Optimization of non-failure operation of one class components of aircraft control systems at the active loaded reservation

Computer Science and Control


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

Reliability enchancement is one of the important problems, which aircraft control system designers are needed to solve. An approximate analytical technique and a numerical one are suggested to optimize some class of aircraft control system units basing on active redundancy approach.

Keywords:

non-failure control systems; optimization; sudden failure; active redundancy; extremum; modularredundancy

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