FIELD: weapons and ammunition.
SUBSTANCE: invention relates to weapons, in particular, to systems of fire destruction of objects with controlled ammunition. Method of target destruction by controlled ammunition in complicated target environment consists in determination of spatial coordinates of target location area, using a matrix of geo-information parameters of the image of the region of location of the target and based on the formation of a binary matrix of geo-information parameters of the image of the region of the location of the target with a threshold of binarisation excluding regions from analysis of the image of the region of location of the target, where target by its tactical-physical properties can not be located, making values of binary matrix of geo-information parameters of image of location area of target in onboard computer of controlled ammunition, execution of controlled ammunition launching and its output to area of target location, making from the controlled shot side a portion of the target location area, forming an image frame parameter matrix of the area of the target location area for the j-th time moment and transmitting its values to the on-board computer of the controlled ammunition, where is the current time instantaneous number, N is number of time points, onboard of controlled ammunition determining coordinates of its location for j-th moment of time and spatial parameters of shooting section of area of target location for j-th time moment, transmitting their values to an on-board computer of the controlled ammunition and forming an element of a binary matrix of geo-information frame parameter parameters of the area of the location region for the j-th time moment, forming an image frame parameter convolution matrix of the target location area section for the j-th time moment by multiplying the image frame matrix values of the target location area section for the j-th time moment and the binary matrix element of the image frame geo-information frame parameters of the target location area section for the j-th time moment, implementation of the processing of the values of the convolution matrix of image frame parameters of the target location area section for the j-th time moment and based on its result selection of target parameters and correction of the guided missile flight to the target, repetition of procedures for j+1-th moment of time from formation of parameters matrix of image frame of target location area section before processing of values of matrix of convolution of parameters of image frame of section of area of location of target for j+1-th moment of time and by result of selection of parameters of target and correction CA flight to target.
EFFECT: disclosed is method of target destruction with controlled ammunition.
1 cl, 2 dwg
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Authors
Dates
2020-04-23—Published
2019-07-09—Filed