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.

    A control system for a rotorcraft, which system includes at least one control unit allowing a rotor of a rotorcraft to be driven, with the rotorcraft including at least three independent landing-gear units, with each landing-gear unit including means for detecting a ground reaction force F1, F2, F3 exerted on the landing-gear unit when the rotorcraft is in contact with the ground, and with the control system being suitable for receiving information from the detection means. The invention also relates to the rotorcraft and to a control method corresponding to the control system.


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    Title :

    ROTORCRAFT CONTROL SYSTEM ROTORCRAFT ASSOCIATED AND CORRESPONDING CONTROL METHOD


    Additional title:

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


    Publication date :

    2018-05-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

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



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