Aircraft Engineering
Аuthors
Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia
e-mail: Vyacheslav.Grishin@gmail.ru
Abstract
Faultness increase task is one of important problems of flying devises designers. Approximate analytical methods and exact numerical method of preference optimization of one class of flying devises units under active separate loaded reservation is considering in this working.Keywords:
non-failure of elements, optimization, sudden failure, active redundancy, extremum
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