Intellectualized Control of Self-Guidance

A problem of the self-guidance intellectualization of a flying vehicle to put itself on a maneuvering object under conditions of complicated influence of environment is considered. It is shown that if to solve the problem in a traditional way, then with sinusoidal maneuver of the object, the probability density of miss is bimodal. A method of self-guidance is developed on the basis of the object motion prediction and modified scalar evaluation of the flying vehicle state. The method provides the normal probability density of miss and acceptable precision of guidance; it is efficient with other kinds of the object maneuver.