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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.
Solving the problem of minimax closed-loop control of liquid-propellant launch vehicle fuel consumption control
Shorikov A.F., Kalev V.I.
Onboard digital computer systems of the «Malachite» family for extreme conditions
Antimirov V.M., Umansky A.B., Shalimov L.N.
Special features of assessing the strength of nuclear reactor equipment under dynamic loads
Lonin K.A., Panov V.A., Patrushev V.L., Savchuk D.V., Soloviev S.A.
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.
Formation of a rotating ring-shaped three-body tethered nanosatellite system with limited control
Chen S., Zabolotnov Y.M.
Multi-position control of movements of large-sized structural elements during static loading using a laser tracker
Sazonnikova N.A., Uklein R.V.
Method of controllung the angular position of IO ASD relative to the system of coordinates of a gyrostabilized platform
Degtyarev M.S.
Control over the financial and economic activity of a joint-stock company carried out by the board of directors
Bogatyryov V.D., Khakimova A.K.
Gas-turbine unit development experience for rotors wedging correction
Kozlyakova I.S., Krupin V.P., Potkin A.N., Fadeev V.A.
Analysis estimation of pulse jet engine operation in detonation mode
Seyfetdinov R.B., Seyfetdinov M.B., Gafurov S.A., Shakhmatov E.V.
Reduction of angular velocities of AIST-2D spacecraft using a system of kinetic moment dumping
Shipov M.G.
Control over the deployment of an orbital tether system of great length
Wang C., Zabolotnov Y.M.
Automated system for measuring geometric parameters of turbine blades in production conditions
Aleksentsev E.I., Shavrin P.A., Fedoseev O.B.
Arrangement of data for the formation of a multidimensional array of essential insights in automated enterprise management system
Kartamyshev A.S.
Internal controls board computer system running real time operation system as an iterative aggregate
Dolbnya N.A.
Methodology complex of hardware-in-the-loop functional modelling of gas turbines and its systems
1 1., 1 1., 1 1., 1 1., 1 1.
Determining the angle of advance of ignition when switching from petrol to gas depending on fuel mixture burning rate
Shishkov V.A.
Creation of infotainment support of designing of control algorithms logic of spacecraft onboard control complexeses
1 1.
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.
Optimization of spatial turns of «AIST-2» small spacecraft on the basis of the principle of minimum control
Petrishchev V.F., Shipov M.G.
Development of information support for the spacecraft controlalgorithm design process
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.
Design of control moment gyro electric drive with strict requirements on ensuring desired rotational velocities
Polozhentcev D.S., Davidov A.A., Shipov M.G., Kazakov E.P., Malykh B.I.
Disturbed transatmospheric motion of the first stage of an aerospace system
Krikunov M.M.
Joint work of units and characteristics of elements gas the equipment for the engine of internal combustion with spark ignition
Shishkov V.A., Lesnih U.I.
Motion control system of multicopter
Sitnikov D.V., Burian Y.A., Russkih G.S.
Conceptually logical model of an integrated data system (software & hardware) for the control of individual and small-scale production of aviation components
Prilepsky I.V.
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.
Reliability indicators of information control systems with hardware and software failures as complex time functions
Maryukhnenko V.S.
Optimizing the propulsion of a hypersonic accelerator aircraft of a two-stage aerospace system
Balakin V.L., Bebyakov A.A., Kotchyan A.G.
Optimal command control of flight paths of aerospace system hypersonic first stage in conditions of atmospheric disturbances
Krikunov M.M.
Disturbed motion of the hypersonic first stage of an aerospace system in climb
Balakin V.L., Krikunov M.M.
Investigation of the thermal regime of microsatellite optoelectronic telescopic complex under operating conditions
Tsaplin S.V., Bolychev S.A.
Thermal design of «AIST» small spacecraft
Kulikov D.S., Erilkin J.N.
Development of discrete pneumatic pressure regulator and researching of its characteristics
Greshniakov P.I., Sinyakov A.F., Ilukhin V.N.
Constructing the specification for the on-board realtime control algorithm
Tyugashev A.A., Bogatov A.Y.
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.
On selection of automatic control system for crvogenic fuel gas turbine engine
Bukin V.A.
Оptimization of gas turbine aircraft engine control throughout the engine service life
Gurevich O.S., Golberg F.D., Smetanin S.A., Trifonov M.E.
Service-oriented distributed software complex for evaluation and multi-criteria analysis of reliability and survivability of on-board equipment of small satellites: Russian and Belarusian segments
Zelentsov V.A., Potryasaev S.A., Sokolov B.V., Skobtsov V.Y., Korenyako S.A., Kim D.S., Vakulchyk E.N., Kulbak L.I., Nikolaenya E.D., Lapitskaya N.V., Saksonov R.V.
