Vol 16, No 3 (2015)

Articles

MODERNIZATION DIRECTIONS OF THE HARDWARE AND SOFTWARE OF «KRABIK-BM» RADIO NAVIGATION SYSTEM

Aleshechkin A.M., Feoktistov D.S.

Abstract

Despite the widespread and easy use of satellite navigation systems (SNS), ground-based radio navigation systems (RNS) remain one of the main means of navigating maintenance of a number of objects, such as ships. Using RNS helps to achieve high accuracy in objects positioning, and to eliminate a number of disadvantages of SNS. From the beginning of the 2000s in the Siberian Federal University in collaboration with the Research and Production Enterprise “Radiosvyaz” were resumed the works on the development and serial production of terrestrial RNS UHF-range “Krabik-BM”, using the phase measurement techniques and navigation options designed for geodetic gridding sea ​​surface objects. This system consists of several aligned transceivers that can be used as a ship station, and the supporting shore stations by selecting an appropriate operating mode. In 2003 the serial production of the RNS and its delivery to the customer were started. Nowadays, system solutions and electronic components, used in the design of this, are obsolete. Therefore, there was a task of modernization of transceivers of the RNS mentioned, using modern components, design tools and software. In the present article the direction to update the hardware of the RNS using modern systems on chip (SoC), manufactured by Xilinx, is considered. Most preferably, according to the authors, is to use the SoC family Zynq-7000, combining into a single chip of programmable logic Artix / Kintex-7 and a high-performance ARM processor Cortex-A9. Using the proposed SoC allows us to solve the task of transceivers RNS “Krabik-BM” upgrade. In particular, it is expected to reduce the cost, weight and dimensions of the transceiver while increasing reliability by eliminating external interactions between the programmable logic and processor system. The article presents the block diagram of the transceiver RNS “Krabik-BM” before and after the upgrade. Another direction of the development of RNS is the development of radionavigation software of the secondary information processing in terms of opportunities and tools provided by modern operating systems and software development environment. For the design of this kind of software cross-platform integrated development environments with open source and high-level languages should be used. The most suitable one is the use of Qt Creator environment, providing the creation of applications with an extensive class library and ready development tools. The article presents the main elements of the radio navigation results measurements of the secondary processing program user interface, as well as its potential in output and processing terms. In conclusion, according to the article the use of selected directions of the RNS modernization in terms of hardware and software will enhance the competitiveness of the “Krabik-BM” and open up opportunities for further improvements due to the significant rise of hardware and computing resources of the system.
Siberian Aerospace Journal. 2015;16(3):546-553
pages 546-553 views

DETERMINATION OF MECHANICAL PROPERTIES OF MATERIALS OF HIGH PRESSURE METAL-XENON TANK

Aniskovich E.V., Seredin V.I.

Abstract

Presented are the results of determining the strength characteristics of mechanical properties of the metal-xenon high-pressure tank materials by means of experimental studies on the static tensile specimens cut from the titanium liner and experimental studies on a cross-four-point bending specimens of composite material cut from the power of the composite shell of the tank. Based on the concluded experimental studies, design study to assess the additional characteristics of mechanical properties of materials has been made. To study the thin-walled welded titanium alloy composite material and the container shell power plane and tensile samples were cut parallel and transverse rolled metal tank. During tensile tests automatic recording of strain diagram with the coordinates of load-displacement was conducted. For the experimental studies of composite strength composite shell tank samples were cut from the two zones of the tank near the top of the flange and the region near the equator of the middle part of the tank. Samples from the top of the angle were characterized by winding tapes -30°...+30°, samples from the equator - -12°…+12°. During the tests on the transverse four-point bending load speed measurement sample with the corresponding value of displacement was applied. According to the results of tests of samples prepared from a titanium alloy obtained were the yield strength, tensile strength, and percentage reduction of the material after rupture. Based on these data, the calculated values were obtained by breaking strain hardening coefficient and a titanium metal alloy. According to the results of tests of samples cut from the composite shell of the tank load-displacement diagrams for two types of samples were obtained. According to these data, the values were calculated by the modulus of elasticity for samples of composite material of two types. The obtained values of mechanical properties of the titanium alloy and composite based on the results of experimental studies were compared with the data of the relevant regulations. Based on this, refined are the grades of titanium alloy and a composite material, used in the manufacture of the metal-made high-pressure xenon tank.
Siberian Aerospace Journal. 2015;16(3):554-559
pages 554-559 views

ABOUT CONTROL OF INERTIA LESS DISCRETE-CONTINUOUS PROCESSES WITH RETARDATION

Bannikova A.V., Korneeva A.A.

