Vol 15, No 3 (2014)

Articles

Model-algorithmic software decision support in information systems management

Aklanov F.A., Kovalev D.I., Tueva E.V., Zelenkov P.V., Pershakova C.K.

Abstract

The creation of information systems management (1MR) of the enterprise and its model-algorithmic software is explained. System components provide support to the decision maker (DM), after finding the optimal plan reserves distribution between consumers and procurement planning. The objective of the procurement is based on the analysis of sales data, current consumer needs, and the purpose is the procurement plan, in which the level of sales will be maximized. It is shown that an important function of the information management system is to support decision making while ensuring cooperation between all departments and branches of the company and prompt submission of data on the balance of goods in warehouses, its arrival, purchase orders, implementations counterparties and on the current financial status of the enterprise as a whole.
Siberian Aerospace Journal. 2014;15(3):10-15
pages 10-15 views

Data mining tools for prospective students’ success rate prediction

Akhmedova S.A., Vishnevskaya S.R., Koromyslova A.A.

Abstract

The aim of that study was prospective students’ success rate prediction in case if they are enrolled at university. For this purpose different classification and prediction methods were used namely support vector machines (SVM), neural networks and fuzzy systems which were obtained by using genetic and bionic algorithms and their modifications. Firstly, meta-heuristic called Co-Operation of Biology Related Algorithms (COBRA), that has earlier demonstrated its usefulness on CEC’2013 real-valued optimization competition benchmark and its modification for solving constrained optimization problems, was applied to SVM-based classifiers design. Then genetic algorithm was used for neural networks and fuzzy logic systems automatic generation. Various benchmark classification problems were solved with those approaches. It was established that support vector machines, neural networks and fuzzy logic systems developed in that way outperform many alternative methods on mentioned benchmark classification problems. So the workability and usefulness of proposed classification or prediction algorithms were confirmed. After that for solving of prospective students’ success rate prediction problem, in case if they are enrolled at university, information about them obtained during the operational period of Admission Committee was gathered and preprocessed. Eventually it was established which kind of information about a prospective student is enough for determining whether he or she will or will not pass end of first semester exams in case of enrollment. Moreover, it should be noted that support vector machines generated by collective optimization method COBRA have shown the best results.
Siberian Aerospace Journal. 2014;15(3):16-20
pages 16-20 views

Modeling of a horn-based lattice based on field distribution in the plane of aperture of the horn

Bakin A.M., Trifanov I.V., Oborina L.I., Ismailov B.N.

Abstract

The method for the approximate simulation thrust antennas in EHF frequencies where direct modeling with the help of the software packages is complicated due to the demanding computing possibilities of computers is proposed. The proposed method is based on the restoration of the far field distribution of the field in the plane of the aperture of the horn. The horn antenna which was applied to researches, represents a horn lattice which is the part of the pyramidal loud-hailer with sizes in aperture 12,4*12,4+0,01 mm, and a disclosure corner 17°30’, and also four sectoral loudhailers 3,8 ± 0,01 mm wide and a corner aperture 17°30’. The thickness of the wall of a loud-hailer of 1,1+0,1 mm, radius of interface of walls of 0,1 mm. The distance between axes of lateral loud-hailers is 17 ± 0,01 mm. High precision of an arrangement of loud-hailers is necessary for ensuring electric parameters and formation of differential and total directional patterns. The following operating modes of the antenna from the horn lattice are possible: simultaneous reception-transmission of a signal with various polarization at different frequencies; signal transmission with various polarization at one frequency; signal reception with various polarization at one frequency. First of all, the irradiator directional pattern is characterized by the sizes of aperture loud-hailers and their electric characteristics, and also frequency characteristics of given waves. The paper applies the analysis of individual elements of the lattice in the software package CST Microwve Studio and subsequent treatment of the resulting field distribution in the lattice points to restore the far field.
Siberian Aerospace Journal. 2014;15(3):21-27
pages 21-27 views

About nonparametric control of object with memory

Bannikova A.V., Korneeva A.A., Kornet M.Y., Sergeeva N.A.

Abstract

This article discusses the problem of nonparametric control of discrete-continuous process of BOF steel smelting. The problem of identifying objects with stochastic discrete - continuous nature of the process is also considered. Additionally, the problem of identification and management of multidimensional stochastic systems is investigated in a closed loop, i. e. in the form of a macroscopic object, including a system to - regulator. Moreover, the emphasis is not only on the presence of random noise in different channels of communication, but also on the lack of information about the course of the process. Special attention is paid to the case when the design is applied to control the impact of a real object in a distorted. The dual-process control scheme, in which the control circuit comprising operator saved but added external control loop that carries the features of dualism is proposed. This control scheme allows to increase the quality of management of the entire system as a whole significantly. Some results of numerical simulation of the two-loop circuit control are given. Some results of the modeling process of BOF steel smelting show that the process is conducted in the framework of technological regulations, however, it is not enough for quality control smelting process.
Siberian Aerospace Journal. 2014;15(3):28-34
pages 28-34 views

Speech-based emotion recognition of the distant student with adaptive intellectual information technologies

Brester C.Y., Vishnevskaya S.R., Semenkina O.E.

Abstract

To overcome the negative sides of distance education and to develop the communicative competence of the distant student, it is necessary to improve the interactive dialogue systems, in particular, to realize the opportunity of speaker state recognition. Although lots of excellent results have already been achieved in this sphere, there are some open questions. Recently scientists have developed various program systems which are good at extracting numerical characteristics from speechsignals. Unfortunately, the amount of features might be huge that becomes a challenge for classification models. Therefore it is significant to determine relevant features from data sets. In this paper we consider the feature selection procedure that is based on the adaptive multi-objective evolutionary algorithm and investigate its efficiency in combination with different classification models. Generally, the feature selection procedure can be organized as a wrapper approach or a filter one. Compared with the wrapper approach, the second technique requires less computational resources and also demonstrates good results. Therefore in this research we implemented the feature selection procedure according to the scheme of the filter approach. Furthermore, to avoid choosing the genetic algorithm settings we developed a self-adaptive modification of the conventional multi-objective genetic algorithm. Due to application of the self-adaptive heuristic optimization procedure it became possible not only to improve the performance of involved classifiers but also to reduce the number of selected features essentially. Obtained results demonstrate high performance of the developed algorithmic scheme and imply the reasonableness of its usage in the dialogue system modules for recognition of student emotions distantly.
Siberian Aerospace Journal. 2014;15(3):35-41
pages 35-41 views

Increase of reliability level of information systems

Bychkov S.S., Popov A.M., Zolotarev V.V.

