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Estimation of mass-dimensional characteristics of a complex propulsion unit of earth remote sensing spacecraft
Kurenkov V.I., Kucherov A.S., Yakishik A.A.
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.
Motion control system of multicopter
Sitnikov D.V., Burian Y.A., Russkih G.S.
Development of a calculation method for control system of radial clearance in the turbine of gas turbine engine
Bondarchuk P.V., Tisarev A.Y., Lavrushin M.V.
Fluctuations of pressure in rail gas injection of engines with spark ignition
Shishkov V.A.
The process of creating the system of multi-level continuous vocational training of specialists
Stolbov V.I.
Research and optimization of parameters of a system controlling the process of tube inside surface coating
Skvortsov B.V., Zaretskaya M.I., Kurylyova P.A.
Effect of radial location of nozzles on width on performance of pre-swirl systems
Didenko R.A., Karelin D.V., Ievlev D.G., Lebedev V.V.
Designing a seal as an element of air secondary system in aircraft engines
Vinogradov A.S.
Economic-mathematical model of system of monetary stimulation of workers of the special mechanical engineering enterprise
Ivanov D.U.
Optimal designing of precision small-size non-platform inertial navigation systems for highly manoeuvrable moving objects
Voditcheva L.V., Belsky L.N., Maslova O.N., Lukin N.A.
Selection of new heat-resistant nickel alloys for advanced aviation engines
1 1., 1 1., 1 1., 1 1., 1 1.
About the thermal protection of the oil cavities for designing gas turbine engines
Tryanov A.Y., Grishanov O.A., Vinogradov A.S.
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.
Modelling the architecture of a system controlling the condition of maintenance objects
Koptev A.N., Yergaliyev D.S., Sakhanov K.Z.
Improvements in methods of analysis and control of space-rocket equipment reliability at the stage of complex electrical testing
Belova V.V.
Parametrical design of discrete mapping of Van der Pol oscillator
Zaitsev V.V., Nuraev D.B., Yudin A.N.
Influence of space vehicle remote power supply on thermal regimes of solar batteries
Steganov G.B., Beznyakov A.M., Nemirov A.V.
Optimal command control of flight paths of aerospace system hypersonic first stage in conditions of atmospheric disturbances
Krikunov M.M.
Model of a queueing system with non-stationary streams and partial mutual assistance between channels
Romanenko V.A.
Method of constructing diagnostic models of aircraft hydraulic systems in an analytic form
Kovalev M.A., Borodkin G.V., Khablo I.I.
Heat meter for AKSUE, integrated into management information system TP of the industrial enterprise
Biryuk V.V., Leonovich G.I., Livochkina N.A.
Experimental and theoretical research of continuous motion of rotor on anisotropic gapped elastic support
Nikiforov A.N., Panovko G.Y., Shokhin A.Y.
Development of methods for ensuring energy balance for the operation of mission equipment of “AIST”-series small satellites under conditions of power limitations
Ivanushkin M.A., Salmin V.V., Tkachenko S.I., Tkachenko I.S., Volgin S.S.
Arrangement of data for the formation of a multidimensional array of essential insights in automated enterprise management system
Kartamyshev A.S.
Estimation of functional efficiency of the air transport service system at a regional airport terminal
Koltsov I.V., Romanenko V.A.
Morphological characteristics of the intermetallic phase of heat resisting nickel alloys
Kirikov S.V., Perevezentsev V.N., Tarasenko Y.P.
Analysis of motion stability of a deployed space tether system with an atmospheric probe
Zhe D., Zabolotnov Y.M., Changqing W.
Analysis of the influence of the scheme of flight of the stage with a reactive recovry system on the energy characteristics of a two-stage medium class launch vehicle
Kuznetsov U.L., Ukraintsev D.S.
Nominal motion control program in a supersonic carrier aircraft
Balakin V.L., Potapov V.I.
Development of a multiparameter model of an optimum coherent system of incentives for workers of aircraft construction enterpricses
Ivanov D.Y.
Vortex cleaning of fuel tank pressurant gas
Biryuk V.V., Shimanov A.A., Onoprienko D.A., Smorodin A.V., Shepelev A.I.
Choosing the law of distributing request input flow in the modeling of a trade enterprise queuing system
Duplyakin V.M., Knyazheva Y.V.
Synthesis of dynamic modes of attitude motion of spacecraft with solid propellant rocket engine
Balakin V.L., Doroshin A.V., Krikunov M.M.
