FIELD: flying vehicle control and stabilization systems; guided missiles. SUBSTANCE: in guidance on target, phase shift introduced by on-board actuators at rocket rotational frequency are measured and input signal vector is turned through angle opposite to that being measured. Two-axis self-adaptive autopilot includes gyro position indicator and two actuator units; it is additionally provided with phase shifter, integrator, four ripple filters of second order, cosine non-linear converter, adder, two standard signal production units and four amplitude limiters. EFFECT: enhanced stabilization of rocket in the course of guidance. 1 dwg
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