Abstract

Presented is the problem of stochastic control objects with discrete-continuous nature of the process in non-parametric uncertainties, in particular, the problem of the process management without memory delay has been studied. Similar processes occur in many different control loops of aerospace objects and systems. For example, in the manufacture of electro-radio products, in the spacecraft about reaching 150 thousand, can be represented both as a series of local objects dynamic nature and freewheeling delay. This article describes a situation where the input object receives several controlled input variables. It leaves its mark in the management of such processes, and determines the relevance of the problem. The article provides theoretical information on nonparametric control algorithms under incomplete information about the controlled process. The focus is on the construction of nonparametric algorithms of dual control. The essential difference between dual control algorithms from the standard is that the control unit performs two functions: research and management in the process of active accumulation of information. Algorithm for computing the sequence of control input actions (chain) is based on following Manufacture scheme: first control actions are chosen at random, based on practical considerations, but the following one is calculated using the nonparametric algorithms of dual control taking into account the first. Further, this pattern is repeated, i. e. each subsequent value of the components of the control actions is calculated taking into account all the previous ones. Thus, the form of the equation describing the local process remains unknown due to the lack of a priori information. Detailed results of the numerical investigation of the use of nonparametric algorithms for adaptive dual control at several control actions are given. In the simulation, the characteristics of the objects were described by non-linear components, the form of which was unknown, and which, in the active acquisition of information automatically restored on the basis of measurement of the input-output variables of the process. The study was conducted at different reference variables that could have stepped character, or comply with one or another path. Also the effect of different noise acting on the object and the measurement channels were investigated. The results of numerical studies have shown high enough efficiency of nonparametric algorithms of dual control multidimensional process without memory under conditions of incomplete information.
Siberian Aerospace Journal. 2015;16(3):560-565
pages 560-565 views

SOME GENERALIZATIONS OF METHOD OF MOMENTS IN PROBABILITY DENSITY ESTIMATION BY ORTHOGONAL SERIES

Branishti V.V.

Abstract

A problem of probability density function estimation for continuous random variable is considered in the paper. Actuality of this problem for science and technology including aerospace branch is discussed. Building of the probability density functions estimation by orthonormal series is considered. Applying of the method of moments to statistical estimating series coefficients is investigated, and some generalizations are suggested. Within the scope of method of moments the author uses consecutive ordinary moments of random variable. In this case the calculation of series coefficients estimations is reduced to solving system of linear equations. The paper has the proof of the theorem that in specified conditions of orthonormal system choice, suggested generalization of the method of moments includes the ordinary method of moments and also more widespread estimating coefficients method by sample means of orthonormal functions as particular cases. The paper shows that in the case of using Legendre’s orthonormal system the considered methods are identical. The properties of built estimations are researched, mathematical expectations and covariance matrix are founded. The paper shows that in particular cases the estimations of series coefficients are biased. The estimations of series coefficients, which are calculated by suggested method, were used for building estimation of probability density function. The paper has results of numerical calculations of quality functional values for built estimations of probability density function. The calculations are carried out for uniformly distributed random value. The author compares the suggested method with the widespread estimating method with using Chebyshev’s and trigonometric orthonormal systems. Research shows that generalized method of moments gives substantially better result on small samples.
Siberian Aerospace Journal. 2015;16(3):566-571
pages 566-571 views

RESEARCH OF THE CASE ANALYSIS ALGORITHM IN THE CLASSIFICATION OF PROBLEM OF INFORMATION SECURITY INCIDENTS

Zhukov V.G., Shalyapin A.A., Sokolov M.M.

Abstract

The article is devoted to solution of the actual practical task of determining the strategy for responding to information security incidents in information systems with the help of case analysis. The author examines the process approach to incident management and its main stages. Incident management process, according to regulatory requirements, involves four steps: detection of an incident, incident response, investigation, corrective actions. At the second stage there is an urgent problem of a prompt response to information security incidents. It is necessary to decide which strategy should be chosen from a variety of specific strategies or to determine that there is no appropriate strategy and therefore it should be formed. As a solution of the problem of the response strategy selection it is proposed to use the case based analysis apparatus. To solve this problem it is supposed to use a simplified cycle of reasoning based on cases and not including the stage of response scenarios adaptation. The classification is based on the number of found analogies and the value of the similarity degree. Incidents are compared with case classes on the basis of similarities found in each class. According to the degree of similarity an incident corresponds to a specific case in the class and the response strategy associated with it. A new algorithm for classification of information security incidents in information systems based on the case and statistical analysis was worked out in accordance with the proposed concept of incidents analysis. The developed algorithm differs from the well-known ones in automatic selection of the optimal threshold value using ROC-analysis. The algorithm allows the selection of the criterion of classifier maximum quality depending on the permissible value of errors of the first and second kind under the given circumstances. The assessment of the developed algorithm effectiveness was carried out. The proposed concept of building the case based system of information security incidents increases responsiveness and allows repetitive using of the previous experience in the process of information security incidents management.
Siberian Aerospace Journal. 2015;16(3):572-579
pages 572-579 views

SIMULATION OF NON-STEADY CONTACT IN ROLLING BEARINGS

Ivanov V.A., Erkaev N.V.

