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Authors
Use of phase portraits of hydro-mechanical units for diagnosing aircraft hydraulic systems
Gareyev A.M., Popelnyuk I.A.
Locally optimal control of space tug motion between the libration points of the Earth-Moon system
Starinova O.L., Fain M.K.
Procedure of designing a pilot operated gas pressure regulator for launch vehicle fuel tanks
Gimadiev A.G., Sverbilov V.Y., Stadnik D.M.
High resolution equipment for the future spacecraft «Resource-PM»
Baklanov A.I., Blinov V.D., Gorbunov I.A., Zabiyakin A.S., Malakhov I.A.
System-mathematical simulation of engine air hydraulic power supply
Goryunova N.R., Goryunov A.A.
Conversion of gas turbine engine oil system
Boev A.A., Grishanov O.A.
Experimental research of internal heat transfer in the vortex heat generator
Zhornik M.N., Piralishvili S.A., Mogileva K.A.
Development of a solar battery orientation robot system for small spacecraft
Beznyakov A.M., Vlasov V.A., Malenin E.N.
Analysis of the thermal state of aircraft engine supports
Vinogradov A.S., Badykov R.R., Fedorchenko D.G.
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.
Experimental verification of the specified characteristics of a solar battery at the stages of production and ground operation
Shuplyak Y.P., Sorokoletov V.I.
Engineering education on level learning
Shehonin A.A., Tarlykov V.A.
Simulation modeling of stock markets
Steryakov A.A.
Basic approaches and requirements to the formation of polyplatform integrated automated system of aircraft life cycle support based on the product electronic definition
Nazarov V.V., Shabalkin D.Y., Polyanskov Y.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.
Problems of unmanned spacecraft reengineering in abnormal flight situations and their knowledge-based solutions
Akhmetov R.N., Makarov V.P., Sollogub A.V.
Improvement of the resolution on the basis of use of spatial filters
Savelyev D.A., Khonina S.N.
Ways of the development of the radar space systems of the remote sensing of the Earth
1 1.
Development of information support for the spacecraft controlalgorithm design process
1 1., 1 1.
Features of adaptation of first-year students of SSAU in the application of computer technologies of training
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.
Analysis and ballistics project the gun tube system with a joined drive on chamber
Safronov A.I., Potapenko V.V.
An algorithm for extracting invisible information from scanned polygraphic products
Glumov N.I., Mitekin V.A., Sergeev A.V., Fedoseev V.A.
Modelling changes of condition of aircraft hydraulic system working fluid
Gareyev A.M.
Experimental simulation of registration of outer space objects
Baryshev Y.Y., Syomkin N.D., Voronov K.Y.
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.
Fuzzy-controller simulation model as a tool of optimization of a limited availability ground handling system at a hub airport
Romanenko V.A.
Peculiarities of starting a spark-ignition gas fuel internal combustion engine
Shishkov V.A.
Research of the possibility of thermal conditions LREST using an infrared thermal imaging system
Ryzhkov V.V., Silyutin M.V.
Analysis and ballistics design of a laboratory installation system a small calibre with a joined drive on chambers
Safronov A.I., Zorkin V.A., Potapenko V.V.
Research of the operability of an air-fuel lubrication and cooling system of gas turbine engine rotor bearings
Klimov V.N., Dud’ev D.Y., Sigaylo V.Y., Klimov N.I., Mashkov Y.K.
Problematic issues of assessing the strength of axisymmetric parachute systems by conducting breakdown tests in flight experiments
Ivanov P.I., Kurinnyy S.M., Krivorotov M.M., Shmerova G.V.
Selecting a squeeze film damper model for solving problems of gas turbine engine rotor dynamics
Leontiev M.K., Kutakov M.N.
Efficiency of aft diffusers in vacuum systems of test benches for high-altitude firing tests of low-thrust liquid rocket engines
Galperin R.N., Gulyaev Y.I., Ivashin Y.S., Nigodjuk V.E., Ryzhkov V.V., Sulinov A.V.