Abstract

In the presented work the question of increase of reliability level of information systems is considered. The problem is solved by creation of mathematical model of information system, as the special case possessing increased requirements to level of reliability, the system of electronic document flow is taken. In this work the analysis of existing methods of an assessment of reliability level of information systems is carried out, the methods allowing to raise reliability level of information system at various operational phases of information system are also considered. Within the methods of an assessment of reliability level of information systems methods of forecasting of level of reliability of information system, and also probability of emergence of mistakes are considered at operation of information system. Within the carried-out work the authors have combined the algorithm of increase of reliability level of information system, in the conditions of need of continuous operation of information system on the basis of application of methods of mathematical modeling was created. The work of the combined method also includes the work of a dynamic method of an assessment of reliability level of information system which is the indicator of achievement of an optimum condition of reliability level of information system. The results of work can be applied to carry out pilot studies concerning ensuring information security, optimization of work of information systems.
Siberian Aerospace Journal. 2014;15(3):42-47
pages 42-47 views

Goldshtik’s problem of pasting of vortical currents of an ideal liquid in the axially symmetric case

Vainshtein I.I., Fedotova I.M.

Abstract

We consider that axially symmetric model of vortical flows of an ideal incompressible liquid with discontinuous nonlinear vorticity. The proposed model is a generalization of the Lavrentev’s scheme planar separated flows of an ideal fluid for the axially symmetric case. In terms of the the flow function we solve the Dirichlet problem for the inhomogeneous elliptic Euler-Poisson-Darboux equation with discontinuous nonlinearity is relative to the decision in the right part of the equation. This problem is a generalization of the well-known problem of Goldshtik of pasting planar vortical and potential flows of an ideal liquid on the axially symmetric case. The existence of the so-called trivial solution, which corresponds to the potential flows in the whole domain is shown. On a model example (flow in the ball) we establish the existence of two non-trivial solutions. For the general case of the problem we prove the existence of a nontrivial solution, indicating the existence of this class of axially symmetric vortical flows of an ideal liquid. In the model it is assumed that the stationary flow of an ideal liquid is a limiting flow of a viscous with viscosity tends to zero.
Siberian Aerospace Journal. 2014;15(3):48-54
pages 48-54 views

Simulation and optimisation in technological systems with distributed parametres

Demidenko N.D., Kulagina L.V.

Abstract

The article presents a method of simulation and optimal control for rectification plants, containing technological furnaces and rectification columns. This complicated system is shown as a system with distributed parameters, as for static and dynamic modes simulation a mathematical formalism of differential equations in partial differential was applied. As a rule scientific literature deals with operation modes outcomes for single plants. Due to complicated mathematical formalism and computation investigations dealing with a number of objects with distributed parameters are infrequently. The optimal control tasks solutions for complicated plants are poorly shown in scientific literature A phenomenological approach was applied for mathematical model of heat processes in technological furnaces and separation processes in multicomponent mixtures for rectification columns. The model contains partial differential equitations for heat- and mass-exchange processes and hydrodynamics for flue gas flows in technological furnace and mass-exchange equitations for rectification column. Described processes occurs with recirculation flow interaction and heat-exchange processes' boundary conditions for rectification columns are described in ordinary derivatives. The conditions are given at the opposite ends of the plant. The optimal control modes solutions were formulated an optimal control task for desired product and necessary conditions for optimality. Due control functions are included in the main boundary derivatives, control variations in the range and on the boundary are dependent, this works on dual problem structure. Arguments of variational calculus was applied. Necessary conditions for optimality are containing original boundary-value problem conjugated relatively to the Lagrangians. Original and boundary tasks solution determines optimal control and technological processes parameters. The article gives numerical outcomes with control of flow of raw materials in debutanizer plant for sulfuric acid alkylation of isobutane with butenes. A numeric algorithm was worked out. The peculiarity of the algorithm is solving a boundary conditions tasks for some parameters at the opposite ends of the area. Moreover Lagrangians for conjugated system are given at a finite time. Optimal characteristics of heat-exchange process of desired product in the dephlagmator and cube were obtained.
Siberian Aerospace Journal. 2014;15(3):55-62
pages 55-62 views

Structural analysis in ANSYS of the axial flux permanent magnet generator

Karpenko E.V., Kolbasina N.A., Morozov D.I.

Abstract

The object of this research is the axial flux permanent magnet generator. In the article the necessity and technique of checking calculations of the generators is described. A finite element analysis is provided as a tool for these calculations. Its results for the specified parameters are at the end of the article. The main stages of the calculation and the possibilities of the environment ANSYS were examined. To simplify the work in the ANSYS environment software that allows you to build a simulation model in an automated mode was developed. Using our software can be useful for design and technological production tasks, improving competitiveness and increasing demand for the product. The resulting computational model in ANSYS environment allows you to get a complete picture of the stress-strain state of the computational model. Developed software as a part of an automated design environment of the generator, greatly simplifies the process of solution, because it requires only the input of the parameters without entering commands in the language APDL. Such automated model significantly reduces the time spent on the construction of computational models, and excludes cases of incorrect commands for environment ANSYS. In the future, this software will significantly simplify the design and testing of new designs generators.
Siberian Aerospace Journal. 2014;15(3):63-67
pages 63-67 views

Assessment of stability learning algorithms large artificial neural networks of biometric application

Kachalin S.V.

Abstract

The problem of increasing the speed, stability and efficiency of known and emerging algorithms for training large artificial neural networks is considered. To solve this problem it is proposed to create the most balanced multi-criteria performance comparison of different learning algorithms, enter a numerical estimate of the learning parameters and systematically carry out work to improve them. It is argued that resistance training of neural networks is an analogue of the assessment procedure of the condition number of matrices of linear algebra. We propose a measure of stability training, given the connection between this indicator with the computational complexity of learning algorithms, as well as with a number of examples on which the algorithm is efficient. We discuss the effect of increasing the stability by supplementing the training sample synthetic image examples of “your”. The optimum amount of additional synthetic examples, the addition of which can reduce the number of examples in the training set is provided. A block diagram of a promising means of training neural network converters, which introduced the third machine reproduction examples image of “Its” is given. To control the number of synthetic examples, it is proposed to create a table of restrictions for the first machines based on expert opinion.
Siberian Aerospace Journal. 2014;15(3):68-72
pages 68-72 views

Hermite bicubic collocation method in domain with curvilinear boundary

Kireev V.A.

Abstract

In this paper the collocation method with Hermite bicubic basis functions is considered, applied to the first boundary value problem for an elliptic equation in a domain with a curved boundary. The collocation method has some advantages compared with Galerkin finite element method: no need to compute the integrals for the determination of the coefficients of the stiffness matrix. Hermite bicubic functions belongs to the class C 1. The consistent with the boundary mesh is constructed for solving the problem. The grid is consistent with the border so that two nodes in irregular cells were lying on a curvilinear boundary. This approach allows to reduce the total number of basis functions in the domain. As an internal collocation nodes the points of the set of Gauss are taken. The collocation points are distributed evenly on a curvilinear boundary. Under such arrangement, the total number of collocation points equal the total number of basis functions with the given boundary conditions. The problem is reduced to solution of a linear system Au=f where A is a square matrix. The results of numerical experiments of solving Poisson equation with different right sides show that the algorithm of solution has the convergence of high order.
Siberian Aerospace Journal. 2014;15(3):73-77
pages 73-77 views

Analysis of problems in the research area of software reliability: a lot of stages and architectural aspect

Kovalev I.V.

