FIBER OPTIC SLAT FLAP SYSTEM AND CONTROL LEVER

    公开(公告)号:EP4371875A1

    公开(公告)日:2024-05-22

    申请号:EP23210977.7

    申请日:2023-11-20

    IPC分类号: B64C13/50 G05D1/49

    CPC分类号: B64C13/503

    摘要: A control system performs a method of controlling a wing of an airplane. The control system includes an optical fiber (112, 114), a bending device (410) and a processor (210). The optical fiber is configured to receive light having an input optical phase. The bending device applies an external force on the optical fiber. The external force causes the light exiting the optical fiber to have an output optical phase. a processor determines a phase shift between the input optical phase and the output optical phase and controls the wing based on the phase shift.