FIELD: armament.
SUBSTANCE: spin-stabilized missile (1) with an electric control actuator has electric motor (2), reduction gear (5), command driver (10), electronic power amplifier (11), feedback potentiometer (9), correcting feedback circuit and control surfaces (7). Rotor (12) of electric motor (2) is installed in stator (13) for retention in one of its extreme positions by means of magnetic forces, displacement by the value of damping relative to stator (13) and engagement in its other extreme position with additionally adjusted supports (14) fastened on frame (15) of electric motor (2).
EFFECT: improved dynamic characteristics of missile.
5 cl, 3 dwg
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