Abstract

In the survey, it is shown that estimation and reliability analysis should be performed at each step, create a failover. Due to the fact that there is no single approach, methods and parameters for estimating the reliability of Software, there are many models and algorithms, tested virtually, but has several disadvantages. The main drawback of all models is "specialization ". Models are always tied to any one phase of software development, and sometimes have a purely theoretical value due to the fact that they must be used the data obtained at other stages of development, and the authors of such models usually consider this fact of secondary importance. The most promising approach is aimed at creating some hybrid model, which includes all the advantages of a well-validated models and algorithms. Existing models and algorithms need to be modified so that the output of one model became the input for the other; to provide a unifying parameters, units of measure conversion, normalization of data and satisfying the current requirements and trends, such as object-oriented analysis and programming. From this review we can see that it is very important to use as much a priori information before beginning each phase of creation, as this will provide the most appropriate and accurate results. The analysis of methods, models and methodologies in the field of creation of reliable, fault-tolerant (Software) is carried out. Attempts to systematize and unify the existing methodology are made. The multiple steps involved in the creation and architectural aspect within the entire life-cycle fault-tolerant software are taken into account.
Siberian Aerospace Journal. 2014;15(3):78-92
pages 78-92 views

Nonparametric models of the Hammerstein dynamical objects

Koplyarova N.V., Sergeeva N.A.

Abstract

The problem of nonlinear dynamical systems of the Hammerstein type identification is considered. Systems in the conditions of partial parameterization are considered. In this case structure and parameters of equation, which describe the linear dynamical part of the object, are unknown. The common type of nonlinearity is assumed to be known with the set of parameters. It is required to construct the mathematical model of the investigation system, which is based on the input-output measures sample. The proposed method of dynamic objects modeling is based on the nonparametric estimation of linear and nonlinear parts of the system. At first it is offered to estimate the nonlinear element parameters, and to the input of system consistently applied different input actions. Then the linear dynamical part model can be constructed as a Duhamel integral, where the impulse response function is estimated with nonparametric algorithm. Presented algorithm doesn’t require a complete priory information about the object structure. In the work the results of computer modeling of the Hammerstein type systems with the quard and the saturation nonlinearity are shown. This nonparametric model can describe the investigation systems with different types of nonlinearity, in conditions of noise in the measure channels, and with different sample sizes and input actions. The numerical researches show that the algorithms should be used to identify the Hammerstein type nonlinear systems.
Siberian Aerospace Journal. 2014;15(3):93-99
pages 93-99 views

Analysis of electromagnetic processes in ac-dc converters with possibility of reverse flow of energy and increased efficiency

Krasnobaev Y.V., Zakharov V.V., Karnaukhov M.A.

Abstract

The paper considers the questions of energy transfer in a charge/discharge autonomous power supply device. Power circuit of considered charge/discharge device is based on the scheme of reversing up/down converter with the switching mode of power transistors at zero-voltage that ensures high efficiency of device. In the course of analysis of electromagnetic processes in the converter, mathematical expressions that describe the transfer of energy, from the side one to the side two of the reversible converter have been obtained. Using the obtained mathematical expressions, a method and algorithm for calculating RMS current through elements of the power converter circuit using parameters of the power circuit elements and parameters of energy transformation, in particular, using reverse displacement current of a choke, providing switching mode of power transistors at zero voltage have been developed. Correlation between RMS current through a choke and power transistors, and value of reverse replacement current of a choke for a number of modes are given graphically. All correlations were obtained at fixed power at the side two and variation of voltage value at the side one of converter. Analysis of obtained correlations has shown growth of RMS current through power circuit elements of the converter at increasing reverse displacement current of a choke, which corresponds the theoretical requirement. Developed method, algorithm and program for the calculation of RMS current through elements of the power circuit of converter can be used for solving design problems of the charge/discharge device which based on the scheme of reversing up/down converter with the switching mode of power transistors at zero-voltage, and for solving the problem of minimizing the total static and dynamic energy losses in the converter.
Siberian Aerospace Journal. 2014;15(3):100-106
pages 100-106 views

About computer research of H models

Medvedev A.V., Mihov E.D.

Abstract

A modeling of discrete-continuous processes with “tubular” structure in space “input - output” variables is considered. Moreover general scheme of the test process, including not only the input-output variables but also intermediate is discussed. Attention is drawn to the essential factor which shows that a change of input variables carries out through various time intervals. This is due to various output variables controlled by electrical means, as a result of chemical analysis and physico-mechanical tests. In this regard the various component models for different process output are given. The question is analyzed in the identification of “narrow” and “broad” sense. Recursive algorithm provides estimates of the parameters of adaptive models based on stochastic approximation method. Modelling of processes of this class differs significantly from conventional parametric models representing the surface in the same space. When constructing students’ parametric models “tubular” processes require the use of appropriate non-parametric indicators. The recurrent algorithms estimate the parameters that take into account the relevant indicators in parametric models are also given. It may be noted that the H-pattern is more common in comparison with conventional. That is, if the test process does not have “tubular” structure, then H-model in this case, goes to the class of well-known models of free-wheeling systems. Thus, the adaptive models freewheeling processes change somewhat, unlike conventional. Some special examples of modeling “tubular” processes, from which it follows that the “tubular” processes take place in the space of fractional dimension. We present the case of functions of several variables and analyzed the situation where, over time these variables can “disappear” and “occur” again. Statistical modeling method, has been carried out numerical study of H-models with different sample sizes measuring input-output variables and different levels of noise. As a result of this study shows that the dimension of the space in which the process takes place, not only fractionally, but also changing. It turns out that the calculation of fractional dimension space can be done in different ways.
Siberian Aerospace Journal. 2014;15(3):107-113
pages 107-113 views

The improvement of technology manufacturing units of aerospace industry

Ponomarev S.I., Eresko S.P., Eresko T.T.

