METHOD FOR GUIDING GUIDED MISSILE Russian patent published in 2008 - IPC F41G3/22 F41G7/30 

FIELD: weapons.

SUBSTANCE: invention refers to military techniques, and, more specifically, to the method for guiding guided missiles. Method involves measuring the distance to the target, defining target angle in a horizontal and vertical planes, direction and value of linear transversing of aiming line deviation, ranging to the target caused by maneuvering of the carrier. The method further involves moving an aiming line towards reduction of deviation with the angular speed depending on linear transversing aiming speed, initial distance to the target, linear speed of the carrier, time of movement of the carrier from input of initial distance to the target and to reaching the target by the guided missile, a target angle of the carrier in a horizontal plane, a target angle of the carrier in a vertical plane. The offered method allows to reducing stabilisation error of an aiming line by 25-30% that raises by 10-15% efficiency of shooting under conditions of action of hindrances.

EFFECT: increased efficiency of shooting under jamming conditions.