Optimization of non-failure operation of one class components of aircraft control systems at the active loaded reservation
Computer Science and Control
Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia
AbstractReliability 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
mai.ru — informational site of MAI
Copyright © 1994-2020 by MAI