FIELD: aviation.SUBSTANCE: group of inventions relates to a control system for controlling actuators of an aircraft, an aircraft comprising such a system, control method of executive elements of aircraft steering surface. System comprises at least one preliminary control unit and a differential force controller. Aircraft comprises at least one steering surface and two actuating elements connected to the steering surface. To implement the method, actuators are adjusted/controlled to impart overall simulated characteristics and alignment of control deviations using a differential force controller.EFFECT: providing optimum separation of power of actuators of one steering surface to each other.11 cl, 4 dwg


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    Title :

    УПРАВЛЯЮЩАЯ СИСТЕМА ДЛЯ УПРАВЛЕНИЯ ИСПОЛНИТЕЛЬНЫМИ ОРГАНАМИ ЛЕТАТЕЛЬНОГО АППАРАТА


    Publication date :

    2019-06-17


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Russian


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge