SOLUTION OF TASK OPTIMAL PLANNING OF AIR DEFENSE MEANS AGAINST LOW-ALTITUDE AIR TARGETS

The article examines the methods of their destruction by air defense systems, taking into account the low-altitude operation of various types of air attack weapons fighter airplane, helicopter, cruise missile, reconnaissance unmanned aerial vehicles and armed unmanned aerial vehicles. For this purpose, taking into account the tactical and technical characteristics of low-altitude air attack weapons, efficiency coefficients were determined using methods of destruction by specially selected anti-aircraft missile systems. To solve the problem S-125 2TM, BUK-MB, BARAK-8, S-300 PMU2, TOR-M2KM, PATRIOT MIM-104, PANSIR S-1, NASAMS-III against low-altitude air attack weapons such as fighter airplane, helicopter, cruise missile, reconnaissance unmanned aerial vehicles and armed unmanned aerial vehicles by applying the method Gomori modified variant of the Simplex method is solved. As a result, it was possible to determine the maximum and minimum number of destroyed low-altitude air targets. Maximum 86 % and minimum 78 % of air targets operating at low altitude of this conventional enemy. These results can be used in optimal planning of the use of air defense systems against air attack systems operating at low altitude during combat operations.