An aircraft vibration detecting device applicable to an aircraft having a moving surface to be driven by an actuator includes a difference calculating unit for calculating a difference between a target value of an angle of the moving surface and an actual measured value of the angle of the moving surface, a threshold value determining unit for determining whether an absolute value of the difference is equal to or greater than a threshold value, and a vibration determining unit for determining that the moving surface is vibrating if the absolute value of the difference is equal to or greater than the threshold value.


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    Title :

    AIRCRAFT VIBRATION DETECTING DEVICE, AIRCRAFT VIBRATION DETECTING METHOD, AND NON-TRANSITORY COMPUTER-READABLE STORAGE MEDIUM STORING THEREON PROGRAM FOR AIRCRAFT VIBRATION DETECTION


    Contributors:

    Publication date :

    2021-09-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT





    Vibration of aircraft

    Barlow, F.G. | Engineering Index Backfile | 1938


    Vibration of aircraft

    Barlow, F.G. | Engineering Index Backfile | 1938


    VIBRATION CONTROL ASSEMBLY FOR AN AIRCRAFT AND METHOD OF CONTROLLING AIRCRAFT VIBRATION

    WELSH WILLIAM A / GMIRYA YURIY | European Patent Office | 2020

    Free access