Abstract

This article deals with the problem of non-steady hydrodynamic contact of a roller with finite size elastic plate. The lubricant viscosity coefficient is assumed to be exponential function of the pressure. For this problem, an iterative numerical method was elaborated to solve the 2-D Reynolds’ equation consistently with the integral equation of relationship between the surface deflection and pressure distribution in the lubrication layer. A normal motion of the roller causes additional pressure enhancement in the lubrication layer, which is proportional to the normal velocity. Coefficient of proportionality is called as damping coefficient. Carrying capacity and damping coefficient are determined from numerical solution as functions of minimal distance between the roller and plate. The obtained functions were used for modeling of the roller oscillations due to sudden variations of the external loading. Characteristic relaxation time and temporal variations of the pressure maximum are determined. Dependence of the pressure maximum on a special piezo-coefficient was investigated, which is a parameter of the exponential function approximating relationship between viscosity and pressure. Higher values of the piezo-coefficient yield larger values of the pressure maximum in the lubrication layer during the relaxation period. However, deflection of the body surfaces makes an opposite effect on the pressure. Therefore behavior of the pressure maximum is determined by two opposite factors related to the viscosity piezo-effect and surface deformations. From numerical simulations, a critical value of the piezo-coefficient is found when the influence of the piezo-coefficient is compensated by that of deformation of the elastic plate.
Siberian Aerospace Journal. 2015;16(3):580-586
pages 580-586 views

INVESTIGATION OF GRADIENT FIELDS OF THE EARTH SURFACE BASED ON SATELLITE DATA

Kartushinsky A.V., Kukoba N.A.

Abstract

To determine the horizontal structure of the physical and biological heterogeneities calculated are time-space gradients based on long-term satellite data. AVHRR MCSST, CZCS, SeaWIFS, MIRAS AQUARIUS, MODIS, MSS and NOAA, TERRA, AQUA, SPOT, LANDSAT picture images were used as input satellite data. Satellite data was used to calculate mean gradient fields of temperature, salinity and chlorophyll concentration in the ocean for different periods of time. The software calculates and averages the horizontal gradients in the ocean for different grids. Calculations are also made to find zonal, meridian, and absolute gradients, pointing to main frontal zones. The gradient fields and their high values give us information about spatial distribution of main frontal zones in the ocean. For study of the gradient field surface in aquatic systems realized is the averaging algorithm for dynamic object. Gradient of land surface shows changes of relief as steady state object. Space-time variability of gradient fields in the ocean has been received. Here we used satellite data on sea surface temperature, sea surface salinity and chlorophyll concentration. The main stage of research is evaluation of statistical correlation between gradients of temperature and chlorophyll concentration, which suggests a combined effect of physical and biological processes. Horizontal temperature and turbidity fields were considered for small object as Lake Shira (Russia, Khakasia) based on satellite data. Gradient zones of land relief were tested on satellite images. In this case, software ENVI 4.7 and IDL were used to calculate absolute (modulo) gradients surface height. Though idealized, our results suggest the importance of surface gradient parameters for the measuring from space.
Siberian Aerospace Journal. 2015;16(3):587-596
pages 587-596 views

A NEW FAST FACE DETECTION TECHNIQUE

Mamdouh M. Gomaa -.

Abstract

The problem of human face detection in a natural or artificial environment has always been among the highest priorities for researchers working in the field of computer vision systems and artificial intelligence. An effective face detection system should provide high percentage of correct detections, and low false detection rate in short time. Viola-Jones method is one of the best algorithms in terms of speed/quality ratio. However, this method in many cases gives a large number of false detections. The color of human skin is one of the features that helps to make face detection. The presence of the color information improves the efficiency of face allocation; narrows the search area and reduces the number of false detections and processing time of the input images. This paper solved is the problem face area detection, based on two new methods. The first technique uses the image pixel skipping process instead of testing each pixel to label it as skin or non-skin by using RGB color space. Second technique uses YCbCr color space and block approach which divides the image into blocks, the size of each block is 3×3 pixels, then we check the central pixel. If the central pixel satisfies the skin criteria, the whole block will be considered as a skin. Finally, we applied Viola-Jones algorithm to detect faces. The experimental results presented in the paper shows that the proposed algorithms provide high speed detection at low false error rate.
Siberian Aerospace Journal. 2015;16(3):597-603
pages 597-603 views

ABOUT BOOSTED LEARNING OF NONPARAMETRIC ESTIMATORS

Mangalova E.S., Shesterneva O.V.

