The article is the sequel of another one of this digest of authors “Approximate optimization solution by Pareto of discrete extremal problem of complexation of new generation avionics” and its development in the direction of creating optimization model and organization under synthesis of avionics structure. Рассмотрено приближенное оптимизационное по Парето решение дискретной экстремальной задачи комплексирования авионики нового поколения и ее развитие для создания оптимизационной модели и организации ограничений при синтезе структуры авионики. Розглянуто наближений оптимізаційний за Парето розв’язок дискретної екстремальної задачі комплексування авіоники нового покоління і її розвиток для створення оптимізаційної моделі й організації обме...
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This article describes the method for separating the regions of stability of electro-reducing valve ...
AutoCAD possibilities of 3D solid modeling are described in the article. The optimum methods of desi...
Considered are problems of joint estimation and control of high speed and highly manoeurable aircraf...
The structural model of information technology drying of printing materials, based on mathematical m...
The article provides general formulation of the problem and proves terminology base for the local go...
The article is conceded the basic aspects of influence of pedagogical directions on the forming of ...
The design schemes of electrodynamic maglev systems with a plane track structure are developed and t...
The problems of iteratively refined analytical models constructing of multilayer structures deformat...
The article analyzes the automated crushing and screening production (ACSP), as a complex multi-leve...
This article analyzes the development trends of processing Big Data tools and multi-format data stor...
Considered is the evaluation of generalized coordinates vector in the active damping problem of airc...
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This article describes the method for separating the regions of stability of electro-reducing valve ...
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Considered are problems of joint estimation and control of high speed and highly manoeurable aircraf...