Resources management and planning of product realization in ERP “1C” and MES “Sprut” (ERP: Enterprise Resource Planning; MES: Manufacturing Execution System)
Abramova I., Lisitsin M.S., Abramov D.A.
Classification of models of basic links in the air transport sector in the context of the process of macrologistic system formation and development
Pakhomov A.A.
Analysis and ballistic design of a medium-caliber system with an attached camera of accelerating
Safronov A.I., Azovsky V.M., Zorkin V.A., Chirkunova N.V.
The machine and methods of tribotehnical tests of materials
Ibatullin I.D., Zhuravlev A.N., Utjankin A.V., Galljamov A.R., Neyaglova R.R.
Algorithm of adaptation of an electronic control system of internal combustion engines to various chemical compositions of gas fuel
Shishkov V.A.
Kick-stage control by navigational data of satellite navigation system
1 1.
Tooling system of express assessment of explosive military equipment objects after hitling effects
1 1., 1 1.
Extrapolation of conditions of an information measuring and control system with the iterative algorithm of operation
Zelensky V.A.
Development of advanced low thrust rocket engines with ecologically friendly propellants
1 1., 1 1., 1 1.
The integrated information model architecture for working out, manufacture and operation GTE together with its system of automatic control, the control and diagnostics
Kulikov G.G., Rizvanov K.A., Denisova S.S.
Development of the finite element model of vibroacoustical characteristics of pipe system
Mironova T.B., Prokofiev A.B., Shahmatov E.V.
Computer-aided-design system for calculating adsorption thermodynamic characteristics
Zelenko L.S., Varfolomeyeva V.V., Kuznetsov V.Y., Fed’kayev A.V., Terentyev A.V., Buryak A.K.
Verifying models of mechatronic systems «man-centrifuge» for ground and space usage on the basis of set theory
Anshakov G.P., Akulov V.A., Balakin V.L.
Multilevel system of Earth operational hyperspectral monitoring
Anshakov G.P., Egorov A.S., Raschupkin A.V., Skirmunt V.K.
Experimental studies of the components of high-frequency ion engine RD0310
Kazbanov A.A., Dronov P.A., Spivak O.O., Derkachev A.B.
Method of preliminary solution of the problem of space robot navigation by onboard astronomical measurements using the butterworth filter
Ananenko V.M., Golyakov A.D., Kalabin P.V.
Problem of optimization of the number of processors in distributed processing
Pavlov P.A.
Internal combustion engine some cooling system components detailed calculation
Kolomin I.V., Ajukov A.A., Birjuk V.V.
Problems of modern aircraft maintenance
Kovalev M.A., Poddubniy I.V.
Оptimization of gas turbine aircraft engine control throughout the engine service life
Gurevich O.S., Golberg F.D., Smetanin S.A., Trifonov M.E.
Rotor-pendulum self-synchronization of parametrical vibration generators on an isotropic elastic foundation
Koshelev A.V., Dentsov N.N.
Peculiarities of using additional low-power energy sources in the power supply system of small spacecraft
Kargu D.L., Beznyakov A.M., Nemirov A.V., Radionov N.V., Chudnovsky Y.A.
Analysis of heat transfer in a helically coiled cooler of a mechatronic sample conditioning system
Gimadiev A.G., Utkin A.V.
Metodological basis of the development of a problem-oriented system for selecting design parameters of space vehicles
Stratilatov N.R., Kurenkov V.I., Kucherov A.S., Yakishik A.A.
Modeling orbital tether system deployment with limitations on the deployment speed
Ishkov S.A., Filippov G.A., Xiaoye X.
Study of characteristics of the vortex throttling valve for the sysytem of water sample conditioning
Gimadiev A.G., Utkin A.V.
Computer-aided design of aircraft gas turbine engines and selection of materials for their main parts
Akhmedzyanov D.A., Kishalov A.E., Markina K.V.
Method of gas turbine malfunction diagnostics using hybrid intellectual systems
Antropov P.G., Dolinina O.N., Shvarts A.Y.
Models of discrete multycriterion optimization for hierarchical systems of corporations
Geraskin M.I.
Measurability of knowledge and competences in studying humanities
Ryabinova E.N., Titov B.A., Pavlova I.O.
The formation of the contoured surface roughness level of optical purity by using a CNC machine
Abulkhanov S.R., Sazonov M.B.
