Embodiments are directed to obtaining at least one measurement of blade bending associated with at least one blade of at least one rotor of an aircraft, processing, by a device comprising a processor, the at least one measurement to obtain moment data, obtaining data from an inertial measurement unit (IMU), and processing, by the device, the moment data and the data from the IMU to generate a command configured to stabilize the aircraft.


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    Title :

    ROTOR MOMENT FEEDBACK FOR STABILITY AUGMENTATION


    Contributors:
    ELLER EREZ (author) / WULFF OLE (author)

    Publication date :

    2015-07-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    ROTOR MOMENT FEEDBACK FOR STABILITY AUGMENTATION

    ELLER EREZ / WULFF OLE | European Patent Office | 2016

    Free access

    Rotor moment feedback for stability augmentation

    ELLER EREZ / WULFF OLE | European Patent Office | 2016

    Free access

    Rotor moment feedback for stability augmentation

    ELLER EREZ / WULFF OLE | European Patent Office | 2016

    Free access

    ROTOR MOMENT FEEDBACK FOR STABILITY AUGMENTATION

    ELLER EREZ / WULFF OLE | European Patent Office | 2016

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