An estimation system includes a module for measuring a current angle of attack and current flight parameters of the aircraft, a module for estimating a current lift coefficient of the aircraft from the current flight parameters and from a mass of the aircraft, a module for estimating an angle of attack for a zero lift from the current angle of attack, from the current lift coefficient and from a slope of an affine part of at least one theoretical curve describing a lift coefficient of the aircraft as a function of an angle of attack, a module for estimating the current position of the flaps of the aircraft from the angle of attack for a zero lift and a module for sending the current position of the flaps to a user device.


    Access

    Download


    Export, share and cite



    Title :

    PROCÉDÉ ET SYSTÈME D'ESTIMATION DE LA POSITION DE VOLETS D'UN AÉRONEF


    Additional title:

    METHOD AND SYSTEM FOR ESTIMATING THE POSITION OF THE FLAPS OF AN AIRCRAFT
    VERFAHREN UND SYSTEM ZUR POSITIONSABSCHÄTZUNG DER KLAPPEN EINES FLUGZEUGS


    Contributors:

    Publication date :

    2020-03-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    PROCEDE ET SYSTEME D'ESTIMATION DE LA POSITION DE VOLETS D'UN AERONEF

    SEMAT MAXIME / ANDISSAC DAVID | European Patent Office | 2019

    Free access

    Procédé d’estimation d’une empreinte environnementale pour un vol d’un aéronef et système électronique d’estimation associé

    LALUQUE LAURENT / PABIA GUILLAUME / LEGOUX PIERRE-ETIENNE | European Patent Office | 2024

    Free access


    AERONEF EQUIPE D'UN SYSTEME D'ESTIMATION DES PARAMETRES D'UN IMPACT

    GENDRE DIDIER / GOUTAUDIER DIMITRI | European Patent Office | 2020

    Free access

    AÉRONEF ÉQUIPÉ D'UN SYSTÈME D'ESTIMATION DES PARAMÈTRES D'UN IMPACT

    GENDRE DIDIER / GOUTAUDIER DIMITRI | European Patent Office | 2020

    Free access