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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