CONTROLLED MISSILE Russian patent published in 2010 - IPC F42B15/00 

FIELD: weapons and ammunition.

SUBSTANCE: missile comprises propulsion device with two nozzles installed symmetrically relative to longitudinal axis of missile at the angle to it, sensor of missile careen angle, receiver and decoder, two pairs of aerodynamic control surfaces, unit of weight compensation, two summators, two sine functional units, two cosine functional units and according links. At the same time each nozzle is equipped with controlled valve, through which it is connected to propulsion system, and additional summator is installed, the first input of which is connected to the first nozzle, and the second one - to output of missile careen angle sensor. Missile also comprises serially connected scaling unit, input of which is connected to output of weight compensation unit, additional sine functional unit, the second input of which is connected to output of additional summator, and output - to control input of the first controlled valve, and inverter, output of which is connected to control input of the second controlled valve.

EFFECT: improved manoeuvrability of missile, its speed and distance of flight.

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