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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.
Assessment of the possibility of shortening the landing distance of maneuverable aircraft
Strelets M.Y., Tarasov A.Z., Grishin I.A.
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.
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 program for noncoplanar heliocentric flight to Venus of non-perfectly reflecting solar sail spacecraft
Khabibullin R.M.
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.
Controlled vibration protection systems: optimization and energy efficiency
Chernyshev V.I., Polyakov R.N., Fominova O.V.
Method of controllung the angular position of IO ASD relative to the system of coordinates of a gyrostabilized platform
Degtyarev M.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.
Design of robust systems for the stabilization of unmanned aircraft equipment
Sushchenko O.A., Azarskov V.N.
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.
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.
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.
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.
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.
Device for rejection of semiconductor diodes
Tyulevin S.V., Piganov M.N., Chopin G.P., Arhipov A.I.
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.
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.
Main approaches and features of the design of aircraft hydro-mechanical control systems
Petrov P.V., Tselischev V.A., Kuderko D.A.
Iteration procedure of choosing a low-thrust rendezvous transfer control program in problems of space debris disposal in the geostationary orbit
Philippov G.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.
Flight development tests and attempted operation of «AIST» small satellites
Kirilin A.N., Tkachenko S.I., Salmin V.V., Semkin N.D., Papkov A.P., Abrashkin V.I., Tkachenko I.S., Zheleznov Y.E., Galaeva E.Y.
Research of small spacecraft dynamiсs taking into account the influence of elastic vibrations of asjacent solar panels and aerodynamic moment
Yelenev V.D., Titov B.A., Davydov E.I., Davydov I.E., Kochyan A.G., Yudintsev V.V.
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.
The automated control system of form of nonrigid shafts in lathing
Nabilkin A.U., Kravchenko S.A., Birukov V.P.
Up-to-date laser measuring systems in the production cycle of space technique
Grishanov V.N., Oynonen A.A.
Generation of control programes for disposable unmanned aircraft vehicle propulsion system by means of dynamic characteristic
Mikhailov A.Y., Akhmedzyanov D.A., Akhmetov Y.M., Mikhailova A.B.
Optimal program of controlling continuous low thrust in the flight between noncoplanar elliptical and geostationary orbits
Fadeenkov P.V., Ishkov S.A.
Control programs and motion trajectories of hypersonic first stage of an aerospace system
1 1.
Analytical approximation of aircraft dynamics model in problems of approximate optimal control synthesis
Blinov A.O., Gurman V.I., Fralenko V.P.
Operate reliability enhancement of thermogenerator modules for heat engine with acoustic emission method
1 1.
Developing a mathematical model of aircraft honeycomb sandwiches
Tits S.N.
Current state of the theory and practice of circuit wiring control and testing of the avionics of rocket fairings of middle-class launch vehicles
Koptev A.N., Gulyaev A.A.
Deployment and stabilization of the motion of a space tethered system in a lunar orbit
Ledkova T.A., Zabolotnov Y.M.
Optimal control of spacecraft motion in the vicinity of Eros 433 asteroid
Shornikov A.Y.
Automated system for measuring geometric parameters of turbine blades in production conditions
Aleksentsev E.I., Shavrin P.A., Fedoseev O.B.
Investigation of thermal conditions of nanosatellite optoelectronic telescopic module for different modes of operation
Tsaplin S.V., Bolychev S.A.
Optimization of space vehicle combined orbital plane change maneuver on the basis of the successive linearization method
Balakin V.L., Ishkov S.A., Khramov A.A.
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.
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.
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.
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.
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.
Disturbed transatmospheric motion of the first stage of an aerospace system
Krikunov M.M.
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