A method of operating a vibration control system (VCS) using a single actuator which operates to attenuate a system frequency of a system is provided. The method includes determining whether current vibrations at a non-system frequency exceed a predefined level, determining a system response to compensate for the current vibrations exceeding the predefined level and adjusting the force response of the single actuator to respond to a system frequency and the non-system frequency according to the determined system response toward compensating for the current vibrations.


    Access

    Download


    Export, share and cite



    Title :

    DAMAGE ADAPTIVE VIBRATION CONTROL


    Contributors:

    Publication date :

    2017-10-05


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F16F SPRINGS , Federn



    Damage adaptive control

    LITWINOWICZ ANTHONY / SAHASRABUDHE VINEET / GARHART JONATHAN K et al. | European Patent Office | 2016

    Free access

    Damage adaptive control

    LITWINOWICZ ANTHONY / SAHASRABUDHE VINEET / GARHART JONATHAN K et al. | European Patent Office | 2017

    Free access

    Damage adaptive control

    LITWINOWICZ ANTHONY / SAHASRABUDHE VINEET / GARHART JONATHAN K et al. | European Patent Office | 2015

    Free access

    DAMAGE ADAPTIVE CONTROL

    LITWINOWICZ ANTHONY / SAHASRABUDHE VINEET / GARHART JONATHAN K et al. | European Patent Office | 2015

    Free access

    Adaptive passive vibration control

    Franchek, M.A. | Online Contents | 1996