A separated lift-thrust (SLT) aircraft includes a longitudinal-thrust engine and articulated electric rotors, at least some of which are variable-position rotors having variable orientations based on rotor position signals. Control circuitry independently controls thrust of the longitudinal-thrust engine and the thrust and orientation of each of the variable-position rotors, relative to the aircraft lifting surface and longitudinal thrust engine, to provide for commanded thrust-vectoring maneuvering of the aircraft during VTOL, fixed wing flight, and intermediate transitional states, including maintenance of a desired pose of the lifting surface independent of orientation of the rotor orientations when hovering the aircraft in windy conditions. A flight and navigation control system automates flight maneuvers and maintains desired aircraft pose and position relative to static or dynamic coordinates during station keeping, tracking, avoidance, or convergence maneuvers.


    Access

    Download


    Export, share and cite



    Title :

    SEPARATED LIFT-THRUST VTOL AIRCRAFT WITH ARTICULATED ROTORS


    Contributors:

    Publication date :

    2021-04-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    Separated lift-thrust VTOL aircraft with articulated rotors

    BAITY SEAN MARSHALL / MILLER STEPHEN W | European Patent Office | 2024

    Free access

    Separated lift-thrust VTOL aircraft with articulated rotors

    BAITY SEAN MARSHALL / MILLER STEPHEN W | European Patent Office | 2024

    Free access

    SEPARATED LIFT-THRUST VTOL AIRCRAFT WITH ARTICULATED ROTORS

    BAITY SEAN MARSHALL / MILLER STEPHEN W | European Patent Office | 2021

    Free access

    SEPARATED LIFT-THRUST VTOL AIRCRAFT WITH ARTICULATED ROTORS

    BAITY SEAN MARSHALL / MILLER STEPHEN W | European Patent Office | 2021

    Free access

    SEPARATED LIFT-THRUST VTOL AIRCRAFT WITH ARTICULATED ROTORS

    BAITY SEAN MARSHALL / MILLER STEPHEN W | European Patent Office | 2022

    Free access