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

Аuthors

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

Toropov Machine-Building Design Bureau "Vimpel", 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

Download