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.


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    Title :

    PITCH FEEDBACK CONTROL SPLITTING FOR HELICOPTERS


    Additional title:

    NEIGUNGSRÜCKKOPPLUNGSTEUERUNGSTEILUNG FÜR HUBSCHRAUBER
    DIVISON DE COMMANDE DE RÉTROACTION DE TANGAGE POUR HÉLICOPTÈRES


    Contributors:

    Publication date :

    2017-08-30


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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