Abstract

Versatility of identification methods allows to apply them in different technical areas (including the aerospace industry), as well as in medicine, economics, etc. In recent years, ensemble learning is becoming one of the most common methods of identification. Ensemble methods train multiple learners and further combine their use. One of the main tasks of combining multiple models with the same type is to eliminate certain drawbacks of individual models. This paper deals with some peculiar properties of the Nadaraya-watson kernel estimator. These peculiar properties are related with existence of sparse areas in the space of input variables (some regions contain a small number of observations in the training set) and with the behavior of the Nadaraya-watson kernel estimator near the boundary of the input variables space. The ensemble learning approach proposed by the authors is based on boosted learning of nonparametric estimators. There is a formalized approach to ensemble building with configurable parameters and there are some guidelines for choosing these parameters. The numerical researches shows that proposed boosted ensemble is significantly more accurate than a single Nadaraya-watson kernel estimator both in case of sparse areas in the space of input variables, and in case of areas with a large number of observations in the training set. Also the numerical research demonstrates high accuracy of proposed boosted ensemble near the boundary of the input variables space and shows the possibility of using boosted ensemble in the extrapolation problem.
Siberian Aerospace Journal. 2015;16(3):604-610
pages 604-610 views

SHUNKOV GROUPS, SATURATED BY GROUPS L 2( pn), U 3(2 n)

Pronina E.A., Shlepkin A.A.

Abstract

Investigated are Shunkov groups, saturated by groups (projective special linear group of degree 2 over finite fields), (projective special unitary group of degree 3 over fields of odd characteristics). Arbitrary group is called a Shunkov group, if every cross section by a finite subgroup of any pair of conjugate elements of Prime order generates a finite subgroup. Under periodic part group G is the subgroup generated by all elements of finite order of G, provided that it is periodic. Presented is a series of lemmas, in which we prove that: - G contains infinitely many elements of finite order; - In G there are finite subgroups K 1 and K 2, that and , but for no group of such that ; - Sylow 2-subgroup S, group G, locally finite and for any ; - All involution of S lies in - For any with the property it follows that ; - If V is a Sylow 2-subgroup of G and , then ; - All Sylow 2-subgroups of G are conjugate; - If and , then ; - Subgroup has a periodic part , where H is a locally periodic cyclic group without involutions; - The subgroup B is embeddable in locally finite simple subgroup L group G that is isomorphic U 3 (Q), where Q is a locally finite field of characteristic 2; - If the a for arbitrary nonunit element of H0, then has a periodic part N and , where t is an involution. Based on the above lemmas, we prove the theorem: the Shunkov group saturated by multiple groups of the form , has a periodic part , is isomorphic to either , or , for suitable locally of finite fields P and Q.
Siberian Aerospace Journal. 2015;16(3):611-617
pages 611-617 views

SHUNKOV GROUPS

Senashov V.I.

Abstract

The paper is devoted to the study of a class of conjugately biprimitively finite groups named as groups of Shunkov. Finiteness condition in such groups is superimposed on the subgroup generated by two conjugate elements of the group and group sections on finite subgroups. The paper presents results concerning groups of Shunkov. The relations between the class of groups of Shunkov with classes of groups of Chernikov, groups of Aleshin, almost layer-finite groups and periodic groups are shown. We have proven two results establishing the properties of groups of Shunkov. V. P. Shunkov in his first theorem dedicated to the class of groups of Shunkov established their connection with Chernikov groups in the class of primary groups. Further the groups of Shunkov together with the minimal condition for Abelian subgroups, with a primary minimality condition and with different conditions for systems of subgroups are studied. V. P. Shunkov establishes the existence of infinite Abelian subgroups in an arbitrary infinite Shunkov group. A. I. Sozutov described the structure of complement of group of Shunkov which is a Frobenius group or constituting a Frobenius pair with a proper subgroup. The structure of periodic groups of Shunkov with Chernikov Sylow 2-subgroups was studied. Several authors have established relationships of Shunkov groups with similar classes of groups. The existence of Shunkov groups without periodic part was proved. A. V. Rozhkov using techniques for working with automorphisms of trees divided an infinite set of classes of subgroups, generalizing the concept of Shunkov group by transferring finiteness conditions from the subgroup generated by two elements conjugate to the subgroup generated by any of its n conjugate elements. The results on Shunkov groups with the condition of saturation have been intensively studied in recent years were not included in this work because they can be found in the review of A. A. Kuznetsov and K. A. Filippov in the Siberian Electronic Mathematical News. Our results will be used in the study of infinite groups with finiteness conditions.
Siberian Aerospace Journal. 2015;16(3):618-623
pages 618-623 views

THE MAGNETIC EFFECTS OF THE TUNGUSKA EVENTS IN 1908

Shaydurov V.V.

