ANALYTICAL SYNTHESIS OF THE METHOD OF TARGETING A SUPERSONIC UNMANNED AERIAL VECHICLE BASED ON MULTI-DIMENSIONAL NONLINEAR DYNAMIC MODEL per V. E. Markevich

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INCREASE OF EFFICIENCY OF SUPPRESSION OF THE ACTIVE NOISE JAMMING IN RADAR INTERCEPTION OF AIR TARGETS IN THE REVIEW MODE per V. E. Markevich

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Modified method of proportional guidance in case of the limited sector of tracking of the control object per V. E. Markevich, V. V. Legkostup

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Method for determining of the distance to the object in the hyperbolic navigation system via doppler frequency offsets per V. V. Legkostup, V. E. Markevich

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Analytical design of the missile control device to intercept aerodynamic target per V. E. Markevich, V. V. Legkostup

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Increase of the coordinate measurement accuracy in the multi-static radar in case of the receiving position placement on the aerial vehicle per V. V. Legkostup, V. E. Markevich

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Guiding a supersonic controlled object in a multi-position air basing radar per V. E. Markevich, V. V. Legkostup

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Modified method of proportional navigation to intercept aeroballistic targets with a limited sector guidance of missile per V. E. Markevich, V. V. Legkostup

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Methodology of determining of the transfer function of engagement kinematics of accelerations of an aircraft and its elliptic coordinates used for thr guidance based on time differ... per V. V. Legkostup, V. E. Markevich

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Method of Obtaining a Control Low Using a Synergetic Approach for the Problem of Aircraft Guidance Along a Hyperbola per V. V. Legkostup, V. E. Markevich, S. A. Shaban

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Procedure of the Synthesis of Control Device by the Method of Analytical Design of the Optimal Regulator for the Problem of Aircraft Guidance Along a Hyperbola per V. V. Legkostup, S. А. Shaban, V. E. Markevich

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