The present invention discloses a method and flight controller for controlling an aircraft, comprising the following step: —determining the pitch control input δE for at least one pitch moment generator element, based on the lift control input δF for at least one lift generator element; wherein the step of determining the pitch control input δE based on the lift control input δF includes the step of determining a feed forward filter output Fq,δE,δF(q).


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Method and controller for controlling an aircraft by improved direct lift control


    Beteiligte:

    Erscheinungsdatum :

    2022-05-17


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    METHOD AND CONTROLLER FOR CONTROLLING AN AIRCRAFT BY IMPROVED DIRECT LIFT CONTROL

    GÁLFFY ANDRÁS | Europäisches Patentamt | 2019

    Freier Zugriff

    METHOD AND CONTROLLER FOR CONTROLLING AN AIRCRAFT BY IMPROVED DIRECT LIFT CONTROL

    GÁLFFY ANDRÁS | Europäisches Patentamt | 2024

    Freier Zugriff

    METHOD AND CONTROLLER FOR CONTROLLING AN AIRCRAFT BY IMPROVED DIRECT LIFT CONTROL

    GÁLFFY ANDRÁS | Europäisches Patentamt | 2020

    Freier Zugriff

    Direct-lift aircraft

    Sikorsky, I.I. | Engineering Index Backfile | 1944