FIELD: military technology.
SUBSTANCE: invention relates to weapons, namely anti-aircraft missiles. The missile includes wings, a warhead with a fuse, control equipment with a fiber-optic gyroscope mounted on the axis of the missile, steering mechanisms and a power source. The missile design includes three fiber-optic gyroscopes mounted on three axes of the rocket, three integrators and three-channel control equipment for the steering mechanisms of the rocket separately on three channels: roll, yaw and pitch without spinning the missile around its axis.
EFFECT: increasing the accuracy of missile guidance and ensuring maximum controllability of the missile.
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