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Vol 19, No 1 (2020)

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.

(Rus)

Vol 10, No 6 (2011)

Method and technical tools of assessing the reliability of digital angle converters

Grechishnikov V.M., Yudin A.A.

(Rus)

Vol 10, No 3-2 (2011): Special Issue

On selection of automatic control system for crvogenic fuel gas turbine engine

Bukin V.A.

(Rus)

Vol 17, No 4 (2018)

Оptimization of gas turbine aircraft engine control throughout the engine service life

Gurevich O.S., Golberg F.D., Smetanin S.A., Trifonov M.E.

(Rus)

Vol 16, No 4 (2017)

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.

(Rus)

Vol 16, No 2 (2017)

Micro gas turbine engine imitation model

Kuznetsov A.V., Makaryants G.M.

(Rus)

Vol 15, No 3 (2016)

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.

(Rus)

Vol 10, No 7 (2011)

Modeling in management systems

Krasnoschekov A.D., Tyulevin S.V., Kozlova I.A., Tokareva A.V.

(Rus)

Vol 11, No 7 (2012)

Control device zener diode

Tyulevin S.V., Kozlova I.N., Shopin G.P., Arkhipov A.I.

(Rus)

Vol 11, No 4 (2012)

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.

(Rus)

Vol 11, No 3-2 (2012): Special Issue

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.

(Rus)

Vol 11, No 1 (2012)

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.

(Rus)

Vol 11, No 5-1 (2012): Special Issue

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.

(Rus)

Vol 10, No 2 (2011)

Optimum programs of correction of quasielliptical and circular orbits of spacecraft with the limited-thrust engine

Khramov A.A.

(Rus)

Vol 9, No 2 (2010): Special Issue

Usage of the graphical languages in lifecycle of embedded software for spacecrafts

1 1., 1 1.

(Rus)

Vol 8, No 4 (2009)

Using active noise suppression non-adaptive systems with a transfer function model for the reduction of medical equipment noise

Sementsov S.G.

(Rus)

Vol 8, No 3-2 (2009): Special Issue

Current preventive control of a technical process on a basis of exponential smoothening

1 1.

(Rus)

Vol 8, No 1 (2009)

Command control of hypersonic aircraft angle of attack during acceleration and climb

Kotchyan A.G.

(Rus)

Vol 12, No 1 (2013)

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.

(Rus)

Vol 19, No 1 (2020)

Optimal command control of hypersonic aircraft flight path in conditions of atmospheric disturbances

Krikunov M.M.

(Rus)

Vol 10, No 6 (2011)

Peculiarities of starting a spark-ignition gas fuel internal combustion engine

Shishkov V.A.

(Rus)

Vol 18, No 2 (2019)

Reduction of angular velocities of AIST-2D spacecraft using a system of kinetic moment dumping

Shipov M.G.

(Rus)

Vol 17, No 4 (2018)

Analysis of control programs and flight paths of a hypersonic vehicle in climb

Balakin V.L., Krikunov M.M.

(Rus)

Vol 16, No 4 (2017)

Simulation and experimental development of a temperature control system of a radiation calibration source based on a PID-regulyator

Volkov V.V.

(Rus)

Vol 16, No 2 (2017)

Control over the deployment of an orbital tether system of great length

Wang C., Zabolotnov Y.M.

(Rus)

Vol 15, No 3 (2016)

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.

(Rus)

Vol 14, No 4 (2015)

Control of in-plane orbit parameters of a geostationary low-thrust satellite

Salmin V.V., Chetverikov A.S.

(Rus)

Vol 14, No 1 (2015)

Missile control on the basis of construction of attainability domains

Tolpegin O.A.

(Rus)

Vol 11, No 7 (2012)

Real-time control algorithms requirements verification mathematical model implementation in visual design computer-aided system

Shulyndin A.V., Tjugashev A.A.

(Rus)

Vol 11, No 4 (2012)

Experimental verification of the specified characteristics of a solar battery at the stages of production and ground operation

Shuplyak Y.P., Sorokoletov V.I.

(Rus)

Vol 11, No 3-2 (2012): Special Issue

Fluctuations of pressure in rail gas injection of engines with spark ignition

Shishkov V.A.

(Rus)

Vol 11, No 1 (2012)

Visual approach to verifictaion of real-time control software

Tyugashev A.A., Bogatov A.Y., Shulyndin A.V.

(Rus)

Vol 10, No 2 (2011)

Promising technologies for solving boundary problems regarding the delivery of separating parts of carrier rockets with terminal targeting

Benevolsky S.V., Goncharenko V.I.

(Rus)

Vol 9, No 2 (2010): Special Issue

Kick-stage control by navigational data of satellite navigation system

1 1.

(Rus)

Vol 8, No 4 (2009)

Extrapolation of conditions of an information measuring and control system with the iterative algorithm of operation

Zelensky V.A.

(Rus)

Vol 8, No 3-2 (2009): Special Issue

Realization of the multichannel cnc machining methods

1 1., 1 1.

(Rus)

Vol 7, No 1 (2008)

Modelling the architecture of a system controlling the condition of maintenance objects

Koptev A.N., Yergaliyev D.S., Sakhanov K.Z.

(Rus)

Vol 12, No 1 (2013)

Determination of optimum plans of Earth Remote Sensing spacecraft detailed survey by the use of a graph

Buzuev K.V.

