Aerial navigation is disclosed. A system can detect a difference between forces applied to a plurality of ground contact points of an aerial vehicle taxiing on a ground surface. The system can determine an adjustment to a vertical component of a thrust. The thrust can be produced by at least one of a rotor or a propeller of the aerial vehicle to reduce the difference between the forces applied to the plurality of ground contact points of the aerial vehicle. The system can generate a control output to cause the at least one of the rotor or the propeller to adjust the vertical component of the thrust to reduce the difference between the forces.


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    Titel :

    THRUST CONTROL FOR GROUND NAVIGATION OF AERIAL VEHICLES


    Beteiligte:
    GEIGER DEREK H (Autor:in) / FELL WILLIAM C (Autor:in) / FAYNBERG ALEX (Autor:in) / KUBIK STEPHEN T (Autor:in) / FRADKIN AARON JOSHUA (Autor:in)

    Erscheinungsdatum :

    10.07.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G01P MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION OR SHOCK , Messen der Linear- oder Winkelgeschwindigkeit, der Beschleunigung, der Verzögerung oder des Stoßes / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / B64C AEROPLANES , Flugzeuge



    THRUST CONTROL FOR GROUND NAVIGATION OF AERIAL VEHICLES

    GEIGER DEREK H / FELL WILLIAM C / FAYNBERG ALEX et al. | Europäisches Patentamt | 2025

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