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Assessment of the possibility of shortening the landing distance of maneuverable aircraft
Strelets M.Y., Tarasov A.Z., Grishin I.A.
The relevance of introducing a requirements management system in the production process of the aircraft engine construction industry
Malinovskiy I.M., Starodumov A.V., Myagkov K.A., Yusipov B.K.
Methodology of designing a space transport system including a “DM” chemical upper stage and an electric rocket transport module
Russkikh A.S., Salmin V.V.
Analysis and improvement of characteristics of power supply systems for the small space vehicle of the AIST-2 type
Mordanov M.R., Safronov S.L.
Application of decision support technology at various stages of the life cycle of space facilities in assembly with the information system of technical condition and reliability
Avtamonov P.N., Bakhmut A.D., Krylov A.V., Okhtilev M.Y., Okhtilev P.A., Sokolov B.V.
The analyze of work of throttle cooling system’s microheat exchanger, wich uses nitrogen with nearly critical parameters
1 1., 1 1., 1 1., 1 1.
Optimization of the parameters of a ground speed meter of low-flying aircraft based on the application of the theory of optimal filtration
Ivanov M.E., Yezerskiy V.V.
Scalable distributed systems of competitive interacting processes and their optimality
1 1.
Methodology of delivering space parts, tools and accessories to a near Earth orbital station on the basis of the reliability factor
Zheleznov I.V., Uperchuk R.A., Eroshenko V.K.
Automated system for measuring geometric parameters of turbine blades in production conditions
Aleksentsev E.I., Shavrin P.A., Fedoseev O.B.
Automated thermovacuum firing test facility for testing and research of workflow in low-thrust rocket engine on hypergolic propellants
Galperin R.N., Ivashin Y.S., Nigodjuk V.E., Ryzhkov V.V., Sulinov A.V.
Seal designing as element of aircraft engine systems and engine units
Vinogradov A.S.
Investigation of the dynamic characteristics of the pneumatic-mechanical drive of the installation movements of machine mechanisms
Prikhodko S.P., Sidorenko V.S., Korotych D.A.
Reduction of angular velocities of AIST-2D spacecraft using a system of kinetic moment dumping
Shipov M.G.
Models and methods of corporation management in case of inter-corporation interaction
Geraskin M.I.
Results of primary operation of NK-37 engine low emission combustion system
Bantikov D.Y., Yeliseev Y.S., Lavrov V.N., Pchelyakov A.A., Fedorchenko D.G., Tsybizov Y.I.
Method of controllung the angular position of IO ASD relative to the system of coordinates of a gyrostabilized platform
Degtyarev M.S.
Model of knowledge in the expert system of aid to the crew
Vorontsov A.A.
Onboard digital computer systems of the «Malachite» family for extreme conditions
Antimirov V.M., Umansky A.B., Shalimov L.N.
Experimental analysis of instability and self-oscillations in an electrohydraulic servo drive
Petrov P.V., Sunarchin R.A., Mashkov M.A., Krivosheev N.S.
Multi-position control of movements of large-sized structural elements during static loading using a laser tracker
Sazonnikova N.A., Uklein R.V.
Cycle air heating system of gas pumping unit NEVA-25NK
1 1., 1 1., 1 1., 1 1.
Verification of aero-engine numerical rotor models based on virtual static structural and modal tests
Shaposhnikov K.V., Degtyarev S.A., Leontiev M.K., Anisimov S.V.
Development of an experimental plant and a numerical model of an axial magnetic rotor suspension
Benedyuk M.A., Lomachev A.O., Badykov R.R., Bezborodova K.V., Yurtaev A.A.
Control over the deployment of an orbital tether system of great length
Wang C., Zabolotnov Y.M.
Optimization of trajectory motion of the first stage of an aerospace system
Khramov A.A.
Approximate models of air transport queueing systems with partial mutual assistance between service channels
Romanenko V.A.
Dynamics of the hydromechanical system of a production machine with an adaptive tool-feeding drive
Sidorenko V.S., Poleshkin M.S., Rakulenko S.V.
Main approaches and features of the design of aircraft hydro-mechanical control systems
Petrov P.V., Tselischev V.A., Kuderko D.A.
Analisys of the influence of radial displacement of a particle on the parameters of an eddy-current probe
Gudkov S.A., Kudryavtsev I.A.
Analysis estimation of pulse jet engine operation in detonation mode
Seyfetdinov R.B., Seyfetdinov M.B., Gafurov S.A., Shakhmatov E.V.
Development of classifier of plane’s parts for the solution of taks of automated CNC programs prepairing for CNC machines
Gismetulin A.R., Sergeev O.S.
Gas-turbine unit development experience for rotors wedging correction
Kozlyakova I.S., Krupin V.P., Potkin A.N., Fadeev V.A.
Choice of parameters of an engineering production preparation system
,
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.
Information control system for space experiments onboard international space station
Voronin F.A., Dunaeva I.V.
Efficiency of terminal control in the trans-atmospheric first stage of an aerospace system under atmospheric and aerodynamic disturbances
Balakin V.L., Kovalyov A.V., Krikunov M.M.
Thermal design of «AIST» small spacecraft
Kulikov D.S., Erilkin J.N.
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.
Increasing the capacity of engine intake system
Kozin A.M., Rusakov M.M.
Rail electromagnetic accelerators with an external magnetic field
Sukhachev K.I.
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.
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.
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.
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.
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