Micro gas turbine engine imitation model
Kuznetsov A.V., Makaryants G.M.
Stabilization of steady motions of a single rotor gyrostat with a cavity filled with a liquid of high viscosity
Alekseev A.V., Bezglasny S.P., Krasnikov V.S.
Using active noise suppression non-adaptive systems with a transfer function model for the reduction of medical equipment noise
Sementsov S.G.
Peculiarities of starting a spark-ignition gas fuel internal combustion engine
Shishkov V.A.
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.
Experimental verification of the specified characteristics of a solar battery at the stages of production and ground operation
Shuplyak Y.P., Sorokoletov V.I.
Fluctuations of pressure in rail gas injection of engines with spark ignition
Shishkov V.A.
Kick-stage control by navigational data of satellite navigation system
1 1.
Extrapolation of conditions of an information measuring and control system with the iterative algorithm of operation
Zelensky V.A.
Realization of the multichannel cnc machining methods
1 1., 1 1.
Modelling the architecture of a system controlling the condition of maintenance objects
Koptev A.N., Yergaliyev D.S., Sakhanov K.Z.
Fuzzy-controller simulation model as a tool of optimization of a limited availability ground handling system at a hub airport
Romanenko V.A.
Operation of an electronic system of control for spark-ignition gas fuel internal combustion engines in ignition misses
Shishkov V.A.
Development of a procedure for the synthesis of a micro gas turbine engine neural controller with account for fuel consumption constraints
Kuznetsov A.V., Makaryants G.M.
Dynamic process modeling of aircraft engine control system
Blyumin K.V.
Algorithm of adaptation of an electronic control system of internal combustion engines to various chemical compositions of gas fuel
Shishkov V.A.
Modelling changes of condition of aircraft hydraulic system working fluid
Gareyev A.M.
Deployment and stabilization of the motion of a space tethered system in a lunar orbit
Ledkova T.A., Zabolotnov Y.M.
Investigation of thermal conditions of nanosatellite optoelectronic telescopic module for different modes of operation
Tsaplin S.V., Bolychev S.A.
Dynamics of feed water flow rate control system with low- noise regulator
Berestovitskiy E.G., Kizilov P.I., Kruchkov A.N., Pialov N.V.
Mathematical model of fuel sloshing in the measuring channel of the fuel expenditure control system
Kryukov Y.A.
Mechanism for the development of an organization process control system
Gerasimov K.B.
Integrated system of controlling Earth remote sensing spacecraft on the basis of multifunctional usage of onboard equipment with the aim of minimizing mass-energy and cost parameters
Belov Y.V., Shikhanov S.V.
Control programs and motion trajectories of hypersonic first stage of an aerospace system
1 1.
Backstepping synthesis of the height control system of an unmanned aerial vehicle
Akhramovich S.A., Barinov A.V., Malyshev V.V., Starkov A.V.
Possibility of using leo satellite communication systems for on-line data interchange
Davydov D.D.
Choosing a program for controlling the deployment of an orbital tether system with deployment speed limitations
Ishkov S.A., Xiaoye X., Filippov G.A.
Experience in the development of 11Д58MФ liquid rocket engines
Smolentsev A.A.
Improvement of the flight attitude control accuracy of the Earth observation spacecraft
Akhmetov R.N., Sollogub A.V., Makarov V.P., Golovchenko A.A., Filatov A.V.
Simulation of fluid contamination control process
Gareyev A.M.
Module of storing information: combining the functions of authorizing access and transfer of information within the control system equipment
Hanevsky D.A., Solovieva N.V., Ananyin A.S., Shchepochkin I.N.
Features of start-up the engine of internal combustion with spark ignition on gas fuel
Shishkov V.A.
Using the «virtual engine» software in automatic control system of gas turbine engine
Golberg F.D., Gurevich O.S., Petukhov A.A.
Stewart platform pneumatic control system development and characteristic research
Greshnyakov P.I.
Development and analysis of screw restrictor hydraulic characteristics in the air bleed valve control unit of a gas turbine engine
Gimadiev A.G., Makaryants G.M., Blyumin K.V., Dudnichenko I.M.
Cycle parameters of an internal combustion spark-ignition gas piston engine with an electronic control system
Shishkov V.A.
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.
Statistical analysis of a capsule’s motion during its reentry into the atmosphere with the aid of a space tether system
1 1., 1 1.
1 - 79 of 79 Items

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