Abstract

In the paper a new explanation for the magnetic effect registered by magnetographs of the Irkutsk Observatory during the Tunguska catastrophe in 1908 is presented. The effect was due to a local perturbation of the geomagnetic field, which began two and a half minutes after the main explosion at the epicenter of the Tunguska event in the basin of the Podkamennaya Tunguska River in Krasnoyarsk Region. The disturbance lasted for 6 hours and had a non-monotonic behavior. By now, several hypotheses have been proposed to explain this effect. But the most part of them is not consistent with other data, and the others have been not yet confirmed by quantitative parameters or model computations. The present explanation is based on the established fact of the sputtering of microparticles and submicron inclusions of iron and its oxides in the atmosphere as a result of the ablation and the explosion of the main part of the Tunguska cosmic body and its other fragments. These microparticles and inclusions, when cooling below a certain temperature (called the Curie point) in the Earth's magnetic field due to the well-studied effect of termomagnetization, received a significant unit magnetic moment. After that they moved with regard to the interaction with the Earth’s magnetic field, mainly along the magnetic field lines. In consequence of the deposition, they formed zones of high magnetization and high magnetic susceptibility of soils in the Tunguska catastrophe area. These zones were carefully marked out by A. P. Boyarkina and S. D. Sidoras during the paleomagnetic studies of friable sediments in the Tunguska catastrophe area. Moreover, they differ significantly from the areas of increased deposition of other, non-magnetic materials. Furthermore, the geometrical analysis of deposition areas of magnetic materials admits estimating the trajectory slope of the main cosmic body. This estimation in combination with other data gives a quite large entrance angle of the Tunguska cosmic body to the surface of the Earth about 76º This angle magnitude is in agreement with the results of the modern mathematical modeling of the explosion height of the main part of the Tunguska cosmic body.
Siberian Aerospace Journal. 2015;16(3):624-630
pages 624-630 views

USE OF INFORMATION TECHNOLOGIES FOR IMPLEMENTATION OF INTEGRATED METHODS IN TEACHING AEROSPACE SPECIALISTS ENGLISH FOR SCIENTIFIC PURPOSES

Shumakova N.A.

Abstract

The article considers the content of the course of post graduate students’ training in a foreign language for scientific purposes in a technical university of aerospace profile. The experience of work in the context of SibSAU training of young scientists to effectively functioning in an international professional scientific community is analyzed. The experience of work in connection with the growing trend of writing scientific texts (articles, publications, monographs, etc.) in a foreign language (English) is presented. A complex structure of work with postgraduate students in teaching a foreign language for scientific purposes is developed and presented. Particular attention is paid to the integration of Internet resources in the process of preparing for the candidate's exam in a foreign language, and subsequent publications in international scientific systems such as Web of Science, Scopus. The article reflects the experience of testing and implementation of various Internet sources, presents the most effective ones. High cognitive professionally-oriented and didactic potential of the Internet technologies used is marked.Particular attention is paid to the scientific search systems, allowing a full-text search on articles of major foreign publishers’ magazines, articles in the archives of articles and preprints, scientific resources of Internet. Links for work with authentic scientific periodicals, modern dictionaries and encyclopedias are proposed. The article maybe of interest to postgraduate students of technical universities of aerospace profile, preparing for the successful functioning in the scientific community in order to accommodate their publications in leading peer-reviewed journals, as well as for foreign language teachers using in integrated methods in teaching a foreign language for scientific purposes.
Siberian Aerospace Journal. 2015;16(3):632-637
pages 632-637 views

AXIAL BALL STRAIN INFLUENCE ON MEASURABLE VALUE OF BALL INDENTATION BY TOP POINT OF BALL

Avtonomov N.N., Tololo A.V.

