A refueling system has a vehicle having a fuel tank connected to a deployable fuel hose, an end effector having controlled flight, the fuel hose connected at an end away from the first vehicle, through the end effector to a fuel connector under the end effector, a second vehicle having a fuel tank coupled through a pumping apparatus to a fueling port on an acquisition apparatus adapted to acquire the end effector and connect the fueling port and the fuel connector of the end effector, and control circuitry enabling controlled flight of the end effector, wherein the end effector is controlled to be acquired by the acquisition apparatus to couple the fuel connector with the fueling port and fuel is provided from the fuel tank of one of the vehicles to the fuel tank of the other of the vehicles through the pumping apparatus.

A package coupling apparatus for securing a package to an unmanned aerial vehicle (UAV) is provided. The package coupling apparatus includes a support plate configured to be secured to an upper surface of the package and a handle extending up from the support plate. The handle includes a handle opening and a bridge that extends over the handle opening, wherein the bridge is configured to be secured by a component of the UAV.

An UAV 1 performs a detachment control to detach a cargo supported by a support portion 117 or connected a connecting portion 118, and thereafter, performs a load detection process of detecting a mechanical load applied to the support portion 117 or the connecting portion 118. And then An UAV 1 performs different control according to the mechanical load, with respect to a movement of the UAV 1 after the detection of the mechanical load.

A drone is for installing an object on a power line. The drone has a connection means for connecting the drone to the object, so that the drone may carry the object. A first engagement member is for engaging a second engagement member on the object. A power source is for operating the first engagement member so as to actuate a locking means on the object, via the second engagement member, for securely locking the object to the power line. The drone further has a device for limiting one or more degrees of freedom of the object relative to the power line before engaging the locking means.

A detection system for detecting underwater conditions according to an embodiment or embodiments may include an aerial vehicle and a suspended device suspended from the aerial vehicle, wherein the suspended device includes a detecting section that performs an underwater detection operation, and a position information acquisition section that acquires position information.

An example UAV landing structure includes a landing platform for a UAV, a cavity within the landing platform, and a track that runs along the landing platform and at least a part of the cavity. The UAV may include a winch system that includes a tether that may be coupled to a payload. Furthermore, the cavity may be aligned over a predetermined target location. The cavity may be sized to allow the winch system to pass a tethered payload through the cavity. The track may guide the UAV to a docked position over the cavity as the UAV moves along the landing platform. When the UAV is in the docked position, a payload may be loaded to or unloaded from the UAV through the cavity.

An unmanned aerial vehicle executes: a movement control process that moves the unmanned aerial vehicle to a delivery area including a delivery address to which a package is to be delivered, the delivery area including delivery destination candidates, and each of the delivery destination candidates including an identification information indicator located at a position where the identification information indicator is readable from outside; an identification information acquiring process that acquires identification information associated with each delivery destination candidate by reading a corresponding identification information indicator; a delivery destination identifying process that identifies, as a delivery destination, a delivery destination candidate in which the acquired identification information matches the delivery address; a position identifying process that identifies a receiving position of the package based on a position of the identified delivery destination; and a placing process that places the package at the identified receiving position.

A UAV for transporting a payload comprising a vehicle body; a retractable rail exposed on an underside of the vehicle body; a retraction mechanism coupling the rail to the vehicle body for causing the rail to raise and lower relative to the vehicle body; and a barrier located on the vehicle body so as to confront the rail when the rail is in its raised position to block the removal from the rail of a payload slidably engaged with the rail. A mechanism for advancing a payload onto and along the rail and pushing it off.

FIG. 1

A refueling system has a vehicle having a fuel tank connected to a deployable fuel hose, an end effector having controlled flight, the fuel hose connected at an end away from the first vehicle, through the end effector to a fuel connector under the end effector, a second vehicle having a fuel tank coupled through a pumping apparatus to a fueling port on an acquisition apparatus adapted to acquire the end effector and connect the fueling port and the fuel connector of the end effector, and control circuitry enabling controlled flight of the end effector, wherein the end effector is controlled to be acquired by the acquisition apparatus to couple the fuel connector with the fueling port and fuel is provided from the fuel tank of one of the vehicles to the fuel tank of the other of the vehicles through the pumping apparatus.

Unmanned autonomous vehicle (UAV) selection information identifying a UAV, flight path information, and a relative elevation difference value that is a difference between a first elevation value of a start location and a second elevation value of a drop location are received. Navigation of the UAV is initiated using the UAV selection information and the flight path information. A relative altitude difference value is obtained using a first altitude value of the UAV associated with the start location and a second altitude value of the UAV associated with the drop location. In response to a difference between the relative elevation difference value and the relative altitude difference value being outside a predefined threshold, UAV is caused to adjust the second altitude value such that an updated difference between the relative elevation difference value and an updated relative altitude difference value is within the predefined threshold.