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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.
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.
Technological future of Russia: the challenge of the “third nature”
Gorbunov D.V., Nesterov A.Y.
Optimization of trajectory motion of the first stage of an aerospace system
Khramov A.A.
Controlled vibration protection systems: optimization and energy efficiency
Chernyshev V.I., Polyakov R.N., Fominova O.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.
The fiber-optical gauge of pressure for the control system of engine BPLA
Leonovich G.I., Matjunin S.A., Kilejnov Y.U., Livochkina H.A., Solovjov V.I.
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.
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.
Conception of base graphic and geometric training for bachelors of standardization and quality management
Gavrilov V.N., Ivashchenko V.I.
Command control of hypersonic cruising aircraft during climb
Balakin V.L., Kotchyan A.G.
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.
Economic-mathematical model of forming the capacity of an enterprise
Borodin A.I., Goloshchapova L.V.
Education organization in common information sphere given about product
Prodanov M.Y.
Optimizing a vehicle trans-atmospheric motion using Pontryagin’s maximum principle
Balakin V.L., Ishkov S.A., Khramov A.A.
Terminal control of aerospace system subhypersonic first stage
Balakin V.L., Kovalyov A.V.
Practical application of the methodology of mature production process for pitomated work flow management technology
Puzakina E.J., Larin S.N.
Information system of normative requirement management in airline for prevention of accidents
Dyatlov A.Y., Zaykin M.A., Kondratyeva A.S., Gorbunov I.V.
Analytical approximation of aircraft dynamics model in problems of approximate optimal control synthesis
Blinov A.O., Gurman V.I., Fralenko V.P.
Disturbed transatmospheric motion of the first stage of an aerospace system
Krikunov M.M.
Bases of methodology of maintenance of system safe operation of engines at all stages of life cycle
Grigoriev V.A., Kuznetsov S.P.
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.
Stewart platform pneumatic control system development and characteristic research
Greshnyakov P.I.
Stabilization of steady motions of a single rotor gyrostat with a cavity filled with a liquid of high viscosity
Bezglasnyi S.P.
Modern approach for design management in production enterprise integrated information space
Ivaschenko A.V., Kremenetskaya M.E., Filatov A.N., Peisakhovich D.G.
Development and study of the designs of sprayers with increased speed for internal combustion engine (ice)
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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.
Reduction of angular velocities of AIST-2D spacecraft using a system of kinetic moment dumping
Shipov M.G.
Modeling in management systems
Krasnoschekov A.D., Tyulevin S.V., Kozlova I.A., Tokareva A.V.
Fulfilment of initial design level of gas turbine engine using the methods of «ASTRA» CAE system
Kuzmichev V.S., Krupenich I.N., Tkachenko A.Y.
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.
FMS-3000, programming amilling machine 6M13GN-1 a program controller
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Fuzzy-controller simulation model as a tool of optimization of a limited availability ground handling system at a hub airport
Romanenko V.A.
Disturbed motion of a hypersonic vehicle in climb
Balakin V.L., Krikunov M.M.
Iteration procedure of choosing a low-thrust rendezvous transfer control program in problems of space debris disposal in the geostationary orbit
Philippov G.A.
Control of in-plane orbit parameters of a geostationary low-thrust satellite
Salmin V.V., Chetverikov A.S.
The automated control system of form of nonrigid shafts in lathing
Nabilkin A.U., Kravchenko S.A., Birukov V.P.
The combined fuel draining control system for liquid oxygen and liquid hydrogen upper stage
Ivanov V.P., Partola I.S.
Command control of hypersonic aircraft angle of attack during acceleration and climb
Kotchyan A.G.
Optimization of space vehicle combined orbital plane change maneuver on the basis of pontryagin’s maximum principle
Khramov A.A.
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.
Missile control on the basis of construction of attainability domains
Tolpegin O.A.
Obstacles of on-board mathematical models application in ACS
Gayday M.S., Dobrodeev A.V., Muhammedov N.A., Chervonyuk V.V.
Design of robust systems for the stabilization of unmanned aircraft equipment
Sushchenko O.A., Azarskov V.N.
Modelling the architecture of a system controlling the condition of maintenance objects
Koptev A.N., Yergaliyev D.S., Sakhanov K.Z.
Application of differential evolution algorithm in the problem of aeroassisted orbital plane change maneuver
Elisov N.A., Ishkov S.A., Khramov A.A.
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.
Optimization of space vehicle trans-atmospheric motion by using the method of sequential linearization
Balakin V.L., Ishkov S.A., Khramov A.A.
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.
Prospects of development of methods of maintenance of complex systems of airborne equipment complex
Chekrizhev N.V., Koptev A.N.
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.
System of artificial intellect support of low-thrust spacecraft interplanetary mission optimization
Starinova O.L.
Formation of a rotating ring-shaped three-body tethered nanosatellite system with limited control
Chen S., Zabolotnov Y.M.
Disturbed motion of the hypersonic first stage of an aerospace system in climb
Balakin V.L., Krikunov M.M.
Analysis of control programs and flight paths of a hypersonic vehicle in climb
Balakin V.L., Krikunov M.M.
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.
Rearrangement of digital control algorithms with variable discrete pitch size
Belonogov V.D.
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.
Length of restoration sequences for systems without information loss
Shulga T.E.
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.
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