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Authors
Approximation of characteristics of linear displacement inductive sensors using modified Gaussian function with a first order difference argument
Tingaev V.S., Matyunin S.A., Mednikov V.A.
Optimization of model positional harakterstik of the electromagnetic sensor of the linear peremeshchny
Tingaev V.S., Matyunin S.A., Mednikov V.A.
Approximation of forces of fluid film bearing lubricating layer using machine learning methods
Kazakov Y.N., Stebakov I.N., Shutin D.V., Savin L.A.
Ballistic analysis of a mission to Jupiter’s moon Callisto with landing on the surface
Kovalev V.V., Marchenko A.D., Starostina T.V., Sharipova A.R.
Design procedure of factor of rigidity of aviation elastic elements
Barmanov I.S.
Parameters transducers of the blade’s dynamic movements of turbounits based on nonlinear approximation of primary signals
Chernyavskiy A.Z., Danilin A.I., Danilin S.A.
Programme realization of mathematical operations of flow multiplexing and demultiplexing for network models
Bakhareva N.F.
Analytical approximation of aircraft dynamics model in problems of approximate optimal control synthesis
Blinov A.O., Gurman V.I., Fralenko V.P.
The device for the determination of blades oscillation parameters based on nonlinear approximation of primary transducers signals
Danilin A.I., Chernyavskiy A.Z., Danilin S.A.
Use of approximative analysis outcome of experiment in problem of diagnostics technical conditions of hydraulic systems
Malchikov K.Y., Logvinov L.M., Kovalev M.A.
Analytical description of stress–strain diagram in stress and stability analysis
Saveljev L.M.
Development of the information technology for estimation of fundus image geometric parameters
Kuprijanov A.V., Ilyasova N.Y.
Comparative analysis of parabolic lens and axicon in geometric and scalar paraxial optical models
Ustinov A., Karsakov A.V., Khonina S.N.
Solving the polynomial approximation problem with use of the iterative kachmazh method
Ivanov A.A.
Application of the artifical neyral networks theory methods for generalization and representation charachteristics of aviation gas turbine engines axial compressors
Grigoriev V.A., Kalabukhov D.S., Rad'ko V.M.
Agreement between criterial equations of heat transfer in the process of cooling aluminium ingots and experimental data
Gorshenin A.S., Krivosheev V.E.
Ion source of DMS-01 scientific equipment for «AIST no 2» small spacecraft
Semkin N.D., Piyakov I.V., Rodina M.A., Rodin D.V.
Approximate correlative-spectral analysis of temperature patterns of combustion chambers
Prokhorov S.A., Ilinsky S.A., Aleksandrova T.G., Solovyova Y.V.
1 - 18 of 18 Items

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