Embodiments are directed to generating, by a processing device, a feedback command for an aircraft based on a reference input and an output response of the aircraft, and analyzing, by the processing device, the feedback command to allocate control to a plurality of control surfaces over a plurality of separate frequency bands.


    Access

    Download


    Export, share and cite



    Title :

    Pitch feedback control splitting for helicopters with redundant actuators


    Contributors:

    Publication date :

    2016-04-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / B64C AEROPLANES , Flugzeuge



    PITCH FEEDBACK CONTROL SPLITTING FOR HELICOPTERS WITH REDUNDANT ACTUATORS

    GREENFIELD AARON L / WULFF OLE / WHITE MATTHEW A | European Patent Office | 2015

    Free access

    PITCH FEEDBACK CONTROL SPLITTING FOR HELICOPTERS

    GREENFIELD AARON L / WULFF OLE / WHITE MATTHEW A | European Patent Office | 2017

    Free access

    PITCH FEEDBACK CONTROL SPLITTING FOR HELICOPTERS

    GREENFIELD AARON L / WULFF OLE / WHITE MATTHEW A | European Patent Office | 2015

    Free access

    ADJUSTABLE PITCH PROPELLER OR GTE FAN WITH REDUNDANT ACTUATORS.

    GRICE CHRISTOPHER | European Patent Office | 2020

    Free access