Using of a priori information about the aerodynamic loading missiles for performing safety separation


Аuthors

Pravidlo M. N., Kuznetsova Y. O.*

State Machine Building Design Bureau «Vympel» by name I.I. Toropov, 90, Volokolamskoe shosse, Moscow, 125424, Russia

*e-mail: alenka_elenka@inbox.ru

Abstract

In 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


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