FIELD: aircrafts.SUBSTANCE: automatic control system of the unmanned aerial vehicle along the yaw angle contains a regulator, an actuator, six amplifiers, yaw angle sensor, angular velocity sensor, two adders, differentiator, integrator, connected in a certain way.EFFECT: increase in the stability margin, the desired quality of transient processes and system astatism is provided.1 cl, 1 dwg


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    Title :

    Система автоматического управления беспилотным летательным аппаратом по углу рыскания


    Publication date :

    2018-05-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Russian


    Classification :

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