Abstract

The automated ball indentation method is of special interests for aerospace industry at present time since this method can be used in situ test without making standard specimen. During the ball indentation depth of proposed device testing, applying automated ball indentation for acquisition of force-displacement diagram showed that this device has a minimal dimension chain. This was made possible due to the device original construction allowing measuring of the ball indentation depth by top ball point displacement. Only one element of dimension chain having dimension modifications was an indentation ball. Also the ball indentation numerical solution was presented. The object of this research is the determination of axial strain influence on measurable value of ball indentation by top point of ball and real ball indentation definition applicable in automated ball indentation tests. For the ball and specimen contact analysis ANSYS Multiphysics 15.0 software that realized finite elements method for theory of elasticity problem solution considering two solid contact was used. In the process of investigation it was revealed that relative ball axial strain value remains constant in loading elastic region and depends on ball and specimen modulus of elasticity relation. It is allowed to find relative axial ball strain and real ball indentation depth formulas by knowing ball and specimen modulus of elasticity. Thus, using the proposed device and finding the top ball point allows to determine the real ball indentation depth, considering the axial ball strain contribution that was used in situ test taking into account the force-displacement diagram and possibility to find yield point.
Siberian Aerospace Journal. 2015;16(3):638-644
pages 638-644 views

ABOUT THE CHOICE OF STRATEGY OF TECHNICAL SYSTEMS OPERATION

Vainshtein I.I., Mihalchenko G.E., Vainshtein J.V., Safonov K.V.

Abstract

The intensity function of exportation expenses for the strategy of strongly periodical systems recovery technology according to the time of carrying out preventive recoveries is investigated. The frequency functions of substitution elements service time under the emergency and preventive recoveries may be not equal. In the strategy of strong periodical recovery in the case of systems crash, the emergency recoveries are carried out, and if the system had worked without a crash for a definite period of time, then preventive recoveries are performed. The case of frequency functions correspondence under the emergency or preventive recoveries is well studied in the mathematical theory of reliability. For the exponential distribution (where the distribution parameters are different) the correlation was established between the parameters of the distribution and the costs of emergency and preventive recoveries, when the cost intensity function has one minimum point. In this case a characteristic graph of the costs intensity is set. The minimum value of the cost intensity is less than the cost intensity of the strategy of emergency recovery only (for the strategy of purely emergency recovery the preventative recovery is not carried out). In general, the condition is obtained for the function of time distribution of developments of replaceable elements under emergency and preventive recovery for the choice of the strategy implementation methods under study including equal and different functions of distribution by the criterion of the minimum intensity of the operating costs. In the case, where the developments distributive laws under failures in emergency and preventive recoveries are identical, but differ in parameters. The conditions are defined for the parameters where the given strategy should be considered with not equal distribution functions for the distribution laws frequently used in the reliability theory, in particular the exponential, Erlang distribution of the nth order, Weibull-Gnedenko, Rayleigh, Maxwell, and the log-normal distribution. The results of the choice of strategies of technical systems operation in order to minimize the operating costs intensity of the strategy under study are considered to be valid for maximizing the availability factor.
Siberian Aerospace Journal. 2015;16(3):645-650
pages 645-650 views

CALCULATION OF OPTICAL SYSTEMS FOR THE INFRARED SPECTRAL RANGE USED FOR THE DETECTION OF SMALL POCKETS OF FIRE FROM GEOSTATIONARY ORBIT

Veselkov S.A., Gorbatyuk E.O., Kuzakova N.M., Zavarzina A.V.

Abstract

The article discusses the possibility of detection of small fires from geostationary orbit, using optical systems operating in the IR-range. In the time of the scientific and technological revolution, forest protection has become one of the most pressing issues. Forest fires are a powerful natural and anthropogenic factor which significantly alters the function and condition of the forest. Forest fires cause damage to the environment, the economy, and often lives are under threat. According to statistics, 93 % of all forest fires are a 10-kilometer suburban area, which means that they are the fault of the local population. Strong fires from lightning are rare, approximately 2 % of cases as a thunderstorm is usually accompanied by rain. Therefore, it is extremely important to continuously follow precisely the southern districts of the region, home to the vast number of people. With the help of a special optimization program CODE V, the optical wide-angle telescope was numerically investigated. Using a high-aperture optical system f / 1,5, allowing the CCD-matrix size 8k x 8k, get a spatial resolution of 200 m per pixel from GSO. The optical system is a system of direct focus with three-lens corrector in a converging beam. All surfaces of the lens and the main mirror are aspherical surfaces. Given are the design parameters and the quality of graphics images. There is a possibility to conduct almost continuous monitoring of large areas of the earth surface for the search of small fires - up to 1-2 hectares if you put the calculated optical system in geostationary orbit.
Siberian Aerospace Journal. 2015;16(3):651-657
pages 651-657 views

REDUCTION OF SPACECRAFT HARNESS MASS

Dvirnyi V.V., Eremenko N.V., Dvirnyi G.V.