Terminal control of aerospace system subhypersonic first stage
Balakin V.L., Kovalyov A.V.
Influence of the suspension system on the accuracy of the aircraft modal testing results
Berns V.A., Dolgopolov A.V., Zhukov E.P., Marinin D.A.
Research of hydrodynamic processes in the lubrication system of gas turbine engines
Gulienko A.I., Shchurovskiy Y.M.
Investigation of the seizing mechanism of aviation hydraulic drive spool–and–sleeves
Gareyev A.M., Popelniuk I.A.
Experience in the development of 11Д58MФ liquid rocket engines
Smolentsev A.A.
Conceptual model of the formation of flying skills in the process of training using flight simulators
Godunov A.I., Kuatov B.Z., Yurkov N.K., Kurtaev S.Z.
Information support of aviation embedded information and control systems lifecycle
Akimova T.E.
Method of choosing spacecraft design characteristics on the basis of creating task-oriented systems of computer-aided design
Kucherov A.S., Kurenkov V.I.
Dynamic construction of the educational process in an integrated learning system
Grinberg G.M.
Determining the angle of advance of ignition when switching from petrol to gas depending on fuel mixture burning rate
Shishkov V.A.
Developing models of information-analytical monitoring system design, engineering and manufacturing processes aircraft companies
Zheleznov O.V., Blyumenshteyn A.A., Chernikov M.S.
Аcoustical-mechanical sound generators for creating an acoustical impression of а car
Starobinski R.N., Krasnov A.V., Kovaleva A.A., Vilch N.V.
Constructing the specification for the on-board realtime control algorithm
Tyugashev A.A., Bogatov A.Y.
Reduction of the focal spot size in high-aperture focusing systems at inserting of aberrations
Pelevina E.A., Khonina S.N.
Inkjet heat transfer working model phone (fuel transportation) refrigerator drip emitters prospective spacecraft
1 1., 1 1., 1 1.
Solving the problem of stabilizing program deployment of an orbital tether system taking into account limitations on the rotary motion of the tip body
1 1., 1 1.
Motion trajectories of the vehicle with mass injection pre-compressor cooling turbojet engines as the first stage of aircraft-space systems
1 1., 1 1.
Statistical modeling of the process of serving the leaving passengers at the international Kurumotch airport
Romanenko V.A.
3D model didactic properties investigations for geometrical modeling principles training
Ivashchenko V.I.
Optimizing the propulsion of a hypersonic accelerator aircraft of a two-stage aerospace system
Balakin V.L., Bebyakov A.A., Kotchyan A.G.
Analysis of schemes and methods of hydrodynamic cleaning of hydro-fuel system units
Sanchugov V.I., Reshetov V.M.
Disturbed transatmospheric motion of the first stage of an aerospace system
Krikunov M.M.
Analysis of load balancing algorithms using discrete event simulation
Khayrutdinov A.R., Vostokin S.V.
Operation of an electronic system of control for spark-ignition gas fuel internal combustion engines in ignition misses
Shishkov V.A.
The concept of generalized method of calculation and design of wet cleaning duct GTD
Silaev B.M., Malcev E.N.
Development of elements and parameters of LNG fuel system with cryogenic piston pump and gas receiver for road gas turbine locomotive
Bukin V.A., Rudenko V.F.
Imitation models of aircraft hydraulic units with account for typical faults
Gareyev A.M., Popelnyuk I.A., Stadnik D.M.
Biological module “BiNOM” for cubesats of the SamSat family
Zakharov V.P., Konyukhov V.N., Bakhtinov P.I., Molchkov E.V., Kornilin D.V., Konovalov S.G.
Peculiarities of using hot-air balloons in tests of parachute systems
Kurinny S.M., Krivorotov M.M., Baranichenko E.A.
Prospective lines of improving the process of evaluating the technical condition of aircraft hydraulic system working fluid
Koptev A.N., Gareyev A.M., Popelnyuk I.A.
Mathematical model of fuel sloshing in the measuring channel of the fuel expenditure control system
Kryukov Y.A.
