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Assessment of the possibility of shortening the landing distance of maneuverable aircraft
Strelets M.Y., Tarasov A.Z., Grishin I.A.
The relevance of introducing a requirements management system in the production process of the aircraft engine construction industry
Malinovskiy I.M., Starodumov A.V., Myagkov K.A., Yusipov B.K.
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.
Main approaches and features of the design of aircraft hydro-mechanical control systems
Petrov P.V., Tselischev V.A., Kuderko D.A.
Experimental analysis of instability and self-oscillations in an electrohydraulic servo drive
Petrov P.V., Sunarchin R.A., Mashkov M.A., Krivosheev N.S.
Development of information support for the spacecraft controlalgorithm design process
1 1., 1 1.
Determining the angle of advance of ignition when switching from petrol to gas depending on fuel mixture burning rate
Shishkov V.A.
Kick-stage control by navigational data of satellite navigation system
1 1.
Optimization of spatial turns of «AIST-2» small spacecraft on the basis of the principle of minimum control
Petrishchev V.F., Shipov M.G.
Control over the deployment of an orbital tether system of great length
Wang C., 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.
Analysis estimation of pulse jet engine operation in detonation mode
Seyfetdinov R.B., Seyfetdinov M.B., Gafurov S.A., Shakhmatov E.V.
Gas-turbine unit development experience for rotors wedging correction
Kozlyakova I.S., Krupin V.P., Potkin A.N., Fadeev V.A.
Automated system for measuring geometric parameters of turbine blades in production conditions
Aleksentsev E.I., Shavrin P.A., Fedoseev O.B.
Method of controllung the angular position of IO ASD relative to the system of coordinates of a gyrostabilized platform
Degtyarev M.S.
Onboard digital computer systems of the «Malachite» family for extreme conditions
Antimirov V.M., Umansky A.B., Shalimov L.N.
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.
Problems of unmanned spacecraft reengineering in abnormal flight situations and their knowledge-based solutions
Akhmetov R.N., Makarov V.P., Sollogub A.V.
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.
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.
Peculiarities of starting a spark-ignition gas fuel internal combustion engine
Shishkov V.A.
Experience in the development of 11Д58MФ liquid rocket engines
Smolentsev A.A.
Optimizing the propulsion of a hypersonic accelerator aircraft of a two-stage aerospace system
Balakin V.L., Bebyakov A.A., Kotchyan A.G.
Operation of an electronic system of control for spark-ignition gas fuel internal combustion engines in ignition misses
Shishkov V.A.
Mathematical model of fuel sloshing in the measuring channel of the fuel expenditure control system
Kryukov Y.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.
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.
Backstepping synthesis of the height control system of an unmanned aerial vehicle
Akhramovich S.A., Barinov A.V., Malyshev V.V., Starkov A.V.
Possibility of using leo satellite communication systems for on-line data interchange
Davydov D.D.
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.
Optimal command control of flight paths of aerospace system hypersonic first stage in conditions of atmospheric disturbances
Krikunov M.M.
Arrangement of data for the formation of a multidimensional array of essential insights in automated enterprise management system
Kartamyshev A.S.
Motion control system of multicopter
Sitnikov D.V., Burian Y.A., Russkih G.S.
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.
Fluctuations of pressure in rail gas injection of engines with spark ignition
Shishkov V.A.
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.
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.
Оptimization of gas turbine aircraft engine control throughout the engine service life
Gurevich O.S., Golberg F.D., Smetanin S.A., Trifonov M.E.
Nominal motion control program in a supersonic carrier aircraft
Balakin V.L., Potapov V.I.
Algorithm of adaptation of an electronic control system of internal combustion engines to various chemical compositions of gas fuel
Shishkov V.A.
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.
Deployment and stabilization of the motion of a space tethered system in a lunar orbit
Ledkova T.A., Zabolotnov Y.M.
Dynamic process modeling of aircraft engine control system
Blyumin K.V.
Features of start-up the engine of internal combustion with spark ignition on gas fuel
Shishkov V.A.
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.
Micro gas turbine engine imitation model
Kuznetsov A.V., Makaryants G.M.
Cycle parameters of an internal combustion spark-ignition gas piston engine with an electronic control system
Shishkov V.A.
Mechanism for the development of an organization process control system
Gerasimov K.B.
Control programs and motion trajectories of hypersonic first stage of an aerospace system
1 1.
1 - 49 of 49 Items

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