The present invention relates to a control input device applicable to an eVTOL aircraft, which is an electric-powered vertical take-off and landing aircraft, and more particularly, to an aircraft control input device that may replace a cyclic control stick, a tail rotor control pedal, and a collective control stick used for flight control of a conventional aircraft, which is simpler in configuration and easier to operate than conventional control devices and may improve pilot convenience and stability of flight operation through simple and accurate flight manipulation, and a command input method using the same.


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    Title :

    AIRCRAFT CONTROL INPUT DEVICE AND COMMAND INPUT METHOD USING THE SAME


    Contributors:
    KANG YOUNGSHIN (author) / PARK BUMJIN (author) / CHOI SEONGWOOK (author) / KIM YUSHIN (author) / BAE JONGMIN (author) / CHOI JOOWON (author) / CHANG SUNGHO (author)

    Publication date :

    2023-09-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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    KANG YOUNGSHIN / PARK BUMJIN / CHOI SEONGWOOK et al. | European Patent Office | 2025

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    Aircraft control input device and command input method using the same

    KANG YOUNGSHIN / PARK BUMJIN / CHOI SEONGWOOK et al. | European Patent Office | 2023

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    COMMAND INPUT DEVICE

    DUNAEV NIKOLAJ ALEKSANDROVICH / CHENDRIKOVA INESSA VLADIMIROVNA | European Patent Office | 2019

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