A flying object control system includes a flying object, and a setting base that performs holding of the flying object and releasing the holding, the flying object and the setting base being communicable with each other. The flying object controls, upon receiving a takeoff instruction, thrust for taking off from a predetermined initial position, and when the thrust becomes greater than or equal to a first threshold, the flying object notifies the setting base of a start notification. Upon receiving the start notification, the setting base releases the holding of the flying object and notifies the flying object of a release completion notification. Upon receiving the release completion notification, the flying object takes off from the predetermined initial position by controlling the thrust in such a manner that the thrust becomes a second threshold smaller than the first threshold.

Provided herein is a taxiing system for steering an amphibious aircraft on a body of water. The system has a pair of thrusters that are deployed after landing on the water to taxi the amphibious the aircraft prior to docking and to unloading and are retractable to taxi the amphibious aircraft prior to take-off. Also provided is a docking device to dock the amphibious aircraft to a mooring buoy. In addition provided herein is a system for maneuvering an amphibious aircraft during taxiing and docking on water that integrates the taxiing system with the docking device.

Provided herein is a taxiing system for steering an amphibious aircraft on a body of water. The system has a pair of thrusters that are deployed after landing on the water to taxi the amphibious the aircraft prior to docking and to unloading and are retractable to taxi the amphibious aircraft prior to take-off. Also provided is a docking device to dock the amphibious aircraft to a mooring buoy. In addition provided herein is a system for maneuvering an amphibious aircraft during taxiing and docking on water that integrates the taxiing system with the docking device.

An anchor for an aircraft. The anchor comprises a jack comprising a housing and a head that is able to move in translation in relation to the housing along an elevation axis, the head having three degrees of rotational freedom respectively about a longitudinal axis as well as a transverse axis and the elevation axis, the anchor comprising a member for taking up forces surrounding the jack and provided with a fastening suitable for being secured to the aircraft.

The present invention discloses a helicopter hoisting platform for a wind turbine nacelle cover, the helicopter hoisting platform comprising a composite layer and a plurality of metal plates arranged on the outer surface of the composite layer, wherein the plurality of metal plates forms a conductive network electrically connected to a ground connection.

An electric vertical take-off and landing (eVTOL) vehicle is positioned to be in a charging position on the ground, wherein the eVTOL vehicle is capable of performing vertical take-offs and landings. The battery is charged while in the charging position on the ground using a wind turbine that includes the rotor.

An electric vertical take-off and landing (eVTOL) vehicle is positioned to be in a charging position on the ground, wherein the eVTOL vehicle is capable of performing vertical take-offs and landings. The battery is charged while in the charging position on the ground using a wind turbine that includes the rotor.

A control device (200) includes a ground vehicle controller (230) that causes a ground vehicle to travel at a target area, an acquirer (210) that acquires state information expressing a state of a surface of the target area while the ground vehicle travels the target area, and a determiner (240) that determines, based on the acquired state information, whether or not an aircraft is landable at the target area.

Disclosed is a naval platform equipped with a deck-landing/takeoff zone for at least one aircraft and dolly-type mechanism for handling the aircraft to move it over the deck-landing/takeoff zone. The dolly-type mechanism includes a vacuum disc for immobilizing the dolly and thereby securing the aircraft in position on the deck-landing/takeoff zone, the operation of which is triggered by an analyzer of the behavior of the platform in order to avoid any risk of uncontrolled movement of the aircraft.

Innovative new methods in connection with lighter-than-air free floating platforms, of facilitating legal transmitter operation, platform flight termination when appropriate, environmentally acceptable landing, and recovery of these devices are provided. Especially, termination of radio transmissions and flight related to regional, governmental and international border requirements, regulations and laws. The new methods comprise specific criteria, detection of the criteria and elements of operation for reducing or preventing illegal transmissions, for producing rapid descend to the ground, for environmentally acceptable landing and for facilitating recovery all with improved safety and enhanced compliance with known regulations.