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Solving the problem of minimax closed-loop control of liquid-propellant launch vehicle fuel consumption control
Shorikov A.F., Kalev V.I.
Intelligent robust controllers for tribotronic conical fluid film bearings
Kazakov Y.N., Shutin D.V., Savin L.A.
Algorithm for solving optimal open-loop terminal control problem for spacecraft rendezvous with account of constraints on the state
Shorikov A.F., Goranov A.Y.
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.
Control program for noncoplanar heliocentric flight to Venus of non-perfectly reflecting solar sail spacecraft
Khabibullin R.M.
Assessment of the possibility of shortening the landing distance of maneuverable aircraft
Strelets M.Y., Tarasov A.Z., Grishin I.A.
Controlled vibration protection systems: optimization and energy efficiency
Chernyshev V.I., Polyakov R.N., Fominova O.V.
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.
Multi-position control of movements of large-sized structural elements during static loading using a laser tracker
Sazonnikova N.A., Uklein R.V.
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.
Method of controllung the angular position of IO ASD relative to the system of coordinates of a gyrostabilized platform
Degtyarev M.S.
Thin-film electrodes of dielectric elastomer-based actuators for an active vibration control system
Shcherbakova V.S., Bazinenkov A.M., Sidorova S.V., Kouptsov A.D., Ivanova D.A.
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.
Design of robust systems for the stabilization of unmanned aircraft equipment
Sushchenko O.A., Azarskov V.N.
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.
Conducting functional control of field-programmable gate arrays
Ogurtsov A.A.
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.
Experimental analysis of instability and self-oscillations in an electrohydraulic servo drive
Petrov P.V., Sunarchin R.A., Mashkov M.A., Krivosheev N.S.
Optical characteristics of a multilayer solar sail and their effect on its heliocentric motion
Rozhkov M.A.
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 trajectory motion of the first stage of an aerospace system
Khramov A.A.
Formation of a rotating ring-shaped three-body tethered nanosatellite system with limited control
Chen S., Zabolotnov Y.M.
Device for rejection of semiconductor diodes
Tyulevin S.V., Piganov M.N., Chopin G.P., Arhipov A.I.
Main approaches and features of the design of aircraft hydro-mechanical control systems
Petrov P.V., Tselischev V.A., Kuderko D.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.
Optimization of spatial turns of «AIST-2» small spacecraft on the basis of the principle of minimum control
Petrishchev V.F., Shipov M.G.
The use of computational methods for the parametrization of the angular motion control program in on-board control systems of Earth remote sensing spacecraft
Galkina A.S., Manturov A.I., Pyrinov N.I., Yurin V.E.
Exponential smoothing parameter time series in the presence of trend
Kerensky A.M.
Disturbed motion of a hypersonic vehicle in climb
Balakin V.L., Krikunov M.M.
Backstepping synthesis of the height control system of an unmanned aerial vehicle
Akhramovich S.A., Barinov A.V., Malyshev V.V., Starkov A.V.
Construction of an upper stage flight pattern for placing a group of spacecraft into an orbit plane with the required angular distance between the satellites
Poplevin A.S., Panov N.A.
Optimization of parameters of a hub aircraft ground handling system on the basis of a fuzzy-controller simulation model
Vasileva I.A., Romanenko V.A., Khvostova T.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.
End mill design and manufacturing with modern multi-axis grinding machines
Skuratov D.L., Kuznetsov A.V., Oparin V.M., Sazonov M.B.
Command control of hypersonic cruising aircraft during climb
Balakin V.L., Kotchyan A.G.
The combined fuel draining control system for liquid oxygen and liquid hydrogen upper stage
Ivanov V.P., Partola I.S.
Simulation of fluid contamination control process
Gareyev A.M.
Improving the operating characteristics of engines by the imposition of manufacturing operation of hermeticity inspection of vacuum-tight radio electronic device cases
System of artificial intellect support of low-thrust spacecraft interplanetary mission optimization
Starinova O.L.
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.
Optimization of space vehicle combined orbital plane change maneuver on the basis of pontryagin’s maximum principle
Khramov A.A.
Arrangement of data for the formation of a multidimensional array of essential insights in automated enterprise management system
Kartamyshev A.S.
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.
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.
Internal controls board computer system running real time operation system as an iterative aggregate
Dolbnya N.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.
Obstacles of on-board mathematical models application in ACS
Gayday M.S., Dobrodeev A.V., Muhammedov N.A., Chervonyuk V.V.
Complex automation of process planing and numeric control of mechanical processing of hulls details
Khrustitskiy K.V., Cherepashkov A.A.
