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Methodological and analytical support for the creation and maintenance of aerospace industry technological development strategic programs
Gaponenko O.V.
Algorithm of planning operational and financial activity of a manufacturing enterprise
Bogatyryov V.D., Yesipova O.V.
Method of constructing diagnostic models of aircraft hydraulic systems in an analytic form
Kovalev M.A., Borodkin G.V., Khablo I.I.
Selection of a nanosatellite group separation program for cluster launching from the «Soyuz» launch vehicle orbiter
Avaryaskin D.P., Shcherbakov M.S.
Turning and milling layered details
Kondratyev A.I., Pronichev N.D., Kuznecov A.V.
Providing carrier rocket motion controllability on the basis of design smoothed wind profile application
Yendutkina Y.A., Titov B.A.
Development of the design procedure of the shaping rigging with the use of the integrated information systems
, ,
3D-model of compressor rotor blade development
Boyarov K.V., Ryazanov A.I., Chempinsky L.A.
Nominal motion control program in a supersonic carrier aircraft
Balakin V.L., Potapov V.I.
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.
Design of method of project complex selection for investment program of project organization
Bogatyrev V.D., Gorbunov D.V.
About the centre of science-educational of laser systems and technologies at faculty DLA SSAU
1 1., 1 1., 1 1.
Determination of the optimal parameters and engine layout for a strike unmanned aerial vehicle
Zinenkov Y.V., Lukovnikov A.V., Agaverdyev S.V.
Internal combustion engine some cooling system components detailed calculation
Kolomin I.V., Ajukov A.A., Birjuk V.V.
Choosing a program for controlling the deployment of an orbital tether system with deployment speed limitations
Ishkov S.A., Xiaoye X., Filippov G.A.
Compressor blade profile reverse-engineering: building of middle curve and symmetrical profile
Shabliy L.S.
Technical approach for estimation of engineering level of universal launch complexes for space launch vehicles witn use of overal parameter
1 1., 1 1., 1 1., 1 1.
Realization of the multichannel cnc machining methods
1 1., 1 1.
Deployment and stabilization of the motion of a space tethered system in a lunar orbit
Ledkova T.A., Zabolotnov Y.M.
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 model of financing production of an industrial enterprise of space-rocket industry
Inozemtsev V.V.
Optimization of casing on mass with ensuring requirements for deduction of the ragged blade
Krundaeva A.N., Gabov D.V., Maralev A.Y.
Kick-stage control by navigational data of satellite navigation system
1 1.
Models competence of bachelor and master’s degree for innovation machine building
Belashevsky G.E., Kozlov D.M.
Optimal command control of hypersonic aircraft flight path in conditions of atmospheric disturbances
Krikunov M.M.
Thermal medical software hardware-based thermal imager COX CX - 320U
Davydov I.E., Agafonov A.N.
End mill design and manufacturing with modern multi-axis grinding machines
Skuratov D.L., Kuznetsov A.V., Oparin V.M., Sazonov M.B.
Scalable distributed systems of competitive interacting processes and their optimality
1 1.
Centrifugal force field effect consideration in dynamics investigation of blade wheels
Davydov D.P., Ermakov A.I.
Optimal control of spacecraft motion in the vicinity of Eros 433 asteroid
Shornikov A.Y.
Iteration procedure of choosing a low-thrust rendezvous transfer control program in problems of space debris disposal in the geostationary orbit
Philippov G.A.
Correct numering of two-pole directed graphs
Popova-Kovartseva D.A.
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.
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.
Ways 3D parametrization TJ blades for use CAD/CAM/CAE packages
Smelov V.G., Shitarev I.L.
Control program for noncoplanar heliocentric flight to Venus of non-perfectly reflecting solar sail spacecraft
Khabibullin R.M.
Construction of an upper stage flight pattern for placing a group of spacecraft into an orbit plane with the required angular distance between the satellites
Poplevin A.S., Panov N.A.
Economic-mathematical model of optimizing financial cycles of bearing industry enterprises
Geraskin M.I., Yegorova V.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.
Methodology of the adaptive graphic and geometric training for the computer aided design teaching
1 1.
Determination of optimum plans of Earth Remote Sensing spacecraft detailed survey by the use of a graph
Buzuev K.V.
Problem of optimization of the number of processors in distributed processing
Pavlov P.A.
Control over the deployment of an orbital tether system of great length
Wang C., Zabolotnov Y.M.
Optimal program of controlling continuous low thrust in the flight between noncoplanar elliptical and geostationary orbits
Fadeenkov P.V., Ishkov S.A.
Conception of the student work place arrengement for the computer aided design base teaching
1 1., 1 1.
Optimal control of the angle of attack of a hypersonic flight vehicle
Bebyakov A.A.
1 - 46 of 46 Items

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