FIELD: actuating control systems of flight vehicles, applicable in control actuators and autopilots of small-sized guided missiles. SUBSTANCE: guided missile self-sustained autopilot uses a power source and series-connected subtraction unit, non-linear element, power amplifier, actuator with a control magnet, feedback transmitter; the non-linear element is made in the form of series-connected summing element, linear amplifier-limiter and a differentiating link, whose output is connected to the output of the subtraction unit, and the output of the linear amplifier/limiter is connected to the input of the power amplifier. EFFECT: enhanced accuracy of autopilot. 3 cl, 1 dwg
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