Dynamic process modeling of aircraft engine control system
Blyumin K.V.
Calculating maximum amplitude in an oscillatory system with many-valued perturbation
Lepilov A.N.
Using statistical Markov models for the analysis of electromagnetic compatibility of autonomous electric installations
Kubarkov Y.P., Goldshtein V.G., Inahodova L.M.
Task-oriented systems in the problems of spacecrafts designing
1 1., 1 1., 1 1., 1 1.
Choosing the structure of power-supply systems for low-orbit space vehicles
1 1., 1 1., 1 1., 1 1.
History of small space vehicle progress and development at Plesetsk cosmodrome. Current problems of further development
Korotkov V.V., Vinogradov A.V.
Hydrodynamic rinsing of hydrofuel system’ unflowing units
1 1.
Research of a seal work as an element of the air engine support
Vinogradov A.S., Rempel A.P.
Action of random vibration on non-linear dry friction damping system
Ulanov A.M., Parovay F.V.
Software for investigating the process of catalytical masking layer formation
Kolpakov V.A., Bonyachuk A.A.
Deployment and stabilization of the motion of a space tethered system in a lunar orbit
Ledkova T.A., Zabolotnov Y.M.
Mathematical model of the “tank – nozzle” cooling system
Shalay V.V., Shcherban K.V.
Methods of validation of the ballistic structure of space surveillance system orbital segment
Fadin I.A., Yanov S.V., Samokhvalov O.A.
Preliminary tests of tank with cryogenic charging for onboard throttle system of cooling
Dovgjallo A.I., Sarmin D.V., Uglanov D.A.
Using of resonance oscillations in intake system for a car noise tuning
Starobinski R.N., Mescheriakova M.A., Nazarov A.G., Sokolov A.V.
Dynamics of a dual-mass resonant vibration screen in a first approximation
Dentsov N.N., Koshelev A.V.
Investigation of the thermal regime of microsatellite optoelectronic telescopic complex under operating conditions
Tsaplin S.V., Bolychev S.A.
Mathematical modelling of the working process of a hot gas pressure feed system
Salich V.L.
Analysis of the accuracy of Earth remote sensing satellite angular motion control and track guidance during route observation intervals
Galkina A.S., Platoshin I.V.
Optimal stabilization of small spacecraft angular motion in the process of deployment of an orbital tether system
Zabolotnov Y.M., Lobankov A.A.
Optimization of spatial turns of «AIST-2» small spacecraft on the basis of the principle of minimum control
Petrishchev V.F., Shipov M.G.
Determination of thermal state and modification of the flame tube cooling system with the help of three-dimensional modeling methods
Matveev S.G., Anisimov V.M., Zubrilin I.A., Kolomzarov O.V., Mironov N.S.
Concept of multilevel adaptation of integrated navigation systems of small spacecraft
Fominov I.V.
Cycle parameters of an internal combustion spark-ignition gas piston engine with an electronic control system
Shishkov V.A.
Mechanism for the development of an organization process control system
Gerasimov K.B.
Modeling oil separation in the impeller of a radial-type centrifugal breather
Petrukhin A.G., Tryanov A.E.
Building a diagnosis face gas dynamic seals
Falaleev S.V., Vinogradov I.S., Midyukin V.V.
Additive technology application details of combustion
Balyakin A.V., Smelov V.G., Chempinskiy L.A.
Computer-aided design of programs for CAM-systems based on the use of intelligent pattern mechanical processing of standard elements
Popovich A.V., Levschanov V.V., Lisov K.A., Chavkin E.M.
Gas-discharge generation of near-wall flows
Ivchenko A.V., Zhuravliov O.A., Shakhov V.G.
Simulation and research of factors affecting aerodynamic indices of the gas purification process
Usmanova R.R., Zhernakov V.S.
Problems of simulation and calculation of modes of electrical engineering complexes and off-line systems of electrical power supply
Kubarkov Y.P., Goldshtein V.G., Amelin S.V.
Analysis of possibility of residual propellant utilization in Soyuz orbital stage for controllable descent
1 1., 1 1., 1 1., 1 1.
Control programs and motion trajectories of hypersonic first stage of an aerospace system
1 1.
Chaotic motion of the elastic tether system
Aslanov V.S., Pirozhenko A.V., Ivanov B.V., Ledkov A.S.
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