Abstract

This paper presents a description of the improvement of the technology of manufacturing parts and assemblies of aerospace production using computer-aided design and process control. Theoretical framework and algorithms for constructing process of manufacturing parts and assemblies to the aerospace industry using different connection methods of heat-resistant materials, such as diffusion bonding, designed on the basis of conducted theoretical and experimental studies, the authors proposed a patented process connection “Connection method superalloy cobalt-based ceramic based on silicon nitride” and tooling “Installation for metal products”, as well as obtaining registration in the database of the Russian Federation “Attributive database to create processes for production of aerospace components manufacturing diffusion bonding” and “Attributive database processing equipment, tools and equipment for machining aerospace parts production ”. During the execution of the works were solved the following problems: the algorithm of the adaptive management process of manufacturing parts and assemblies to the aerospace industry using diffusion welding in real time created: the database of materials used for the manufacture of parts and assemblies of aerospace manufacturing, the database of equipment, accessories and modes of machining parts different sizes and configurations, and the database of equipment, accessories and modes of obtaining permanent link of dissimilar materials by diffusion bonding. Based on the results, and created databases, provides guidance for the manufacture of one-piece ceramic-metal assemblies used in the aerospace industry. As an example, the developed method provides design technology of metal-ceramic assembly - the turbine rotor of the turbopump assembly. The proposed method for computer-aided design and manufacturing process control components and assemblies greatly simplifies the organization of work and reduces the pre-production in the manufacture of high quality components and assemblies of aerospace manufacturing.
Siberian Aerospace Journal. 2014;15(3):114-119
pages 114-119 views

Automatic landscape image annotation

Proskurin A.V.

Abstract

The image retrieval in the Internet and specialized datasets is the important task. For such retrieval is expedient to apply the systems of automatic image annotation (AIA) based on low-level features. Due to wide variety of images, it's sometimes useful to categorize images and to customize methods of AIA according these categories. In this article, the automatic landscape image annotation (ALIA) is discussed. Natural objects (rocks, clouds and etc.) on the landscape images often include just one texture. Because of that, for ALIA enough use of the machine translation model. In this model, the process of image annotation is analogous to the translation of one form of representation (image regions) to another form (keywords). Firstly, a segmentation algorithm is used to segment images into object-shaped regions. Then, cauterization is applied to the feature descriptors that are extracted from all the regions, to build visual words (clusters of visually similar image regions). Finally, a machine translation model is applied to build a translation table containing the probability estimations of the translation between image regions and
Siberian Aerospace Journal. 2014;15(3):120-125
pages 120-125 views

Solvability of a difference cauchy problem for multi-layer implicit difference schemes

Rogozina M.S.

Abstract

Difference equations arise in different areas of mathematics. Difference equations in conjunction with a method of generation functions give a efficient technique for studying the enumerative problems in the combinatorial analyses. Another source of difference equations is discretization of differential equations. Methods of discretization a differential equation is an important part of the theory of difference schemes, and also lead to difference equations [1]. In the case of implicit difference schemes its solvability presents a non-trivial question. In [2] investigated the stability of a two-layer homogeneous linear difference scheme with constant coefficients. In [3] to study the stability of multilayer homogeneous difference schemes applied theory of amoebas of algebraic hypersurfaces and a formula for the solution of the Cauchy problem in terms of its fundamental solution. In [4] for the two-dimensional case is investigated difference analog of the boundary value problem for Hormander polynomial differential operator. We investigate the solvability of difference equations with initial-boundary conditions of Riquier and consider them as implicit multi-layer difference schemes. Since this question reduces to solvability of systems of linear equations, we use linear algebra to give necessary and sufficient conditions and a simple sufficient condition for solvability in terms of coefficients of a polynomial difference operator. We show the relation of these results to the elimination algorithm for systems of algebraic equations with band matrices. The results can be applied for studying solvability of difference schemes and construction of monomial bases in quotients of the polynomial ring.
Siberian Aerospace Journal. 2014;15(3):126-130
pages 126-130 views

Features of differential and variational-differential formulations of the problem of the longitudinally cross bend of the core from inertia forces

Sabirov R.A.

Abstract

The variational-differential method of calculation of rectilinear cores stability on axial inertial loadings is developed. The formulations of the boundary value problem of longitudinal cross bending movements are calculated: differential formulation with a final and differential approximation of the allowing equations and variational-differential one. The task is reduced to the generalized problem of own numbers Ax = λBx - for an non-trivial vector x it is required to identify its own number λ, here A is a matrix rigidity, B is a matrix of internal forces of inertia. In considering the differential formulation of the task the main particularity of the inertial loads is that the discrete matrix B gets null values on the main diagonal (the rows of matrix can degenerate). Another feature is associated with the approximation of the differential equations by the method of grids, which forms the matrix B asymmetrical about the main diagonal. The generalized problem has no decision like its feedback form Bx = λ *Ax where λ * = 1 / λ . Brining to the problem of eigenvalues AB -1x = λEx and BA -1x = λ *Ex where A -1 and B -1 are the inverse matrix, E is the identity matrix, doesn’t give any result. Therefore transition from the differential formulation of a task to the variation formulation with sampling by a variational and differential method is executed. The algorithm of formation of matrixes A and B is developed for this approach, which is based on uniform properties of variations of functional. Here the matrix B is always symmetric to the main diagonal and is positively defined. Zeros on the main diagonal were presented because it is a feature of loading, however rows don’t degenerate. The technique of the solution of a task is shown. Examples of calculation of own values and forms of stability loss are given. The critical axial accelerations lose their stability and critical angular speeds for the cores rotating in a drum of the centrifuge when the core is fixed from both sides. Investigated the convergence of solutions from condensation of a finite-difference grid. Purpose: to develop a method of calculation of cores on inertial loadings.
Siberian Aerospace Journal. 2014;15(3):131-138
pages 131-138 views

Dynamics forecasting for electrical characteristics of spacecraft solar arrays by means of computational intelligence

Semenkina M.E., Semenkin E.S., Ryzhikov I.S.

Abstract

We consider the problem of forecasting the degradation process of spacecraft's solar arrays according to their available parameter changes measured together with the corresponding parameters of solar activity during the fulfilment of the real spacecraft's mission. The application of ANN-based predictors is proposed because of their generalization ability. In this paper, predictors automated design with self-adaptive evolutionary algorithms is suggested because of the ANN efficiency dependence on the choice of an effective structure and the successful tuning of weight coefficients. The adaptation of evolutionary algorithms is implemented on the base of the algorithms' selfconfiguration. In self-configuration technique, setting variants were used instead of the adjusting real parameters, namely types of selection, crossover, population control and level of mutation. Each of these has its own initial probability distribution which is changed as the algorithm executes. ANN-based predictors are automatically designed with the self-configured genetic algorithm and the self-configured genetic programming algorithm. In both cases the most informative features are selected for each neural network. Besides, the self-configuring genetic programming is used for the automated design of ensembles of ANN-based predictors. The performance of developed algorithms for automated design of ANN-based predictors is estimated on real-world data and the most perspective approach is determined. Self-configuring genetic programming algorithm for automated ANN design has the best performance among non-ensemble techniques. Self-configuring genetic programming for the automated design of ensembles presents the best result among all considered approaches.
Siberian Aerospace Journal. 2014;15(3):139-145
pages 139-145 views

Biometric stats: smoothing histograms based on small training sample

Serikova N.I., Ivanov A.I., Kachalin S.V.

