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Optimization of algorithm of «air-to-surface» biposition command system trajectory control


V. I. Merkulov, D. A. Milyakov

The traditional three-point guidance method of «air-to-surface» missile to surface target was considered. The imperfections were pointed. On the basis of the mathematical apparatus of the statistical optimum control system theory a modification of biposition command radiocontrol system of missile to surface target guidance algorithm was obtained. The missile is carrier from airborne. Peculiarities of modernized algorithm work were considered. The unlimited practical marketability of modernized algorithm was marked.

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