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Automation of conceptual design and modification of aircraft type unmanned aerial vehicles using multidisciplinary optimization and evolutionary algorithms. Part 1: Methods and models
Komarov V.A., Lukyanov O.E., Hoang V.H., Kurkin E.I., QuijadaPioquinto J.G.
Calculation of optimum transfers from high-elliptic orbits to geostationary orbits using a stationary plasma engine
Kvetkin A.A., Kolesov A.V.
Automation of conceptual design and modification of aircraft-type unmanned aerial vehicles using multidisciplinary optimization and evolutionary algorithms. Part 2: results and analysis
Komarov V.A., Lukyanov O.E., Hoang V., Kurkin E.I., Quijada Pioquinto J.
High fidelity modeling at early stages of airframe structural design
Boldyrev A.V., Komarov V.A.
Research of the wet condition in fuel tanks of high weight booster rockets during storage and aviation transportation periods
1 1., 1 1., 1 1.
Methodological support for the training of UAV designers and operators
Lukyanov O.E., Zolotov D.V.
Mathematical model of turbofan engine weight estimation taking into account the engine configuration and size
Avdeev S.V.
Method for optimizing mass and size characteristics of a high-pressure turbine disk
Siluyanova M.V., Grunin A.N., Alendar A.D., Kandaurov S.K.
Mathematical model for calculating the mass of a heat exchanger in problems of optimizing the parameters of the working process of aircraft gas turbine engines
Kuz'michev V.S., Omar H., Tkachenko A.Y., Bobrik A.A.
Estimation of the required thrust impulse for small spacecraft (SSC) control system with a propulsion system using fuel gas components
Titov B.A., Koltsov I.V.
Rearrangement of digital control algorithms with variable discrete pitch size
Belonogov V.D.
1 - 11 of 11 Items

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