FIELD: rocketry, aircraft air-to-surface guided missiles.
SUBSTANCE: the method consists in measurement of the parameters of target motion and own motion of the missile. Three discrete values of the target attitude and two base distances covered by the missile at a constant flight speed between the first, second and third target detections, one values of the target attitude at accomplishment of the fourth target detection and the base distance covered by the missile at a reduction of its flight speed between the third and fourth target detections are determined. The range, rate of closure of the missile to the target are determined, the missile miss and the target speed angle are determined, the target geometric dimensions are determined by target scanning relative to the second control point relative to the missile, and a command for fasting of the missile warhead relative to the third missile control point is formed. The device has series-connected antenna, receiver, signal processing module connected to the fighter equipment, and a computer of the mismatch parameters. For the same purpose the first key and the computer for forming of the command for blasting of the missile warhead are provided, the first and second inputs of the computer are connected respectively to the output of the system of independent sensors and the output of the power amplifier and antenna drive the first, second, third outputs of the computer for forming of the command for blasting of the missile warhead are connected respectively to the second input of the first key, second input of the power amplifier and antenna drive, warhead of the aircraft guided missile, the third output of the information processing module is connected to the first input of the first key, whose output is connected to the first input of the power amplifier and antenna drive, whose first and second output are mechanically linked with the antenna and the input of the computer for forming of the command for blasting of the missile warhead.
EFFECT: enhanced efficiency of the missile combat employment.
18 cl, 10 dwg