(Rus)

Vol 21, No 3 (2022)

Two-channel optimal discrete law of control of spacecraft with aerodynamic and inertial asymmetry during descent in Mars atmosphere

Lyubimov V.V., Bakry I.

(Rus)

Vol 18, No 4 (2019)

Fuzzy-controller simulation model as a tool of optimization of a limited availability ground handling system at a hub airport

Romanenko V.A.

(Rus)

Vol 10, No 6 (2011)

Operation of an electronic system of control for spark-ignition gas fuel internal combustion engines in ignition misses

Shishkov V.A.

(Rus)

Vol 18, No 2 (2019)

Ensuring permissible level of gas turbine dynamic loading in operation by means of standard engine control devices

Chervonyuk V.V., Korovin B.B.

(Rus)

Vol 17, No 3 (2018)

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.

(Rus)

Vol 16, No 3 (2017)

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.

(Rus)

Vol 15, No 2 (2016)

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.

(Rus)

Vol 14, No 1 (2015)

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.

(Rus)

Vol 11, No 7 (2012)

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.

(Rus)

Vol 11, No 3-2 (2012): Special Issue

Dynamic process modeling of aircraft engine control system

Blyumin K.V.

(Rus)

Vol 11, No 1 (2012)

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.

(Rus)

Vol 10, No 3-1 (2011): Special Issue

System-simulator load the steering organs

Aliluev A.V.

(Rus)

Vol 10, No 1 (2011)

Algorithm of adaptation of an electronic control system of internal combustion engines to various chemical compositions of gas fuel

Shishkov V.A.

(Rus)

Vol 9, No 2 (2010): Special Issue

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.

(Rus)

Vol 8, No 4 (2009)

Interaction of high-speed particles and temperature control elements of a space vehicle

Izyumov M.V., Syomkin N.D., Kalayev M.P.

(Rus)

Vol 8, No 3-2 (2009): Special Issue

Using of heat-pipes with increased heat conduction as core elements of system of thermal control for aerospace equipment

, ,

(Rus)

Vol 7, No 1 (2008)

Modelling changes of condition of aircraft hydraulic system working fluid

Gareyev A.M.

(Rus)

Vol 12, No 1 (2013)

Optimal control of the angle of attack of a hypersonic flight vehicle

Bebyakov A.A.

(Rus)

Vol 20, No 2 (2021)

Deployment and stabilization of the motion of a space tethered system in a lunar orbit

Ledkova T.A., Zabolotnov Y.M.

(Rus)

Vol 18, No 4 (2019)

Optimal control of spacecraft motion in the vicinity of Eros 433 asteroid

Shornikov A.Y.

(Rus)

Vol 10, No 3-4 (2011): Special Issue

Automated system for measuring geometric parameters of turbine blades in production conditions

Aleksentsev E.I., Shavrin P.A., Fedoseev O.B.

(Rus)

Vol 18, No 2 (2019)

Investigation of thermal conditions of nanosatellite optoelectronic telescopic module for different modes of operation

Tsaplin S.V., Bolychev S.A.

(Rus)

Vol 17, No 2 (2018)

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.

(Rus)

Vol 16, No 3 (2017)

Iteration procedure of choosing a low-thrust rendezvous transfer control program in problems of space debris disposal in the geostationary orbit

Philippov G.A.

(Rus)

Vol 16, No 1 (2017)

Dynamics of feed water flow rate control system with low- noise regulator

Berestovitskiy E.G., Kizilov P.I., Kruchkov A.N., Pialov N.V.

(Rus)

Vol 15, No 1 (2016)

Mathematical model of fuel sloshing in the measuring channel of the fuel expenditure control system

Kryukov Y.A.

(Rus)

Vol 14, No 4 (2015)

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.

(Rus)

Vol 14, No 1 (2015)

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.

(Rus)

Vol 11, No 6 (2012)

Mechanism for the development of an organization process control system

Gerasimov K.B.

(Rus)

Vol 11, No 4 (2012)

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.

(Rus)

Vol 11, No 3-1 (2012): Special Issue

The automated control system of form of nonrigid shafts in lathing

Nabilkin A.U., Kravchenko S.A., Birukov V.P.

(Rus)

Vol 11, No 1 (2012)

Up-to-date laser measuring systems in the production cycle of space technique

Grishanov V.N., Oynonen A.A.

(Rus)

Vol 10, No 3-1 (2011): Special Issue

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.

(Rus)

Vol 10, No 1 (2011)

Optimal program of controlling continuous low thrust in the flight between noncoplanar elliptical and geostationary orbits

Fadeenkov P.V., Ishkov S.A.

(Rus)

Vol 9, No 1 (2010)

Control programs and motion trajectories of hypersonic first stage of an aerospace system

1 1.

(Rus)

Vol 8, No 4 (2009)

Analytical approximation of aircraft dynamics model in problems of approximate optimal control synthesis

Blinov A.O., Gurman V.I., Fralenko V.P.

(Rus)

Vol 8, No 3-2 (2009): Special Issue

Operate reliability enhancement of thermogenerator modules for heat engine with acoustic emission method

1 1.

(Rus)

Vol 7, No 1 (2008)

Developing a mathematical model of aircraft honeycomb sandwiches

Tits S.N.

(Rus)

Vol 12, No 2 (2013)

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.

(Rus)

101 - 177 of 177 Items << < 1 2

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