Discreet-time models of parameters of leasing contract optimum control
Pavlov O.V., Fudobina E.A.
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.
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.
Proactive maintenance of hydrosystems on the basis of the analysis of parameters of particles of contamination of hydraulic fluid
Kovalev M.A.
Approximate methods of calculating optimal flights of space vehicles with low-thrust engines. Part II
Salmin V.V., Vassiliev V.V., Ishkov S.A., Romanenko V.A., Sokolov V.O., Starinova O.L., Yurin V.V.
On-stand emergency protection and control system for propulsion tests of «Soyuz-2-1B» launch vehicle
Liseykin V.A., Tozhokin I.A.
Disturbed transatmospheric motion of the first stage of an aerospace system
Krikunov M.M.
Application of differential evolution algorithm in the problem of aeroassisted orbital plane change maneuver
Elisov N.A., Ishkov S.A., Khramov A.A.
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.
Convective current experiments using Dakon-P equipment onboard “Progress” cargo spacecraft
Ayukaeva D.M., Babushkin I.A., Belyaev M.Y., Zilberman Y.A., Matveeva T.V., Sidorov A.S.
Optimizing a vehicle trans-atmospheric motion using Pontryagin’s maximum principle
Balakin V.L., Ishkov S.A., Khramov A.A.
Optimization of space vehicle trans-atmospheric motion by using the method of sequential linearization
Balakin V.L., Ishkov S.A., Khramov A.A.
Development of intelligent peripheral devices of control and emergency protection systems for ground testing of liquid-propellant rocket engines
Volnukhin O.A., Liseykin V.A., Tozhokin I.A., Churin M.N.
Mathematical model of angular motion of nanosatellites with inertial actuators
Moldabekov M.M., Ahmedov D.S., Elubaev S.A., Sukhenko A.S., Bopeev T.M., Alipbayev K.A., Mikhailenko D.L.
Estimation of tension of the surface layer of parts after hardening by different methods of surface plastic deformation
Sazonov M.B., Solovatskaya L.V.
Rearrangement of digital control algorithms with variable discrete pitch size
Belonogov V.D.
Motion control system of multicopter
Sitnikov D.V., Burian Y.A., Russkih G.S.
Gas-turbine unit development experience for rotors wedging correction
Kozlyakova I.S., Krupin V.P., Potkin A.N., Fadeev V.A.
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.
Mathematical models of optimal investment control in fixed assets
Pavlov O.V., Moshkova T.A.
Length of restoration sequences for systems without information loss
Shulga T.E.
Development and study of the designs of sprayers with increased speed for internal combustion engine (ice)
, ,
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.
Onboard digital computer systems of the «Malachite» family for extreme conditions
Antimirov V.M., Umansky A.B., Shalimov L.N.
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.
Control metods of hardening process in the time of SPD
Volkov A.N., Sazonov M.B., Mashinnov K.Y.
Programs of time-optimal control in the problem of rendezvous transfer of spacecraft with low transversal thrust
Ishkov S.A., Filippov G.A., Fadeenkov P.V.
Investigation of the thermal regime of microsatellite optoelectronic telescopic complex under operating conditions
Tsaplin S.V., Bolychev S.A.
Resonant converter with PWM output voltage adjustment
Vorokh D.A., Makhov A.I.
Thermal design of «AIST» small spacecraft
Kulikov D.S., Erilkin J.N.
Analysis estimation of pulse jet engine operation in detonation mode
Seyfetdinov R.B., Seyfetdinov M.B., Gafurov S.A., Shakhmatov E.V.
Check and prediction of gas-turbine engine’s technical state
Zotin N.A.
Stabilization of steady motions of a single rotor gyrostat with a cavity filled with a liquid of high viscosity
Bezglasnyi S.P.
Development of discrete pneumatic pressure regulator and researching of its characteristics
Greshniakov P.I., Sinyakov A.F., Ilukhin V.N.
Increasing the overall performance of a two-stroke engine with spark ignition by fuel injection
Dovgyallo A.I., Krasheninnikov S.V., Shchepetov D.A.
Constructing the specification for the on-board realtime control algorithm
Tyugashev A.A., Bogatov A.Y.
Problems of synthesis and analysis of the system behaviour control theory on the basis of functional redundancy properties for the class of group automata
Sytnik A.A., Shulga T.E., Vagarina N.S.
FMS-3000, programming amilling machine 6M13GN-1 a program controller
, , ,
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.
Test rig for a hydraulic drive under switched inertance control
Shorin V.P., Sverbilov V.Y., Gimadiev A.G., Greshniakov P.I., Ilyukhin V.N., Stadnik D.M.
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