The present invention relates to a control input device applicable to an eVTOL aircraft, an electric vertical takeoff and landing aircraft. More particularly, the present invention relates to an aircraft control input device and a command input method using the same, which replaces the conventional cyclic stick, rudder pedals, and collective stick used in aircraft flight control, offering a simpler structure and easier operation compared to traditional control systems, and facilitating convenient and precise flight operations, thereby enhancing the convenience for pilots and the safety of flight operations.

    본 발명은 전기동력 수직이착륙 항공기인 eVTOL 항공기에 적용할 수 있는 조종입력장치에 관한 것으로, 더욱 상세하게는 종래의 항공기 비행조종에 사용되는 싸이클릭 조종간, 러더 페달 및 콜렉티브 조종간에 대해 본 발명의 조종입력장치로 대체함으로써, 기존의 조종장치에 비해서 구성이 간단하고 조작이 용이하며, 간편하고 정확한 비행 조작을 통해 조종사의 편의성과 비행 운행의 안정성을 향상시킬 수 있는 항공기의 조종입력장치 및 이를 이용한 명령 입력 방법에 관한 것이다.


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    Title :

    Aircraft control input device and command input method using the same


    Additional title:

    항공기의 조종입력장치 및 이를 이용한 명령 입력 방법


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

    Publication date :

    2023-06-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G05G CONTROL DEVICES OR SYSTEMS INSOFAR AS CHARACTERISED BY MECHANICAL FEATURES ONLY , Steuer- oder Regelvorrichtungen oder Steuer- oder Regelsysteme gekennzeichnet ausschließlich durch mechanische Einzelheiten



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