction and the vertical axis direction of the camera coordinate system by a controller, using the deviation in the horizontal axis direction and the deviation in the vertical axis direction.

Methods, apparatus, systems, and articles of manufacture are disclosed to house a vehicle, including a first container leg disposed on a first corner of a first container, a second container leg disposed on a second corner of the first container, a third container leg disposed on a third corner of the first container, a fourth container leg disposed on a fourth corner of the first container, at least one of the first, second, third, and fourth container legs each having an upper portion with a ramped receiving slot and a lower portion with a first ramped foot, and wherein the ramped receiving slot is to receive a protrusion associated with a second ramped foot of a second container different from the first container.

The delivery system S acquires sensing information sensed in a transfer area by a sensor mounted on UAV 1 that delivers an article, and determines whether visibility in the transfer area is good on the basis of the sensing information. Then, in a case where it is determined that the visibility is not good, the delivery system S performs a first notification processing for stopping a recipient who is going to receive the article from heading for the area, while in a case where it is determined that the visibility is good, the delivery system S performs a second notification processing for directing the recipient to head for the area.

The disclosure relates to a method for guiding landing of an unmanned aerial vehicle. The method for guiding landing of unmanned aerial vehicle includes: determining location information of the unmanned aerial vehicle over a target airdrome by using a plurality of position detectors in an airdrome auxiliary positioning system; generating corrected guidance information according to an offset vector between the location information and target location information, where the target location information is information representing any location within signal coverage of a guidance beacon of the target airdrome; and sending the corrected guidance information to the unmanned aerial vehicle, where the corrected guidance information is used to guide the unmanned aerial vehicle to fly into the signal coverage of the guidance beacon.

A system comprising a reel, a tether configured to be wound about the reel, and at least one unmanned aerial vehicle attached to the tether. When unmanned aerial vehicle is at rest, the unmanned aerial vehicle resides on the reel. Related methods of operating such a system can be used to extract crop from a field.

A landing system suitable for receiving an unmanned aerial vehicle (UAV) comprises an autonomous ground vehicle (AGV). A landing surface is disposed on the AGV, and the landing system comprises a loading channel suitable for passing an object delivered by the UAV through a first loading channel opening in the landing surface. The object passes within the loading channel through to a second loading channel opening at a bottom aspect of the AGV. In this way, a UAV can land on the landing surface, and the AGV positions the object in line with a target delivery location, where the object is delivered. Aspects of the landing system comprise an electromagnet or vacuum chamber for securing the UAV to the landing surface, thereby enhancing stability of the UAV during movement of the landing system.

An aircraft includes an airframe with a thrust array attached thereto. The thrust array includes a plurality of propulsion assemblies that are independently controlled by a flight control system. A landing gear assembly is coupled to the airframe and includes a plurality of landing feet. An altitude sensor array includes a plurality of altitude sensors each of which is disposed within one of the landing feet such that when the aircraft is in the VTOL orientation, the altitude sensor array is configured to obtain multifocal altitude data relative to a landing surface. The flight control system is configured to generate a three-dimensional terrain map of the surface based upon the multifocal altitude data.