Abstract

The question of improving the stability of statistical calculations with small training set by complications statistical processing raw data. It is shown that the accuracy of the estimation of the distribution law of small samples of biometric data can be increased by smoothing the histogram. It is proposed to use some digital filter, which will be smoothed traditional histograms, and due to this additional processing will improve the stability of the statistical calculations. The correct choice of the window digital anti-aliasing filter and multiple artificial increase in the number of discrete, used in digital filtering allows to significantly increase the power of goodness of fit test Gini and chi-square test. Graduated Gini goodness of fit test Gini is less sensitive to the number of examples in the test sample. Thus, its use leads to a decrease in error probability of the second kind, due to the limited number of experiments. The article presents a comparative table of the error probability of decision-making by the chi-square test and the Gini for the smoothed data. In contrast to the chi-square test, the Gini criterion is functional even on a sample of small kolichistvo experiments. Thus, for the problems we are seeing biometrics obvious benefit from the application of the criterion of Gini.
Siberian Aerospace Journal. 2014;15(3):146-150
pages 146-150 views

Calculation of the hodograph for Tiva region on the basis of velocity model of media

Tushko T.A.

Abstract

The development of seismic network in Krasnoyarsk region and Tiva republic arouse the interest to earth crust structure model for local earthquake data processing. The seismic waves travel time hodograph as 1-dimensional model of media structure is widely used in seismological practice. In the present paper the results of calculation of the first arrival times of P-wave hodograph for Tiva region are presented. Calculations are based on the block-layered velocity model of media obtained earlier as a result of seismic research of Altay-Sayan folded area data. A brief description of earth crust and upper mantle velocity model for south part of Krasnoyarsk region and Tiva republic is given. The structure of Tiva block is supposed to be 3-layered with horizontal boundaries. Consolidated part of the earth crust is characterized by linear dependence of wave velocity on depth. Values of model parameters were obtained by averaging of DSS and CWME velocity curves. Analysis of the wave pattern in the framework of the media model is carried out. In the paper an algorithm to calculate of seismic rays from sources positioned in different depths within the earth crust is discussed. The algorithm is based on analytical solutions derived from the general formulation of the direct kinematic problem of seismology in the ray approximation. The refracted and head waves propagation in the environment model is considered. Resulted hodograph is compared to that applied recently to regional seismic data. Comparison of head wave hodograph allowed to reveal a systematic error due to a difference in the earth crust thickness. Comparison of refracted P-wave hodograph with experimental travel time catalogue from industrial explosion shows a good agreement. A way to insert station corrections into hodograph originated from low velocity sediments under the seismic stations is proposed. Obtained hodograph is offered to use in hypocenter location problems.
Siberian Aerospace Journal. 2014;15(3):151-156
pages 151-156 views

An improvement of the differential evolution method implementated on GPU

Farkov M.A., Legalov A.I.

Abstract

Differential evolution is a very effective numerical optimization method which applied to diverse the set of computationally intensive tasks. Due to the features of the algorithm, it is very suitable for graphics processing unit (GPU). Most of the algorithm stages can be executed independently that corresponds to the basic programming paradigm of GPU (single instruction multiple data). Besides, an algorithm has a regular memory structure for internal data. The use of GPU allows to improve the speed of the algorithm significantly. The analysis of existing implementations of differential evolution method on GPU is performed. Moreover, existing implementations of the differential evolution algorithm on GPU use several unoptimized techniques which restrict effective application of the algorithm to tasks which use multiple optimization procedures. A new computational model that improves current implementations is described. A presented model reduces kernel calls latency due to combining logically-connected kernel into a single global kernel. The algorithm allows to use computational grid which contains single computational block. This approach satisfies requirements of the differential evolution approach to size of population (from five to ten times greater than number of optimized variables) and allows to use GPU internal barrier synchronization techniques. Besides a proposed implementation has regular data allocation in the global memory of GPU that provides coalescence of requests to the slowest global memory thus all threads in warp can read and write information from global memory per single request. Moreover it allows to use Compute Unified Device Architecture (CUDA) streams in very effective manner. In fact, a proposed model can simultaneously execute as much optimization procedure as multiprocessors available on GPU and belimited only by computer capabilities restrictions.
Siberian Aerospace Journal. 2014;15(3):157-161
pages 157-161 views

A real-time algorithm for human’s hand gesture recognition on video-sequence for human-computer interaction interfaces

Chudnovsky M.M.

Abstract

The author presents the new real-time algorithm for hand gestures recognizing on a video sequence, based on the color clustering principles, interframe differences for video sequences and contour analysis principal. The first chapter of this paper contains the research of related work, which is based on Viola-Jones algorithm, the search for the skin color, wavelet transformation, localization of the centroid of the image, etc. The second chapter describes the new gesture recognition approach, and third includes experiment results. A proposed gesture recognition algorithm resolVes two tasks: gesture localization and gesture recognition. The gesture localization task is resolved by compilation results of the image segmentation by human skin color clustering principle and motion search on the video sequences. The feature extraction task is resolved by invariant gesture contour moments analysis. A presented approach does not use any tutorial images. Gesture domain is not close and can be set up during initialization process. Key performance indicators (KPI) of the proposed approach are number of processed video sequence items per time unit and gesture recognition stability mark. The analysis of the performance of the proposed algorithm shows that the performance is at a high level. An average frame rate, which can function designed system is about 50 fps, which even exceeds the ability of the human visual perception. Recognition stability depends on environment condition changes, but the number of recognition errors can be reduced to a minimum by video device calibrating. The quality of recognition is 96%, which is a good indicator for such purpose algorithms. The KPI analysis, based on experimental data, is shown the applicability of the proposed approach in real-time gesture recognition systems, based on different hardware platforms. This fact allows to use the algorithm primarily in the aerospace industry to build effective management systems based on gestural interfaces.
Siberian Aerospace Journal. 2014;15(3):162-167
pages 162-167 views

Two new eclipsing systems in Cepheus constellation

Shendel A.S., Veselkov S.A., Lapukhin Y.G.

