Search

Issue
Title
Authors
Solving the problem of minimax closed-loop control of liquid-propellant launch vehicle fuel consumption control
Shorikov A.F., Kalev V.I.
Assessment of the possibility of shortening the landing distance of maneuverable aircraft
Strelets M.Y., Tarasov A.Z., Grishin I.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.
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.
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.
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.
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.
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.
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.
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.
Bringing spacecraft into solar-oriented attitude by the measurements of a single-axis angular-rate sensor and an optical solar sensor
Shipov M.G., Steklova A.A., Davydov A.A.
Method and technical tools of assessing the reliability of digital angle converters
Grechishnikov V.M., Yudin A.A.
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.
Suppression of gas-dynamic self-oscillations in the outflow line of a gas control valve
Balyaba M.V., Ermilov M.A., Kryuchkov A.N., Shabanov K.U.
Modeling in management systems
Krasnoschekov A.D., Tyulevin S.V., Kozlova I.A., Tokareva A.V.
Control device zener diode
Tyulevin S.V., Kozlova I.N., Shopin G.P., Arkhipov A.I.
Stabilization of a pilot-operated gas pressure control valve by placing a throttle at the inlet
Stadnik D.M., Sverbilov V.Y., Makaryants G.M., Makaryants M.V.
NC machine tools contact measuring devices uncertainty when products geometrical parameters control
Bolotov M.I., Zhidyaev A.N., Surkov O.S., Tiapaev N.V., Papsuev I.V.
Increase of the role of conformity assessment at the facilities controlled by the federal service on ecological, technological and nuclear supervision
Barvinok V.A., Naumov L.A., Dolgikh A.V.
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.
Optimum programs of correction of quasielliptical and circular orbits of spacecraft with the limited-thrust engine
Khramov A.A.
Usage of the graphical languages in lifecycle of embedded software for spacecrafts
1 1., 1 1.
Using active noise suppression non-adaptive systems with a transfer function model for the reduction of medical equipment noise
Sementsov S.G.
Current preventive control of a technical process on a basis of exponential smoothening
1 1.
Command control of hypersonic aircraft angle of attack during acceleration and climb
Kotchyan A.G.
Mathematical modeling of dynamic processes in a hydraulic drive with a discrete regulator of liquid flow
Shakhmatov Y.V., Gimadiev A.G., Sverbilov V.Y., Sinyakov A.F.
Optimal command control of hypersonic aircraft flight path in conditions of atmospheric disturbances
Krikunov M.M.
Peculiarities of starting a spark-ignition gas fuel internal combustion engine
Shishkov V.A.
Reduction of angular velocities of AIST-2D spacecraft using a system of kinetic moment dumping
Shipov M.G.
Analysis of control programs and flight paths of a hypersonic vehicle in climb
Balakin V.L., Krikunov M.M.
Simulation and experimental development of a temperature control system of a radiation calibration source based on a PID-regulyator
Volkov V.V.
Control over the deployment of an orbital tether system of great length
Wang C., Zabolotnov Y.M.
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.
Control of in-plane orbit parameters of a geostationary low-thrust satellite
Salmin V.V., Chetverikov A.S.
Missile control on the basis of construction of attainability domains
Tolpegin O.A.
Real-time control algorithms requirements verification mathematical model implementation in visual design computer-aided system
Shulyndin A.V., Tjugashev A.A.
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.
Visual approach to verifictaion of real-time control software
Tyugashev A.A., Bogatov A.Y., Shulyndin A.V.
Promising technologies for solving boundary problems regarding the delivery of separating parts of carrier rockets with terminal targeting
Benevolsky S.V., Goncharenko V.I.
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.
Determination of optimum plans of Earth Remote Sensing spacecraft detailed survey by the use of a graph
Buzuev K.V.
Two-channel optimal discrete law of control of spacecraft with aerodynamic and inertial asymmetry during descent in Mars atmosphere
Lyubimov V.V., Bakry I.
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.
Ensuring permissible level of gas turbine dynamic loading in operation by means of standard engine control devices
Chervonyuk V.V., Korovin B.B.
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.
Metrological analysis of a device rof nondestructive control of flight vehicle fuel tank current conductive coatings
Samsonov A.S., Blinov D.I., Skvortsov B.V., Zhivonosnovskaya D.M.
Optimal control laws of onboard coils for the reduction of angular momentum and damping of angular velocity of nanosatellites and microsatellites with magnetic coils on board
Lyubimov V.V., Podkletnova S.V.
Device for monitoring radiation situation on spacecraft
Syomkin N.D., Plokhotnichenko P.G., Ilyin A.B., Kalaev M.P., Ryazanov D.M., Pomel'nikov P.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.
Dynamic process modeling of aircraft engine control system
Blyumin K.V.
Solving tasks of control and targeting for remote sensing devices by systems of processing and analysis of visual information
Sbrodov V.V., Sviridov V.P., Safronov S.G.
System-simulator load the steering organs
Aliluev A.V.
Algorithm of adaptation of an electronic control system of internal combustion engines to various chemical compositions of gas fuel
Shishkov V.A.
Optimization methods of design-ballistic characteristics circumterraneous and interplanetary space vehicle with electrojet engines of low thrust
1 1., 1 1., 1 1., 1 1., 1 1., 1 1., 1 1., 1 1., 1 1.
Interaction of high-speed particles and temperature control elements of a space vehicle
Izyumov M.V., Syomkin N.D., Kalayev M.P.
Using of heat-pipes with increased heat conduction as core elements of system of thermal control for aerospace equipment
, ,
Modelling changes of condition of aircraft hydraulic system working fluid
Gareyev A.M.
Optimal control of the angle of attack of a hypersonic flight vehicle
Bebyakov 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.
1 - 100 of 172 Items 1 2 > >> 

Search tips:

  • Search terms are case-insensitive
  • Common words are ignored
  • By default only articles containing all terms in the query are returned (i.e., AND is implied)
  • Combine multiple words with OR to find articles containing either term; e.g., education OR research
  • Use parentheses to create more complex queries; e.g., archive ((journal OR conference) NOT theses)
  • Search for an exact phrase by putting it in quotes; e.g., "open access publishing"
  • Exclude a word by prefixing it with - or NOT; e.g. online -politics or online NOT politics
  • Use * in a term as a wildcard to match any sequence of characters; e.g., soci* morality would match documents containing "sociological" or "societal"

This website uses cookies

You consent to our cookies if you continue to use our website.

About Cookies