Disclosed is an aircraft and a method of controlling an aircraft. The aircraft comprises a continuous wing assembly extending from port to starboard sides of the aircraft. The aircraft is controlled partially by flexing portions of the wing, and partially or totally by mechanical systems that alter the position of a fuselage with respect to the wing. The fuselage is attached to the wing by a wing/fuselage joint structure that permits at least two mutually orthogonal axes of rotation of the fuselage relative to the wing. The aircraft includes a sensors, a telemetry system linked to a remote server, and a control system for programming flight information and aircraft control instructions and a plurality of actuators responsive to the control system for rotating the fuselage relative to the wing and flexing the wing for controlling the flight of the aircraft in response to instructions from the control system.


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    Title :

    UNMANNED AERIAL VEHICLE WITH SYNCHRONIZED SENSOR NETWORK


    Additional title:

    UNBEMANNTES LUFTFAHRZEUG MIT SYNCHRONISIERTEM SENSORNETZWERK
    VÉHICULE AÉRIEN SANS PILOTE POURVU D'UN RÉSEAU DE CAPTEURS SYNCHRONISÉS


    Contributors:

    Publication date :

    2023-01-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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