Disclosed is an active pilotage input system used in an FBW flight control system. According to an embodiment of the present invention, the active pilotage input system electrically converts the four-axial control inputs of pitch, roll, collective, and yaw from the physical movement between each control using a cyclic assembly, a collective assembly, and a pedal assembly, which are pilotage input devices, and an active control inceptor system (ACIS) controller delivers the result to flight control computers (FLCC). The FLCCs can control signals for pilotage input only with ARINC429 signal communications.

    FBW 비행제어시스템에서 사용되는 능동형 조종입력시스템을 개시한다. 본 발명의 일 실시 예에 따른 능동형 조종입력시스템은 조종입력장치인 사이클릭 조립체(Cyclic Assembly), 컬렉티브 조립체(Collective Assembly), 및 페달 조립체(Pedal Assembly)를 통해 각 조종간의 물리적 움직임으로 발생되는 피치(Pitch), 롤(Roll), 컬렉티브(Collective), 요우(Yaw) 등의 4축의 조종 입력을 전기적으로 변환하여 ACIS(Active Control Inceptor System) 제어기가 비행조종컴퓨터(Flight Control Computer : FLCC)들로 전달해 준다. 그리고, FLCC들에서 ARINC429 신호 통신만으로 조종입력에 대한 신호 제어가 가능하도록 구성된다.


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    Titel :

    FBW ACTIVE CONTROL INCEPTOR SYSTEM USED FOR FLY-BY-WIRE FLIGHT CONTROL SYSTEM


    Weitere Titelangaben:

    FBW 비행제어시스템에서 사용되는 능동형 조종입력시스템


    Beteiligte:
    KIM JAE MAN (Autor:in) / KOO CHIL HYO (Autor:in)

    Erscheinungsdatum :

    2016-11-02


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen




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