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 :

    2016-04-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / B64C AEROPLANES , Flugzeuge / G08B SIGNALLING OR CALLING SYSTEMS , Signalisier- oder Rufsysteme



    Rotor moment feedback for stability augmentation

    ELLER EREZ / WULFF OLE | European Patent Office | 2016

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    ROTOR MOMENT FEEDBACK FOR STABILITY AUGMENTATION

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