Abstract

Mass of cables implemented on-board a spacecraft is one of the drivers taken into account during spacecraft design phase. One of the requirements is to provide a high ratio between Payload and Spacecraft mass because the contribution of cable lines to spacecraft mass budget is significant, and cable lines have significant lengths, so mass of cable lines becomes a challenging issue. The article identifies and assesses major criteria considered during design of power lines belonging to telecommunication satellites harness. Major contributors to satellite mass budget has been identified, a description of major competitors among world level satellite platform manufactures is given, a comparison of masses of satellites manufactured on the basis of powerful Platforms, i. e. E3000 and Express-2000 is provided. The need to consider such generic criteria as mass and cost during selection of harness manufactures is described. Reduction of on-board harness mass is possible when new, state-of-the-art technology is used. The technology should have a flight proven heritage and shall be widely used by satellite manufacturers in Russia and worldwide. The advantage of implementation of power lines ensuring reliable power distribution which are vital elements of telecommunication satellite electric power subsystem has been reviewed. Implementation of state-of-the-art Axon’ Bus Bar technology, allowing to reduce satellite harness mass and to achieve reduction of satellite mass resulting in decrease of launch cost is being justified.
Siberian Aerospace Journal. 2015;16(3):658-663
pages 658-663 views

METHOD FOR THE SYNTHESIS OF AMPLITUDE-PHASE DISTRIBUTION OF HYBRID-MIRROR DOWNLOAD

Serenkov V.I., Kartsan I.N., Dmitriev D.D.

Abstract

The main disadvantage of satellite radio navigation systems is their low noise immunity. This is because the orbit of navigation satellites is 20 000 km above ground level, and the navigation signal from satellites, is extremely low. Applying the optimal methods of signal processing, however, manages to hold reasonably accurate navigational dimension. However, in the case of complex electromagnetic environment navigation signals are easily suppressed. Interference sources can be communication systems, radar, etc. Especially the problem of navigation signal suppression manifests around airports. In recent years, the problem of noise immunity of radio equipment has received much attention. Method synthesis of amplitude-phase distribution of hybrid-mirror antenna, providing formation of contour service area and failures of directional pattern towards at least three sources of an interfering signal is suggested. The method ensures the formation of failures in the chart orientation to minus 45-50 DB at signal level not more than 1 DB for corner signal timing and interference not less than 0.15 of the width of the NAM in the main petal days. Under the situation of interference in the direction of reducing side lobe, useful signal does not occur. In addition, the developed method provides an accelerated adaptation to jamming conditions of a choice of pre-calculated variants of amplitude distribution of antenna array of the most close to the optimal, mainly petal pattern. Adaptation time is reduced by 25 %, taking into account the performance of modern shifters, the speed of which is comparable with the time of work of Adaptive algorithms. To speed up calculation of amplitude-phase distribution of the target function was limited to a set of points specified programmatically that allows the 5 times reduction of time of synthesis in comparison with the classic gradient method.
Siberian Aerospace Journal. 2015;16(3):664-669
pages 664-669 views

ONGROUND TESTING OF SATELLITE ATTITUDE DETERMINATION AND CONTROL SYSTEM WITH THREE-AXIS MOTION SIMULATOR

Fedchenko D.А., Sinitskiy D.Е.

Abstract

In order to increase quality and reliability of newly developed satellite attitude determination and control systems (ADCS), on-ground testing is needed during their development as well as manufacturing. Moreover, the effectiveness of ADCS testing directly depends upon the accuracy of its operating environment simulation which requires highly accurate simulation of environmental effects on the sensitive items of the tested system. This article describes provision of accuracy when setting input effects on the ADCS sensitive items while performing dynamic bench tests using three-axis motion simulator which design is based on three-axis Cardan assembly. The article describes the calculation procedure and the algorithm of control input generation that affects the three-axis motion simulator while simulating absolute angular rate vector for the unit measurement channels, intended to measure satellite body angular rate. Motion simulator main advantages determined by its specific design are given. The article describes main kinematic relations and method of three-axis motion simulator calibration with reference to meridian that allows to take Earth angular rotation rate effect on the unit sensitive axes while the control input, affecting the simulator, is being generated, thus increasing the simulation accuracy. The research resolves an urgent issue which on the one hand allows to increase the quality of unit output performances measurement process, on the other hand it allows to increase effectiveness of ADCS on-ground testing. Effect of uncertainties of the three-axis motion simulator on ADCS dynamic performances measurement process in a damping mode was assessed using mathematical model method. The article also demonstrates that calculated kinematic relations and developed control algorithms simulate satellite angular motion accurately enough. Uncertainty of angular rotation rate in the set mode does not exceed 0.1 ′/sec.
Siberian Aerospace Journal. 2015;16(3):670-679
pages 670-679 views

USE OF DIFFERENT OXIDIZERS FOR AFTERBURNING OF HYDROGEN HEATED BY SOLAR ENERGY IN ROCKET ENGINE

Finogenov S.L., Kolomentsev A.I., Kudrin O.I.

