The disclosure relates to airport stand arrangement (100,200,300) comprising: a display (130); a radar-based system (110R); and one or more additional systems selected from laser-based systems (110L) and imaging systems (110C), wherein said radar-based system (110R) and said one or more additional systems together form a combined system (110,210,310), wherein the airport stand arrangement (100) is configured, based on output data from said combined system (110), to detect and track (S108,S110) an aircraft (10) within a stand area (20) when said aircraft (10) is approaching a stand within the stand area (20) for parking at a parking position (160) therein, and configured, based on said detection and tracking of the approaching aircraft (10), to provide (S114,S116) pilot maneuvering guidance information on said display (130) for aiding a pilot of the approaching aircraft (10) in maneuvering the aircraft (10) towards said parking position (160).

A base station is disclosed for an unmanned aerial vehicle (UAV) that includes: an enclosure defining a window that is configured to receive the UAV to allow for entry of the UAV into the base station and exit of the UAV from the base station; a door that is movably connected to the enclosure such that the door is repositionable between a closed position and an open position; a sealing member that extends about the window and which is configured for engagement with the door so as to form a seal therewith in the closed position; and a heating system that is supported by the enclosure and which is configured to heat the door and/or the sealing member to support operation (e.g., opening and closure) of the door in a cold environment, wherein the heating system includes at least one light source and at least one heating element.

A monitoring system, a base station, and a control method thereof are provided. The monitoring system includes a drone and a base station. The drone includes a main body and at least two leg holders extending from the main body. The base station includes a platform and a positioning mechanism. The platform has a horizontal plate, and the drone is placed on the platform. The positioning mechanism includes at least two movement members. The movement members are movably disposed on the platform and movable between a first position and a second position. When the movement members are located at the second position, the movement members hold and fix the leg holders of the drone, each of the leg holders forms an inclined angle with respect to the horizontal plate, and the inclined angle is less than 90 degrees.

To provide a technology capable of realizing safety flight of a flying object without limiting a flight area for the flying object. An autonomous mobile apparatus according to the present technology includes a mobile unit, a bumper unit, and a control unit. The mobile unit moves an autonomous mobile apparatus by driving. The bumper unit capable of reducing a fall impact of a flying object. The control unit controls driving of the mobile unit on the basis of a position of the flying object.

The present disclosure relates to a device for unstowing an electrical supply cable from a storage chamber disposed within an underground service pit. The cable is configured to electrically connect to an electrical power supply at a first end and to connect to an external power socket of an aircraft at a second end for supplying electrical power to the aircraft. The device includes a cable guiding wheel that is disposed at ground level above the underground service pit and configured to receive the cable. The device also includes a motor coupled to the cable guiding wheel that is configured to drive the cable guiding wheel. Upon activation, the motor rotates the cable guiding wheel to generate a pulling force on the cable to at least partially lift the cable out of the storage chamber.

The present disclosure provides doorway protection assemblies with a base portion and two leg portions that can be positioned over and protect the exterior surrounding a doorway of a vehicle, such as an aircraft, from damage while cargo or other items are being loaded into or unloaded from the vehicle. Each assembly can include one or more attachment portions that wrap over and attach to the door sill area or side jambs of the vehicle doorway in order to secure the assembly in place. Each assembly can include a cushion layer between the various portions and the exterior of the aircraft to further avoid or reduce damage. Each assembly can include retention straps that releasably attach to anchors on the vehicle to further secure the assembly on the vehicle doorway.

Electric aircraft charging system including charging cable configured to carry electricity and energy source, wherein the energy source is electrically connected to the charging cable. The system also including a cable reel module, the cable reel module including a reel, wherein the reel is rotatably mounted to the cable reel module, wherein the reel is configured to rotate in a forward direction and a reverse direction, and the charging cable, in a stowed configuration, is wound around the reel. The cable reel module further including a rotation mechanism configured to rotate the reel in reverse, and a cable reel module door having a closed position and an open position, wherein the closed position prevents access to the reel and the open position allows access to the reel. The system additionally including a controller communicatively connected to the rotation mechanism and configured to send a retraction signal to the rotation mechanism.

A delivery system includes a processor programmed to construct a route so as to include predefined segments traveled by carriers configured to taxi the vehicle and charge a battery thereof such that a state of charge of the battery remains above a target for a duration of the route, and forward the route to the vehicle.

A landing zone arrangement is disclosed for aircraft capable of vertical take-off. The arrangement includes a plurality of segments that form a landing zone in an operating state, a storage space for at least partially storing the segments in a stored state, and a base with a rotatable rotor element in order to rotate the segments for transfer between the operating state and the stored state. The landing zone arrangement allows a lighter technical design as the individual segments are removably secured to the rotor element, and a securing unit of the arrangement is designed to fasten the removable segments to the rotor element for transfer into the operating state and to release this fastening for transfer into the stored state. A lifting unit is provided in order to move the removable segments in the direction of the rotor element when transferring into the operating state.

A device and a method for introducing a drone to an area of interest are presented. The delivery system may include a housing, a drone, either a timer or a receiver, a lock mechanism, and a biasing mechanism. The housing further includes a pair of parts with or without subparts. At least one sensor is attached to the drone. The timer or the receiver is secured to the housing and communicable with the lock mechanism to control function thereof. The lock mechanism is adapted to releasably secure the parts or the subparts. The drone is enclosed within the housing in a CLOSED configuration when the lock mechanism is locked. The biasing mechanism separates the parts or the subparts to an OPEN configuration when the lock mechanism is unlocked. The drone is introducible to the area of interest in the CLOSED configuration and separable from the housing in the OPEN configuration.