Description: Procedure of the automated determination of value of parameters of routes of flight of airplanes (groups) is offered at overcoming of influence of opponent’s air defence system. The Pontryagin’s maximum principle is the Basis of procedure. The conduct of the guided system is described in space of system of differential equalizations. The system of homogeneous linear differential equalizations with variable coefficients is entered for the synthesis of managing influences. The condition of optimumness is formulated.
Keywords: run-time object, air defence system, airplane, route of motion, system of differential equalizations, Pontryagin’s maximum principle, condition of optimumness