Abstract

In this work we describe the method of variable stars search, which is based on the analysis of distribution of a standard deviation of magnitude of stars from magnitude (software VaST and C-Munipack). We present the equipment on which the observation for search was received as well. Our observations have been performed in Krasnoyarsk with a Hamilton telescope (D = 400 mm, F = 915 mm) equipped with an FLI ML9000 CCD chip (3056x3056 pixels, pixel size 12 μm). The size of the fields taken is 2.3 x 2.3. All our CCD-observations were obtained without a filter. All images were obtained with 30-second exposure times. MaxImDL software was used for photometry and for basic reductions for dark current, flat fields and bias. The magnitudes were referred to red magnitudes of comparison stars from the USNO-A2.0 catalog (Monet et al. 1998). In this article we present two new eclipsing binary stars. They were discovered, using own CCD-observation and software C-Munipack. Periods were derived using the WinEfk software provided by V. P. Goranskij. The coordinates in the Table are from the USN0-A2.0 catalog. Stars 2MASS 22065429+6059580 and USNO-A21425-12666148 have types of variability of EW and EA respectively. The photometry of star 2MASS 22065429+6059580 had been with star 2MASS 22065444+6100029 together because their location nearby. General properties of variability for new variable stars: maximum and minimum of magnitude, epochs of the main minima, periods of change of light, we constructed the curves of light to one period, we present chart of sky near new variable stars are presentd. We give a short analysis of the results as well.
Siberian Aerospace Journal. 2014;15(3):168-171
pages 168-171 views

About analytical resuming multiple power series by using one-dimensional matrix methods of summation

Yakovlev E.I.

Abstract

In the theory of analytic functions of K. Weierstrass the concept of the analytical element (power series in C converging in a circle) and its analytic continuation are the main. The method of power series expansion at another, series proposed by Weierstrass, fundamentally solves the problem of analytic continuation, proved ineffective in a particular application. In the works of Hadamard, Mittag-Leffler, Le Roy, Lindelof the so-called summation methods that give good results for the analytic continuation of power series in the case of the star domains of the complex plane have been proposed. In the works of Arakelian a description of the areas, in which the restoration of the analytic continuation of the analytical element with a fixed center is possible by using the universal matrix methods of summation is received. This work is about the analytical continuation of multiple power series in the class offields of synthesis of spiral. Using one-dimensional matrix methods of summation of power series constructed multidimensional matrix methods of summation for multiple power series, which allows you to construct an analytic continuation of this number in the maximum spiral region called (m,α)-the star of the Mittag-Leffler function f defined by this row. This approbation built multidimensional matrix methods of summation of multiple power series is carried out using one-dimensional geometric progression. That is the domains of the complex plane, there is at least one infinite matrix "summarizing" all analytic elements with a given center. These domains were spiral relative to some point and were named Arakelian domains efficient summability.
Siberian Aerospace Journal. 2014;15(3):172-177
pages 172-177 views

Some units spacecraft balancing

Krushenko G.G., Golovanova V.V.

Abstract

Spacecrafts, which include, as a means of launching into orbit and functioning in space - engines, and artificial satellites for various purposes, are components, subassemblies, and assemblies operating in the mode of rotation, and, therefore, affected by the centrifugal forces. And, in the case of unbalance of the material from which they are made, or components relative to the axis of rotation, during operation of the corresponding objects they may be damaged as a result of imbalances that may disturb the working mode or even lead to failure of the spacecraft. In the present work as examples of negative consequences prevent of the imbalance of interest spacecraft, the technology considered balancing and rotating parts turbo-pump assembly of liquid-propellant rocket engine, and b) the electric pump unit of the spacecraft, designed to ensure the maintenance of the temperature modes of the spacecraft. Such objects of study chosen, and due to the fact that the turbo-pump rotor assembly located on it impellers operate a maximum of tens of seconds/minutes either continuously or cyclically at high speed - up to 100000 rpm, they must ensure that the temperature regime of artificial satellites for a much longer time - up to 15 years.
Siberian Aerospace Journal. 2014;15(3):178-184
pages 178-184 views

Perfection of control systems of space vehicles

Krushenko G.G., Golovanova V.V.

Abstract

The main indicators of the quality of space vehicles (SV) are their reliability and lifetime (LT) in the orbit, and a significant role in this plays a temperature mode inside of SV, where are the devices. And one of their stable work is to create a specific thermal regime in the volume of construction, what is the thermal control system in which the heat mode is provided with fan provided by thermal relay at a given temperature. The main indicators of the quality of SV is their reliability and LT in orbit, and a significant role in this plays a temperature mode inside of SV, where are the devices. While circulating in the system of temperature control of heat-transfer fluid, for example, nitrogen, transmits heat from the cold surface of the satellite that radiate excess heat into space. At downturn of temperature of a working body under the specified fan is switched off, resulting who in the absence of convection - to a significant increase in thermal resistance between the radiation surface and internal displacement of the surface of the body, and, ultimately, prevented further decrease of the temperature. As a result of improving the control systems, along with the improvement of other life support systems in the LT satellites to date, is more than 10 years, and by 2016 planned LT up to 15 years.
Siberian Aerospace Journal. 2014;15(3):185-189
pages 185-189 views

Dielectric properties of Bi 1-xLa xFeO 3 thin films

Aplesnin S.S., Ostapenko A.A., Kretinin V.V., Panasevich A.M., Galyas A.I., Yanushkevic K.I.

Abstract

Multiferroics on the basis of BiFeO 3 with spatially-modulated anti-ferromagnetic structure were investigated. The compounds BiFeO 3 widely and intensively are investigated as model objects for research of the mechanism of interaction between electric and magnetic subsystems, and for their possible use in spin electronics. Possibility of electric management of magnetization of a material at a room temperature is of interest from the point of view of its use in elements of computer memory with electric record and magnetic reading. The purpose of the investigation is to define the change in magnetoelectric interaction as a result of a variation of an antisymmetric exchange and to investigate the mechanism of low-temperature and high-temperature anomalies of dielectric permeability at bismuth replacement by lanthanum. It’s important to establish magnetoelectric properties of disorder system with random distribution of a constant of magnetoelectric interaction. On films of La xBi 1-xFeO 3 measurements of dielectric permeability, a tangent of angle of losses in the range of temperatures 100 K < T < 1000 K without magnetic field and in a magnetic field of B=0.8 T are carried out. The temperature dependences of a real part of dielectric permeability and a tangent of losses angles at a frequency of 10 5 Hz are defined. At approach to ferroelectric transition dielectric permeability and dielectric losses are sharply increased. At a temperature 835 K the changes in crystal structure attributed to transition from rhombohederal to the orthorhombic phase was found. In the vicinity of magnetic phase transition the anomalies in temperature behavior of dielectric permeability are absent. Bismuth replacement by lanthanum leads to small increase in magnetocapacity, in comparison with pure BiFeO 3. Magnetocapacity increases in external electric field, passes through a maximum and falls with growth of temperature.
Siberian Aerospace Journal. 2014;15(3):192-197
pages 192-197 views

Effect of lubricating composition with ultra-dispersive additives on fretting fatigue process

Dokshanin S.G.

