A gust compensation system is configured to adaptively reduce gust loads exerted into an aircraft. The gust compensation system may include a first sensor proximate to a front of the aircraft. The first sensor is configured to output a first signal. A second sensor may be distally located from the front of the aircraft. The second sensor is configured to output a second signal. A gust signal sub-system is configured to receive the first and second signals and generate a gust signal based on analysis of the first and second signals. The gust signal sub-system outputs the gust signal and may modify a load parameter signal in response to the gust signal exceeding a load alleviation threshold.


    Access

    Download


    Export, share and cite



    Title :

    Gust compensation system and method for aircraft



    Publication date :

    2017-05-02


    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



    GUST COMPENSATION SYSTEM AND METHOD FOR AIRCRAFT

    ABDEL-MOTAGALY KHALED / CAICEDO RAFAEL E / DALLARA CHRISTOPHER D et al. | European Patent Office | 2021

    Free access

    GUST COMPENSATION SYSTEM AND METHOD FOR AIRCRAFT

    European Patent Office | 2023

    Free access

    GUST COMPENSATION SYSTEM AND METHOD FOR AIRCRAFT

    ABDEL-MOTAGALY KHALED / CAICEDO RAFAEL E / DALLARA CHRISTOPHER D et al. | European Patent Office | 2016

    Free access

    GUST COMPENSATION SYSTEM AND METHOD FOR AIRCRAFT

    KHALED ABDEL-MOTAGALY / RAFAEL E CAICEDO / CHRISTOPHER D DALLARA et al. | European Patent Office | 2017

    Free access

    GUST COMPENSATION SYSTEM AND METHOD FOR AIRCRAFT

    ABDEL MOTAGALY KHALED / CAICEDO RAFAEL E / DALLARA CHRISTOPHER D et al. | European Patent Office | 2016

    Free access