Using the theory of dynamic analogies for modelling automated manufacturing systems
Gareyev A.M., Koptev A.N., Gareyev T.M.
Research of a sleeve connection of the aircraft pipeline under the influence of dynamic loading
Agafonov V.M., Pykhalov A.A.
Iodine as an alternative propellant for electrojet engines
Ostrovskiy V.G., Smolentsev A.A., Scherbina P.A.
Thermal medical software hardware-based thermal imager COX CX - 320U
Davydov I.E., Agafonov A.N.
Internal controls board computer system running real time operation system as an iterative aggregate
Dolbnya N.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.
Development of a virtual prototype of gasturbine engine at the stage of conceptual thermogasdynamic designusing the CAE-system «ASTRA»
Tkachenko A.Y., Krupenich I.N.
Pressure pulsation dampers as a means of improving the inherent vibroacoustic charateristics of hydraulic test rigs
Berestovitsky E.G., Gladilin Y.A., Kryuchkov A.N., Fyodorov A.Y., Frantov A.A., Shakhmatov Y.V.
Investigation of thermal conditions nozzle blades with a cyclone-vortex cooling system
Veretennikov S.V., Khasanov S.M.
Dynamic positioning of a manned submersible over the service object
Alekseev A.V., Olenin A.L., Smirnov G.V., Fendrikov A.N.
Analysis of on-board equipment robustness on the basis of COTS-products
Yefanov V.N., Bondarev A.V.
Tether parameters consideration during motion simulation of orbital tether system
1 1.
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 of the adaptive graphic and geometric training for the computer aided design teaching
1 1.
Mixing parameters investigations and methods of approach to calculations and development of the thrusters with a spray-centrifugal scheme of NT and NDMH mixing on the confusion chamber wall in considered
1 1.
Reliability indicators of information control systems with hardware and software failures as complex time functions
Maryukhnenko V.S.
Solving the least squares problem using the method of an extended set of equations with sparse matrix
Gogoleva S.Y., Zoteeva O.V.
Means of illumination of an underwater situation of manned submersibles
Alekseev A.V., Belenky V.N., Olenin A.L., Smirnov G.V.
Comparison of mass properties of high- pressure cylinders with cryogenic fill for a throttle cooling system
Dovgjallo A.I., Sarmin D.V., Uglanov D.A.
Mathematical modeling of the evolution of a tribosystem in the process of formation of equilibrium roughness of a frictional contact
Kolesnikov I.V., Koropets P.A., Manturov D.S., Shakhmatov Y.V.
Technology of low-emission fuel combustion and conceptual structure of the combustion chamber of a gas-turbine power plant
Tsybizov Y.I., Tyulkin D.D., Vorotyntsev I.E.
Vector optimization of the parameters of a queueing system with partial mutual assistance between channels
Romanenko V.A.
Theoretical and experimental investigation of the photographic reconnaissance plane instrument bay thermal state
Nikolayev V.N.
Use of the methods of the structural programming to form the «reliability» diagrams of the fuel supply system of the gas turbine engines with the control elements failure order of no less than four
Smurova N.A.
On selection of automatic control system for crvogenic fuel gas turbine engine
Bukin V.A.
Analysis of control programs and climb paths of the hypersonic first stage of an aerospace system
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.
Set-theory model of the aircraft hydraulic system working fluid state
Koptev A.N., Gareyev A.M., Popelnyuk I.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.
Spacecraft power supply system using additional low-power sources of energy
Kargu D.L., Beznyakov A.M., Nemirov A.V.
Possibility of using leo satellite communication systems for on-line data interchange
Davydov D.D.
Developing a problem-oriented system for automated design of observation space vehicles capable of interacting with a PDM-system
Yakishchik A.A.
Method and apparatus for evaluating the efficiency of energy transfer from combustion products to abrasive particles at the exit of a sand blaster nozzle
Kornilin D.V., Medvedev M.V.
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.
Creation of a data retrieval system for choosing the optimal cutting tool in manufacturing aircraft engine parts
Shulepov A.P., Meshcheryakov A.V., Ramzaeva E.A.
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