Matrix model of elastic systems of start

Аuthors

Tverdokhleb A. A.

Research production association «Dinafors», 1/21, Stari Petrovsko-Razumovsky proezd, Moscow, 127287, Russia

e-mail: vtverd@yandex.ru

Abstract

The generalised model of systems of start of aviation means of defeat in a kind of the universal matrix model allowing uniformly to describe elastic of property of a launcher at modelling of process of start of aviation means of defeat is developed. Features and properties of matrixes of the rigidity are thus investigated, allowing to carry out their transformations, necessary removals at modelling or imposings of additional mechanical communications, and the technique of definition of factors of matrixes of rigidity with use of a method of static calculation of designs is developed.

Keywords:

саtapult chair; launcher system;means of defeat; matrix model

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