The present invention provides a remote control system of an aircraft 1 that includes a camera 2 mounted on the aircraft 1, a monitor 4 visible from an operator 3 remote from the aircraft 1, a remote controller 5 operated by the operator 3, an acceleration sensor 6 mounted on the aircraft 1 to detect upward/downward, left/right and forward/backward accelerations, sensitive pads 7 configured to be attached to each portion of the operator 3, and a controller 8 that generates a vibration or an electrical stimulus on each of the sensitive pads 7 while a magnitude of the vibration or the electrical stimulus is changed based on an output value of the acceleration sensor 6 to make the operator 3 feel a direction and a magnitude of the acceleration generated on the aircraft 1.


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    Titel :

    REMOTE CONTROL SYSTEM FOR AIRCRAFT


    Beteiligte:
    TERASAKA RYU (Autor:in)

    Erscheinungsdatum :

    2016-11-10


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B60R Fahrzeuge, Fahrzeugausstattung oder Fahrzeugteile, soweit nicht anderweitig vorgesehen , VEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



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