A rotatable thruster aircraft includes an airframe, which includes an aircraft body and a fixed wing; rotatable thruster assemblies, each including first and second thrusters that provide rotation via differential thrust; a rotatable shaft with torsional flexibility; an inertial measurement unit; optionally vertical lift thrusters; and an aircraft control unit, including a processor, a non-transitory memory, an input/output component, and a power manager that controls specific power applied to the thrusters.


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    Title :

    Rotatable thruster aircraft


    Contributors:

    Publication date :

    2021-12-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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