METHOD FOR FUNCTIONING OF MISSILE INFORMATION-COMPUTER SYSTEM AND DEVICE FOR ITS REALIZATION Russian patent published in 2005 - IPC

FIELD: aircraft guided missiles.

SUBSTANCE: on the basis of the source information on the target attitude and range to it, the rate of missile closure, geometrical dimensions of the target, miss of the missile are determined in the immediate proximity from it, and a command is formed for blasting the missile warhead on the basis of this information with due account made for the initial speed of scattering of the missile warhead fragments. The method is realized by a device, having a key and a computer forming the command for blasting the missile warhead, whose first and second inputs are connected respectively to the first and second outputs of the information processing module, the third input is connected to the output of the reflected signal receiver, the first output is connected to the second input of the key, whose first input is connected to the second output of the antenna control channel, and the key output is connected to the first input of the power amplifier and antenna drive, whose second input is connected to second output of the amplifier forming the command for blasting the missile warhead, whose third output serves as the output of the command for blasting the missile warhead.

EFFECT: enhanced functional potentialities of guidance due to informational support of functioning of the fighting equipment.

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