Abstract

In this paper the possibility of improving the fretting wear resistance and anti-wear properties of fat in connection with the introduction of solid additives is considered. The topic work is to evaluate the effectiveness of lubricants with ultra-dispersive additives to reduce fretting-fatigue processes. The mechanism of fretting-fatigue consists of processes such as fretting corrosion and mechanical fatigue. Their interaction leads to the damage of the contact surfaces and leads to a drastic reduction in the fatigue endurance limit of parts. Fretting fatigue damage can occur in the bolt, pin, key and spline connections, surfaces of the parts, which were planted with interference, on surfaces of the shafts, clutches and other parts of friction unit. The results of investigation of grease on fretting-wear resistance, the distribution of the amount of wear from time are presented. The analysis of the state of the friction tracks and changeover of surface roughness after applying lubricant with solid additive is given. The experimental results suggest that the introduction of ultradisperse powder mixture of diamond and graphite in grease reduces the formation of fatigue cracks and improves the quality of the surface parts of friction units. This increases the actual contact area and reduces contact pressure. The values of tangential and normal stresses up to 18-20 % and the action of maximum shearing stress will move deeper into the material under the area of contact are also reduced. The application of lubricants with similar additives can increase the service life period of the mechanism twice as much. Test results can be used to select the lubricant used for the friction units operating in the mode of oscillation.
Siberian Aerospace Journal. 2014;15(3):198-201
pages 198-201 views

Improving the technology of preparation of the Al-Mg system alloy used in aircraft constructions

Krushenko G.G.

Abstract

In present article the improved and developed new technologies, methods and means used by manufacturing the moulded pieces and aircraft constructions made of АМг10ч alloy are described. In connection with containing magnesium in АМг10ч alloy, a whole series of problems are arised by preparation and founding the alloy because of inclination this element to oxidation and inclination the alloy to gasing that leads to worsening the quality of cast wares. The following actions were developed and put into practice to avoid the alloy from interaction with atmosphere and moisture of sand: 1) inserting the boric acid into the sand; 2) degassing of aluminum-zirconium and aluminum-titanium ligatures; 3) the optimal order of melting the burden materials was elaborated; 4) the high-temperature treatment of liquid alloy is used and 5) filtration of alloy by the pouring-in casting-form with using the 6) device of thermal pipe type, provided fast temperature reducing of superheated alloy. All these measures, taken separately as well as in complex provide obtaining the moulded pieces of АМг10ч alloy with necessary and improved mechanical properties. At that the reproducibility of the mechanical properties of moulded pieces of different fusions tests results is marked.
Siberian Aerospace Journal. 2014;15(3):202-209
pages 202-209 views

Thickness measuring of modeled oil-saturated rock with nanosecond bohole electromagnetic loging tool

Muzalevskiy K.V., Mironov V.L.

Abstract

The paper presents the experimental results of sounding a wet sand-air interface using a laboratory model of a borehole GPR. For this purpose a box filled moist sand moisturized with brine was built. The box was located in a laboratory room on a concrete screed. Radar antennas were housed in a waterproof plastic pipe on the bottom of the box. Radar antennas were made in the form of dipoles with extended bandwidth. The transmitting antenna was connected to the generator, the receiving antenna to the stroboscopic oscilloscope. With variation of thickness of a sand layer over the antennas and the distance between the transmitting and receiving antennas the signals of receiving pulses were recorded. An attenuation coefficient of amplitude and propagation velocity of broadband pulse were measured. It is shown that the theoretical model borehole GPR, created by authors using the method of discrete sources, well predicts a temporary shape and time delay of the pulse reflected from the boundary layer. A method for determining the thickness of the layer of wet sand from the measured time delay of the pulse reflected from the boundary layer at different distances between the transmitting and receiving antennas radar was proposed. This method allows to determine the distance to the interface with a relative error of 2.2 % without the involvement of a priori information on the electro physical properties of the medium in the layer. The results of this study allow you to plan and start bench testing of prototypes borehole probes.
Siberian Aerospace Journal. 2014;15(3):210-216
pages 210-216 views

Potential of detection range of borders of oil reservoir using logging tool with broadband electromagnetic pulse

Muzalevskiy K.V., Mironov V.L., Mikhailov M.I.

Abstract

On large-scale radar stand at the IF SB RAS, the experiments on sensing of oil-saturated sand using the laboratory pulsed electromagnetic logging tool, which was placed in a cylindrical shell of a commercially available borehole logging tool (VIKIZ), were conducted. For this purpose a big wood box (1.5м x 3.2м x 2.7м) filled moist sand moisturized with brine was built. The box was located in a laboratory room on a concrete screed. Borehole radar antennas are resistively loaded dipole antenna with extended bandwidth. The transmitting antenna was connected to the hi-voltage (~3kV) generator, the receiving antenna to the stroboscopic oscilloscope. With variation of the distance between the transmitting and receiving antennas the signals of receiving pulses were recorded. On the basis of measurements of the pulse shapes at the output of the receiving antenna, depending on the distance between the transmitting and receiving antennas were found propagation velocity and attenuation of sensing pulses. Experimentally was proved the possibility of recording probe pulses, that propagates in the oil-saturated sand at the distance up to 2.65 m. At given dynamic range of the logging tool transceiver (128.3 dB), the boundary of the oil-saturated sand can be detected at the distances up to 1.3 m. Furthermore it is shown that temporary forms of sensing pulses measured at the output of the receiving antenna of the logging tool are described theoretical model with high accuracy. The results of this study allow you to plan and start bench testing of prototypes borehole probes.
Siberian Aerospace Journal. 2014;15(3):217-223
pages 217-223 views

Weld formation control at electron beam welding with beam oscillations

Trushnikov D.N., Koleva E.G., Mladenov G.M., Shcherbakov A.V.

Abstract

Electron beam welding is used extensively to produce essential machine parts. The control of the basic beam parameters - beam power or beam current at constant accelerating voltage, welding speed, current of focusing lens and distance between electron gun and welded sample surface - is not enough to obtain at most of the regimes sound welds. Control of the focus position using analysis of the high frequency component of the current, collected by plasma, at periodic interactions on the beam (the oscillation of the beam or modulation of the focusing current) could be a way for the formation of non-defect welds at these conditions. The statistical analysis of weld geometry is shown.
Siberian Aerospace Journal. 2014;15(3):224-230
pages 224-230 views

Conceptual approach to the definition of the strategic alternatives of the enterprises development of the space-rocket industry

Erygina L.V., Makarenko N.O.

