FIELD: the invention refers to military technique and designed for guidance of a rocket against an air target and information ensuring functioning of combat outfitting of the rocket.
SUBSTANCE: the essence of the invention is in that that on the basis of initial information about an angular position and distance to the target in immediate proximity from the target the speed of approach of the rocket, the missing of the rocket, geometric sizes of the target is defined. The foreshortening of the target is also determined and a command for blowing up of the warhead of the rocket with taking into consideration the information and the initial speed of recession of fragments of the warhead of the rocket is formed, by means of an arrangement having in its composition the first key and a computer of forming the command for blowing the warhead of the rocket, whose first and the second inputs are connected correspondingly with the first and the second outputs of the information processing module, the third input - with the output of the receiver of the reflected signal. The fourth input of the computer is connected with the second output of the system of autonomous sensors, the first output is connected with the second input of the first key, whose first input is connected with the second output of the channel of antenna control. The output of the first key is connected with the first input of the power amplifier and the driving gear of the antenna, whose second input is connected with the second output of the computer of forming the command for blowing up the warhead of the rocket, whose third output is the output of the command for blowing up the warhead of the rocket.
EFFECT: increases effectiveness of combat application of the rocket at the expense of using additional information about an air target and the parameters of its moving.
16 cl, 9 dwg
