Reliability optimization for aerospace vehicle control systems using standby loaded redundancy

Аuthors

Grishin V. M.^*, Phyo M. K.^**

Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

*e-mail: Vyacheslav.Grishin@gmail.ru
**e-mail: pmgko@mail.ru

Abstract

A method is suggested to increase reliability of control systems for aerospace vehicles under various failures. This method uses optimization of redundancy structure for standby loaded redundancy and it is based on reliability optimization algorithm and non-classical weighed edge graphs.

Keywords:

reliability of control system, sudden failure, standby loaded redundancy, extremum, block reservation, optimization of redundancy structure, wave algorithm, weighed edge graph