Mathematical model of anisotropic elastic-plastic material
Grechnikov F.V., Yerisov Y.A.
Determination of relative position and orientation of nanosatellites by video image analysis
Simakov S.P., Ustyugov E.V.
Application of differential evolution algorithm in the problem of aeroassisted orbital plane change maneuver
Elisov N.A., Ishkov S.A., Khramov A.A.
Aircraft engine design based on unified gas generator
Vinogradov A.S., Parovay Y.F., Mordvinov A.G., Popov D.V., Shirokov M.A.
Simulation of the process of angular rate damping of the SamSat-218D nanosatellite after separation from the launching-transporting container
Melnik M.E.
Method of production testing of electronic parts
Nasedkin A.V., Tyulevin S.V., Piganov M.N.
Visual approach to verifictaion of real-time control software
Tyugashev A.A., Bogatov A.Y., Shulyndin A.V.
Mathematical models of optimal investment control in fixed assets
Pavlov O.V., Moshkova T.A.
A parallel algorithm in the cyclic counter-sweep method for a two-dimensional domain
Loganova L.V.
Analysis of load balancing algorithms using discrete event simulation
Khayrutdinov A.R., Vostokin S.V.
Determination of a rational combination of the radial turbine basic parameters with an allowance for strength, technological and other constraints
Baturin O.V., Shabliy L.S.
Real-time control algorithms requirements verification mathematical model implementation in visual design computer-aided system
Shulyndin A.V., Tjugashev A.A.
High fidelity modeling at early stages of airframe structural design
Boldyrev A.V., Komarov V.A.
Economic-mathematical model of system of monetary stimulation of workers of the special mechanical engineering enterprise
Ivanov D.U.
Parametric function of differential backscattering in multiple scattered media
Zakharov V.P., Sindyaeva A.R.
Peculiarities of starting a spark-ignition gas fuel internal combustion engine
Shishkov V.A.
Application of convolutional codes for the protection of FPGA against single failures caused by outer space radiation effects
Nikitin A.A., Zhigulevtsev Y.N.
Development of the method of valuating the level of competitiveness of industrial enterprises working in the sphere of space-rocket engineering
Kirilina E.V.
Control of the aircraft hydraulic system technical conditions on the basis of monitoring viscidity values and purity level of fluid power
Kovalev M.A., Borodkin G.V.
SAR which parasitize the TV signals
Borisenkov A.V., Goryachkin O.V., Dolgopolov V.N., Zhengurov B.G.
Creation of infotainment support of designing of control algorithms logic of spacecraft onboard control complexeses
1 1.
Method of choosing algorithms for assessing the degree of correspondence of objects to their functional purpose with regard to their efficiency and metrological characteristics
Ryzhakov V.V., Kuznetsova M.V., Ryzhakov M.V.
Operation of an electronic system of control for spark-ignition gas fuel internal combustion engines in ignition misses
Shishkov V.A.
Mathematical model and optimization of helicopter vertical takeoff considering operational conditions and aerodynamic damping
Onushkin Y.P., Sizov D.A., Poluyakhtov V.A., Ostrovoy A.V.
Computational algorithm of forming program motion in a scheduled turn of small spacecraft
Salmin V.V., Filatov A.V., Tkachenko I.S., Tyugashev A.A., Sopchenko E.V.
Algorithm of planning operational and financial activity of a manufacturing enterprise
Bogatyryov V.D., Yesipova O.V.
Constructing the specification for the on-board realtime control algorithm
Tyugashev A.A., Bogatov A.Y.
Usage of the graphical languages in lifecycle of embedded software for spacecrafts
1 1., 1 1.
Software for investigating the process of catalytical masking layer formation
Kolpakov V.A., Bonyachuk A.A.
Method of constructing diagnostic models of aircraft hydraulic systems in an analytic form
Kovalev M.A., Borodkin G.V., Khablo I.I.
Assessment of gas turbine engine airfoil surface microstructure
Nosov N.V., Abramov A.D., Kosulin S.I.
Method of gas turbine malfunction diagnostics using hybrid intellectual systems
Antropov P.G., Dolinina O.N., Shvarts A.Y.
Adaptive algorithm of determining low altitude spacecraft orientation on the basis of processing instant diverse-type measurements
Grigoryeva M.Y., Kramlikh A.V.
Designing a seal as an element of air secondary system in aircraft engines
Vinogradov A.S.
Development of information support for the spacecraft controlalgorithm design process
1 1., 1 1.
Influence of the reliability of Earth remote sensing spacecraft onboard systems on the monitoring of imaging periodicity
Kirilin A.N., Akhmetov R.N., Kurenkov V.I., Kapitonov V.A., Stratilatov N.R., Lokhmatkin V.V.
Features of start-up the engine of internal combustion with spark ignition on gas fuel
Shishkov V.A.
Algorithms of object identification on the basis of hyperspectral Earth survey data using fuzzy linear regression
Trukhanov S.V.
Cycle parameters of an internal combustion spark-ignition gas piston engine with an electronic control system
Shishkov V.A.
Parametric modeling cog wheels in Siemens NX
Ramzaeva E.A.
Algorithm of adaptation of an electronic control system of internal combustion engines to various chemical compositions of gas fuel
Shishkov V.A.
Extrapolation of conditions of an information measuring and control system with the iterative algorithm of operation
Zelensky V.A.
Concept of construction of virtual lab for gas turbine engine testing
Rybakov V.N., Kuzmichev V.S., Tkachenko A.Y.
On-board algorithm for SamSat-218D nanosatellite orientation and stabilization system
Kramlikh A.V., Melnik M.E.
Theoretical basis of directed energy transmission pulses in stationary and moving media
Skvortsov B.V., Skvortsov D.B., Malysheva–Strojkova A.N.
Compressor blade profile reverse-engineering: building of middle curve and symmetrical profile
Shabliy L.S.
Iterative algorithm for calculation of the non-diffractive images using of the narrow spectral ring
Mukhametgaleev I.V., Khonina S.N.
Optimization of material distribution in load-bearing units for several cases of loading
Boldyrev A.V.
Computer-aided design of low-thust rocket engines using the domain-specific knowledge database and CAE / CAD systems
Ryzhkov V.V., Morozov I.I., Lapshin E.A.
Use of the methods of the structural programming to form the «reliability» diagrams of the fuel supply system of the gas turbine engines with the control elements failure order of no less than four
Smurova N.A.
Research methodology of radio electronic development of early theoretical methods in the design
Zatylkin A.V., Golushko D.A., Lysenko A.V.
Determining the angle of advance of ignition when switching from petrol to gas depending on fuel mixture burning rate
Shishkov V.A.
Implementation of FDTD-method by means of CUDA-technology
Golovashkin D.L., Malysheva S.A.
Method of improving control using a simulation object model and its application to the problem of helicopter emergency landing manoeuvre optimization
Kvokov V.N., Trushkova Y.A., Ukhin M.Y.
1 - 54 of 54 Items

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