Using of a priori information about the aerodynamic loading missiles for performing safety separation
State Machine Building Design Bureau «Vympel» by name I.I. Toropov, 90, Volokolamskoe shosse, Moscow, 125424, Russia
AbstractIn the work is considered the algorithm design of initial signal formation on aircraft carrier which is transferred into the inertial missile control system.
Keywords:launch system; aviation guided missile; aircraft-carrier; safety separation; aerodynamic interference; relative path