A commanded control signal is compared against an adaptive control signal in order to detect a rotor strike by a rotor included in an aircraft, wherein the adaptive control signal is associated with controlling the rotor and the adaptive control signal varies based at least in part on the commanded control signal and state information associated with the rotor. In response to detecting the rotor strike, a control signal to the rotor is adjusted in order to reduce a striking force associated with the rotor.


    Access

    Download


    Export, share and cite



    Title :

    ROTOR STRIKE DETECTION AND FORCE REDUCTION


    Additional title:

    ROTORSCHLAG ERKENNUNG UND KRAFTREDUZIERUNG
    DÉTECTION DE FRAPPE DE ROTOR ET RÉDUCTION DE FORCE


    Contributors:

    Publication date :

    2025-03-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



    ROTOR STRIKE DETECTION AND FORCE REDUCTION

    SAUNDERS CHRISTOPHER SCOTT | European Patent Office | 2025

    Free access

    Qatar's new strike force

    Online Contents | 1997


    BIRD STRIKE SIMULATION FOR HELICOPTER ROTOR BLADES

    Surana, M.M. / Tho, C.-H. / Smith, M.R. et al. | British Library Conference Proceedings | 2013



    AIRCRAFT BIRD STRIKE REDUCTION DEVICE

    PETKAR KIRTI / SUBRAMANIAN SESHA / KRAY NICHOLAS J | European Patent Office | 2023

    Free access