An autonomous landing system for vertical landing aircraft includes a vertical landing aircraft including a powertrain and an onboard camera, a motion-stabilized visual cue including a visual indicator, wherein the visual cue is configured to maintain a fixed orientation of the visual indicator with respect to a horizon, and an autonomous control system configured to control a position of the aircraft with respect to the visual indicator of the visual cue based on image data captured by the onboard camera.

An apparatus for permitting a flying vehicle to land on or take off therefrom whilst the apparatus is airborne, the apparatus including: a surface for supporting the flying vehicle during landing or when taking off; at least one propulsion device for sustaining flight of the apparatus and for positioning the surface in a desired landing or taking off orientation; and a link which is connectable at one end to a land- or sea-going vehicle, for tethering the apparatus relative thereto.

A method, apparatus and computer program product are provided to collect additional location-related data. In the context of a method, for example, an entity in motion is identified and a drone is caused to accompany the entity that has been identified and to collect the location-related data while accompanying the entity. After having collected at least some location-related data, the method includes causing the drone to discontinue accompanying of the entity and to travel toward a destination.

The article transfer system S selects an article transfer candidate on the basis of first sensing information obtained from first sensing performed by the unmanned aerial vehicle in flight, performs a movement control of the unmanned ground vehicle on the basis of position information of the selected article transfer candidate, and determines an article transfer place with reference to the selected article transfer candidate on the basis of second sensing information obtained from second sensing performed by the unmanned ground vehicle.

A method for controlling operation of an unmanned aerial vehicle (UAV), includes receiving one or more commands selected by a user via a remote controller of the UAV, and in response to a received landing command: identifying the vehicle from a plurality of vehicles for landing, navigating the UAV to travel in a substantially same direction as the vehicle, and controlling the UAV to land on the vehicle when the UAV approaches the vehicle. The one or more commands includes at least the landing command to land the UAV on a vehicle while the vehicle is in operation.

A thermally controlled payload container for carrying payloads by an Unmanned Aerial Vehicle (UAV) comprising an inner wall and an outer wall. The inner wall forms a chamber having an open end and a closed end. The payload container also comprises a thermal control body adjacent to the inner wall and disposed between the inner wall and the outer wall. The payload container also comprises a thermoelectric cooler (TEC) extending through the outer wall from a first side of the TEC to a second side of the TEC, the first side adjacent the thermal control body and the second side coupled to an external heat sink.

A canister is coupled to a delivery vehicle using a rail bracket. The canister comprises a securing channel having a first securing channel volume and a second securing channel volume. A width of the first securing channel volume is less than a width of the second securing channel volume. The rail bracket comprises a rotational shaft having a finger at one end. The rail bracket is inserted into the securing channel, and the rotational shaft is rotated. When rotated, the finger inhibits removal of the rail bracket from the securing channel, thereby providing a mechanism by which the canister can be releasably coupled to the rail bracket. The rail bracket may be provided on a delivery vehicle, such as an unmanned aerial vehicle (UAV) to transport the canister and contents within it.

A system for swapping one or more batteries includes a battery holder configured to store a first battery, wherein the battery holder further includes retainers positioned proximate a front end and a rear end of the battery holder, the retainers having a first position and a second position such that the retainers, in the first position, are configured to engage the first battery in order to dispose the first battery in a storage position in the battery holder and, in the second position, are configured to disengage from the first battery to allow the first battery to move from the storage position. The system further includes cartridges having a front end and a rear end configured to couple to at least one of the front end and the rear end of the battery holder and further configured to hold a second battery in the second enclosure.

A method for controlling palm landing of an unmanned aerial vehicle (“UAV”) includes detecting a flight status of the UAV under a predetermined condition. The method also includes controlling the UAV to land on a palm of a user when the flight status is a hover state and when the palm is located under the UAV.

An apparatus for housing an unmanned aerial vehicle (UAV) in or on a vehicle includes a landing connection component configured to form a connection between the UAV and the vehicle when the UAV is landed in or on the vehicle, and a cover movable between a plurality of positions to permit the UAV to take off and land in or on the vehicle. The cover includes an antenna or a satellite dish integrated thereto. An orientation of the antenna or the satellite dish is adjustable for tracking a motion of the UAV when the UAV is in flight.