A method for controlling a rotary wing aircraft includes determining a measured airspeed of the rotary wing aircraft based on data from a pitot probe, determining an estimated airspeed of the rotary wing aircraft based on rotor control commands, and determining a blended airspeed based on both the measured airspeed and the estimated airspeed.


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    Titel :

    BLENDED AIRSPEED TECHNIQUE FOR HELICOPTER CONTROL AT LOW AIRSPEEDS


    Beteiligte:
    MONAHAN JAY BENJAMIN (Autor:in) / ELLER EREZ (Autor:in)

    Erscheinungsdatum :

    2024-01-11


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G01P MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION OR SHOCK , Messen der Linear- oder Winkelgeschwindigkeit, der Beschleunigung, der Verzögerung oder des Stoßes




    Helicopter Airspeed System Investigations

    J. R. Melton / J. A. Johnston | NTIS | 1962


    Structural Design Airspeeds

    Lomax, Ted L. | AIAA | 1996


    A starting system for measuring low airspeeds of a single-rotor helicopter

    Nikitin, A. V. / Soldatkin, V. V. | Online Contents | 2012


    A starting system for measuring low airspeeds of a single-rotor helicopter

    Nikitin, A. V. / Soldatkin, V. V. | Springer Verlag | 2012