A method for compensating disturbances in an aerial vehicle having a plurality of thrusters, the disturbances caused by a payload rotating about one or more axes and coupled to the aerial vehicle, the method including the steps of determining aerial vehicle parameters; determining payload parameters comprising physical parameters and dynamic parameters; determining a preferred orientation of the aerial vehicle based on the aerial vehicle parameters and operational instructions; determining a corrective input based on aerial vehicle parameters, payload parameters, and actual orientation feedback; determining an operation of one or more of the plurality of thrusters based on the corrective input and the preferred orientation, then controlling an output of one or more of the plurality of thrusters accordingly; and determining an actual orientation of the aerial vehicle and generating the actual orientation feedback.


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    Titel :

    SYSTEM FOR COMPENSATING AERIAL VEHICLE ATTITUDE DISTURBANCES


    Beteiligte:
    THOMAS JUSTIN (Autor:in)

    Erscheinungsdatum :

    02.09.2021


    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



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