A.B. Skorik, A.S. Kirilyuk, O.F. Galytsky

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The questions of construction of mathematical model of contour of aiming of the zenithal guided rockets are examined in the article. An example of construction of flow diagram of contour of aiming, realizing a «classic» proportional management on the angular speed of line of distance is made. Terms at which the proportional method of aiming is considered optimum are examined. The model of kinematics link, in-use in the flow diagram of contour of aiming, realizing the modified (optimum) method of proportional rapprochement is researched.