An adaptive flight control system for controlling the pitch of blades of a propulsive propeller of a hybrid helicopter as a function of the return value of the pitch. The adaptive flight control system comprises control means supplying the pitch control order, a piloting member controlling variation of the pitch, and piloting means applying a control gain in order to transform the control order into a setpoint, and transmitting the setpoint to the piloting member. The piloting means include information return means applying a return gain that is variable to the return value of the variation of the pitch to the piloting means, also modifying the control gain as a function of the return value.


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    Title :

    SYSTÈME DE COMMANDE DE VOL ADAPTATIVE POUR LES COMMANDES DE VOL EN LACET ET DE POUSSÉE D'UN HÉLICOPTÈRE HYBRIDE


    Additional title:

    AN ADAPTIVE FLIGHT CONTROL SYSTEM FOR THE YAW AND THRUST FLIGHT CONTROLS OF A HYBRID HELICOPTER
    ADAPTIVES FLUGSTEUERUNGSSYSTEM FÜR DIE FLUGSTEUERUNGEN BEIM GIEREN UND ZUM SCHUB EINES HYBRIDHELIKOPTERS


    Contributors:

    Publication date :

    2020-04-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    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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