Mathematical Model of the Process of Destruction of the Aircraft Guidance Missiles with Op-toelectronic System of Matrix Type
Using the theory of automation and digital image processing formulated a mathematical model of the process of destruction of the aircraft, equipped with a heat flare blocks, guided missile with a matrix optoelectronic system. The model accounts for the features selection target algorithm in the presence of noise, based on morphological analysis of images generated by the homing missiles, and significantly increases the immunity system of guidance. Defines parameters of the contour of homing missiles, which provide the minimum bias simulation of high speed air targets.