The present invention relates to a control system (1) of a rotary wing aircraft (4), which comprises at least one control device (2) capable of operating rotors (3, 13) of the rotary wing aircraft (4). The rotary wing aircraft (4) comprises at least three independent landing gears (5, 6, 7). Each of the landing gears (5, 6, 7) includes units (8) for detecting reaction force (F1, F2, F3) on the ground, which acts on the landing gears (5, 6, 7), when the rotary wing aircraft (4) comes in contact with the ground, and control units (10) receive information provided from the detecting units (8). Accordingly, the control system (1) assures definite and efficient operation of the rotary wing aircraft (4). The present invention also relates to the rotary wing aircraft (4) and a control method corresponding to the control system (1).

    본 발명은 회전익 항공기(4)의 회전자(3, 13)를 조종할 수 있게 하는 제어 장치(2)를 적어도 하나 포함하는 회전익 항공기(4)의 제어 시스템(1)에 관한 것으로, 회전익 항공기(4)가 적어도 세 개의 독립적인 착륙 장치(5, 6, 7)를 포함하는데, 각 착륙 장치(5, 6, 7)가, 회전익 항공기(4)가 지면과 닿을 때, 착륙 장치(5, 6, 7)에 작용하는 지면의 반작용력(F1, F2, F3) 탐지 수단들(8)을 포함하고, 제어 수단(1)이 탐지 수단들(8)로부터 나온 정보를 받을 수 있다. 본 발명은 또한 회전익 항공기(4)와 제어 시스템(1)에 상응하는 제어 방법에 관한 것이다.


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    Titel :

    ROTORCRAFT CONTROL SYSTEM ROTORCRAFT ASSOCIATED AND CORRESPONDING CONTROL METHOD


    Weitere Titelangaben:

    회전익 항공기의 제어 시스템, 관련된 회전익 항공기 및 해당 제어 방법


    Beteiligte:

    Erscheinungsdatum :

    14.11.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / G05B Steuer- oder Regelsysteme allgemein , CONTROL OR REGULATING SYSTEMS IN GENERAL




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