According to one aspect, a method of initial rotor state compensation for a rotorcraft includes determining a vehicle attitude of the rotorcraft prior to takeoff of the rotorcraft. A rotor state compensation is computed based on the vehicle attitude. A plurality of rotor servos is commanded to an initial rotor state based on a nominal rotor neutral position value in combination with the rotor state compensation to establish a predetermined takeoff trajectory of the rotorcraft.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Initial rotor state compensation for a rotorcraft


    Beteiligte:

    Erscheinungsdatum :

    16.07.2019


    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



    INITIAL ROTOR STATE COMPENSATION FOR A ROTORCRAFT

    CHEREPINSKY IGOR / DRISCOLL JOSEPH T | Europäisches Patentamt | 2017

    Freier Zugriff

    INITIAL ROTOR STATE COMPENSATION FOR A ROTORCRAFT

    CHEREPINSKY IGOR / DRISCOLL JOSEPH T | Europäisches Patentamt | 2016

    Freier Zugriff

    Beam for a rotorcraft rotor and rotorcraft rotor

    BÜSING MORITZ | Europäisches Patentamt | 2015

    Freier Zugriff

    Beam for a rotorcraft rotor and rotorcraft rotor

    BUESING MORITZ | Europäisches Patentamt | 2019

    Freier Zugriff

    Beam for a rotorcraft rotor and rotorcraft rotor

    MORITZ BUSING | Europäisches Patentamt | 2015

    Freier Zugriff