Mathematical modeling of the adaptive closed-loop system of forced separation of loads

Aviation technics and technology


Аuthors

Belyaev A. N.

Toropov Machine-Building Design Bureau "Vimpel", 90, Volokolamskoe shosse, Moscow, 125424, Russia

e-mail: Alex_JC@mail.ru

Abstract

It is developed the mathematical model of functioning of the autonomous adaptive system on forced separation with feedback for the pusher moving speed which don’t require the information about acing outer forces at the aviation load. It is analyzed the influence of pyrotechnic device type on the moving parameters of separated aviation load.

Keywords:

aircraft armament installation; adaptive system of forced separation; closed system; feedback; linear acceleration transducer; separation load safety from aircraft


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