A method and system for providing corrective action to a rotorcraft experiencing motor failure is provided. Included in the method and system are embodiments that receive feedback from sensors directed at measuring a state of motors used to provide lift to the rotorcraft. The method and system also describe embodiments for determining that there is a malfunctioning motor, and furthermore, the appropriate corrective action for responding to the malfunctioning motor. In some embodiments, the method and system are configured to reduce power to the malfunctioning motor while simultaneously adjusting power supplied to the remaining motors such that changes in total thrust and net torque are minimized.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Integrated feedback to flight controller


    Beteiligte:
    MISFELDT ANSEL (Autor:in)

    Erscheinungsdatum :

    11.08.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



    INTEGRATED FEEDBACK TO FLIGHT CONTROLLER

    MISFELDT ANSEL | Europäisches Patentamt | 2018

    Freier Zugriff

    Integrated flight controller for light aircraft

    Olcott, J. W. / Ellis, D. R. / Seckel, E. | NTRS | 1972



    Droneboarding Tow Bar With Integrated Flight Controller

    HENRY DAVID EDWARD | Europäisches Patentamt | 2020

    Freier Zugriff