Abstract

As a result, numerous problems collecting over the years are capable to push aside home industry SRI on a roadside of economic development. The bills adopted in recent years provide formation of economically steady, competitive, diversified SRI, and as ensuring the guaranteed access and necessary presence of Russia at a space. However, there are presented only the purposes, tasks and stages of their performance, but thus aren't specified mechanisms, ways, tools which will provide effective planning, distribution and control over use of allocated resources. Large-scale financing noticeable now doesn’t guarantee the achievement of results that is clearly demonstrated by decrease in indicators of activity of SRI. It tells about need of completion and expansion of existing tools of management with space-rocket branch. Formation of the directions and the mechanism of market transformation of the enterprises SRI to be at the crossroads between methods of the planned economy untrue market realities and modern approach of strategic and innovative management, which doesn’t methodical based in Russia. Thus, it is necessary improvement the methods of strategic planning, in particular, development the choice tools of the development strategy for the enterprises of SRI. In the article the types of the enterprises of space-rocket branch depending on the purposes of innovative activity and their opportunities are presented. Division the enterprises on the allocated groups important for definition the choice directions of the development strategy. In addition, in the article a need complex research of the external and internal factors having impact on development of allocated groups of space-rocket enterprises, which in turn have to be subject to the account when developing tools the choice of the development strategy and find the reflection in structure of their innovative potential is pointed out. Moreover, the conceptual approach to a choice of the development strategy, based on definition of strategic alternatives of development with allocation the structure of innovative potential and its assessment, and as taking into account possibility of diffusion, realization and commercialization the innovations created in the main production of the enterprises SRI is presented.
Siberian Aerospace Journal. 2014;15(3):232-238
pages 232-238 views

Formation of innovative readiness of a personnel management system for the benefit of implementation of projects related to aerospace enerprise

Kukushkin S.G., Podverbnikh U.S., Samokhvalova S.M.

Abstract

The state priorities of the Russian Federation in the field of space activity set long-range goals to find new approaches in management for the space industry. The uniqueness and complexity of space production, exact resource limits of its life cycle stages define necessity of project approach to the whole enterprise management system, including personnel management subsystem. The article provides a description of some of the conceptual and methodological aspects of personnel management subsystem innovation preparedness to implementation of rocket-space enterprise projects. An integrated typology of rocket-space enterprises projects is proposed as a base for selection and application of project management instruments and technologies. This typology also contains main projects of the development, production and operation of spacecraft and systems, auxiliary projects (logistics, it, HR, PR, marketing, communications and etc.). The personnel management system innovation preparedness of project-oriented enterprise - a state-of-the-art structural-organizational, functional, competence potential of personnel management system, that ensure development, testing and scaling innovation, target project performance of the enterprise. Decomposition of levels of the personnel management system innovation preparedness to implementation of rocket-space enterprise projects includes personnel Department’s availability for managing own personnel management projects implementation as well as personnel support for key industrial projects, consisting in the development and implementation of business process management commands projects. The implementation of innovative preparedness identification and assessment is proposed to accomplish according to the parameters: structural, functional and information system availability management. The article presents the characteristics of the personnel management system innovation preparedness in terms of project management by the example of public corporation “Information satellite systems" of a name of academician M.F. Reshetnev (Zheleznogorsk, Krasnoyarsk region) - the world leader in the field of creation of means of telecommunication and space communication. The model for assessment of the personnel management system innovation preparedness to implementation projects, stated in the article, is based on decomposition of levels of innovation preparedness and proposes a serial expert evaluation on individual criteria and further integral convolution. Conclusions of the evaluation results give an opportunity to determine “weak points”, endangering for achievement of project goals, and justify actions on their elimination. The usage of this methodological toolkit at rocket-space enterprise, on the assumption of its integration into a unified system of project management, allows to fulfill the requirements of customers by functional, quality, cost and time characteristics of modern satellite systems.
Siberian Aerospace Journal. 2014;15(3):239-244
pages 239-244 views

On the scientific basis level assessment effectiveness regional resources

Nosachevckaya E.A., Klimuk V.V.

Abstract

The authors provide an analysis of existing methods of evaluating the effectiveness of the use of resources of the subject of the Russian Federation - Kaliningrad region. On the basis of the diverse opinions of scientists the characterization of regional resources with the release of the corresponding groups in graphical form (material, labor, financial, environmental, intellectual resources) was carried out. Each group consists of 4-5 main categories, characterizing them and used as indicators of effective use. The authors proposed a method of estimating the integral efficiency of the region with the release of material, labor, financial, environmental, intellectual components. Calculation of individual (private) efficiency allows to identify the most and least vulnerable aspects of the functioning of the region, to determine the main directions of influence to improve the efficiency of the whole region (country). Complex (integrated) is used to determine the effectiveness of management (economical) use of resources of all kinds in the whole investigated region (country). A mathematical apparatus for calculating each of the private and integral levels of efficiency. Tools for assessing the effectiveness of private levels are based on the use of relative performance (index change). To calculate the integral level of resource efficiency in the region used the geometric mean value that most accurately reflects the total (complex) change of regional resources for the study period. The approbation of the proposed methodology on the example of Russian exclave region - Kaliningrad region. Based on the statistical data of 2009-2013, the calculation was made on private and integral performance levels with a graphic reflection of the results. As a result, in terms of material, labor, environmental efficiency region recorded performance level close to unity. Intellectual efficiency observed the highest level of differentiation of the calculated values. In general, the integral level of resource efficiency of Kaliningrad region ranged from 0.5 in the 2009-2010 crisis and to 1.2 in 2012.
Siberian Aerospace Journal. 2014;15(3):245-249
pages 245-249 views

Structural shifts in the competitive high-tech modern space rocket technology directions of economic system of Russia

Popova T.S.

Abstract

It is shown on the basis of integral and space monitoring factors that formed the industrial competitiveness policy of Russia, its innovation policy should focus on the desired fields strategic breakthrough in space and rocket, which is possible to achieve or exceed the global technological level. Russian economy is inferior to the level of innovation activity of the global community with a competitive industry. Its innovative activity is directly dependent on the size of the enterprise. Russian industrial enterprises the share of non-technological innovation is low, lagging behind the European countries. Economic data in enterprises space industry and other sectors in eight federal districts of Russia, in the Siberian Federal District, Krasnoyarsk Territory, the top 10 regions, including CFD-TSCHER, 45 leading enterprises, the author's conclusions confirmed that for the expected structural changes in modern high competitive areas, achieving a high level of competitiveness of the space industry in the basis of analytical estimates should be of critical technologies and system management tool that gets in the world called “Technology Platforms”. The author shows that there is a need to develop an integrated management approach and a corresponding innovative tools that allow a single system to consider the priorities of different levels and the scale and stage of the innovation cycle of both the state and business. According to analytical estimates by the author in the structure of the total profits of enterprises of extractive industries priority belongs to the production of energy minerals. Reveals the author's scientific and practical approach, methodology and applications of modern tools in relation to the competitiveness of Russian policy in the industry as a whole, and astronautics, rocketry particularly conducive to modernity demanded structural changes, allowing an economic point of view on the proposed criteria in the comparative analytical characteristics of these critical technologies with Russian technology platforms and technology initiatives of the international community with a high level of competitiveness of the rocket and space industry and economic system of the country as a whole. New versions of the management of the modern knowledge-based competitive technological areas, such as in aerospace industry, and structural changes in them will require the development of new methodologies and tools to solve actual fundamental economic problems.
Siberian Aerospace Journal. 2014;15(3):250-258
pages 250-258 views

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