A method of adjusting a directional movement ability in an aircraft having two or more rotors includes receiving (132) a desired thrust demand for each rotor of the two or more rotors, comparing (134) the desired thrust demands to determine a maximum thrust demand, determining (136) whether the maximum thrust demand exceeds a maximum thrust limit of the two or more rotors, and adjusting (138) each desired thrust demand based on whether the maximum thrust demand exceeds the maximum thrust limit to provide an adjusted thrust demand for each rotor of the two or more rotors. Each rotor is operated based on a respective adjusted thrust demand.


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    Title :

    METHOD FOR ADJUSTING DIRECTIONAL MOVEMENT ABILITY FOR A MULTI-ROTOR AIRCRAFT


    Additional title:

    VERFAHREN ZUR EINSTELLUNG DER RICHTUNGSBEWEGUNGSFÄHIGKEIT FÜR EIN MEHRROTORFLUGZEUG
    PROCÉDÉ DE MAINTIEN DE LA CAPACITÉ DIRECTIONNELLE D'UN AÉRONEF MULTI-ROTORS


    Contributors:

    Publication date :

    2023-07-12


    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 / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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