Abstract

Solar thermal propulsion (STP) with heating of hydrogen in high-temperature “concentrator-absorber” system with the possibility of its subsequent afterburning with cold oxidizer is considered. Such components as fluorine and hydrogen peroxide are suggested as oxidizers. These oxidizers create high-energetic propellant compounds with hydrogen and have high stoichiometric ratios, that allow to reduce required overall dimensions of solar energy mirror concentrator, as one of the most critical elements of STP. Results of parameters optimization of concentrator-absorber system by criterion of maximum of payload weight in the task of payload injection into geostationary orbit for the cases of isothermal (uniform) single-stage absorber and non-isothermal absorber with heating stages (non-uniform heating) use with reference to use of metal or film concentrator are presented. It is shown that requirements to accuracy of concentrator and its tracking system to the Sun are rather high. Decrease of dimensions of solar concentrator at afterburning of heated hydrogen simplifies its creation and improves operation in space conditions, in particular improves inertial characteristics of the STP as a part of space vehicle and simplify orientation to the Sun. Comparative characteristics of the STP use as space vehicle subsystem for the cases of metal and film concentrators are presented at isothermal and not isothermal heating of hydrogen and its afterburning by the considered oxidizers. The required area of concentrator in the case of fluorine use can be significantly reduced (up to 25 % and more) in comparison with oxygen-hydrogen STP. Use of hydrogen peroxide in some tasks allows 10…12 % reduction of the concentrator area as compared to oxygen-hydrogen STP. It is shown that payload injected into geostationary earth orbit, in the case of fluorine-hydrogen STP with film concentrator and non-uniform heating, can be increased up to 70 % and higher in comparison with the use of oxygen-hydrogen liquid propellant rocket engine.
Siberian Aerospace Journal. 2015;16(3):680-689
pages 680-689 views

METHOD of waveguides with conductive vacuum coating fabrication

Khomenko I.I., Ravodinа D.V., Mikheev A.E., Eresko T.T., Eresko S.P.

Abstract

Presented is the way of fabrication of waveguides and waveguide elements using the electroformed method of applying conductive vacuum coating that meets the technical requirements imposed on the waveguide elements: the minimum ratio of a standing wave voltage (VSWR) - 1,03-1,05; minimal loss of energy during the passage of the wave is not more than 5 ∙ 10 -2dB; electrokinetically flange products - up to 40-50 dB. Also the demands on the roughness of the inner surface of the channel (Ra is not more than 0.2 μm) and the deviation from the nominal size in the range of ±0,01 mm. The paper uses the method of manufacturing of a waveguide millimeter range, including the manufacture of the mandrel of aluminum alloy, the outer surface of which follows the shape of the internal channel of the waveguide, causing the mandrel which is a metal layer for forming conductive coating of the inner channel and the body of the waveguide, and further etching the mandrel. Investigated are the microstructure of the waveguide housing tract, the adhesion of the silver coating to the body of the waveguide and the measured roughness of the waveguide path are. Studies of the inner surface of the waveguide path in the presence of various impurities are made. The technology of vacuum deposition of the coating on the mandrel and capacity copper waveguide housing tract with subsequent etching of the mandrel has been developed. In this way it is possible to make the waveguides and waveguide elements tracts complex cross-sections. The conductive coatings, deposited by vacuum method, becomes dense and homogeneous, no absorption, and prevents chemical contamination of the coatings, resulting in reduced energy loss when passing waves and improves the quality of the transmitted signal. This method was made a waveguide of circular cross section with a diameter of 10 mm and length of 120 mm which has high adhesion with a conductive coating to the body of the waveguide.
Siberian Aerospace Journal. 2015;16(3):690-695
pages 690-695 views

MAGNETOCAPACITIVE EFFECTS IN SOLID SOLUTIONS Yb xMn 1-xS

Aplesnin S.S., Kharkov A.M.

Abstract

The paper describes the materials on the basis of solid solutions Yb xMn 1-xS, which could be potentially used as sensors, sensor devices, read-write information. Mechanisms of magneto-electric effects were considered and the mechanism of magnetoelectric coupling at room temperatures in the absence of spin order was clarified. The optimal conditions for the occurrence of magnetoelectric effect on temperature and concentration are found. The results of measurements of dielectric permeability and dielectric loss tangent for several frequencies in the temperature range 80 K < T < 400 K for composition Yb xMn 1-xS, x = 0.05 and x = 0.1, without a field and in magnetic field 0.8 T were presented. The magnetic permeability of solid solutions Yb xMn 1-xS from the measurements of inductance of the solenoid with sample was determined. The magnetic permeability by cooling the sample in zero magnetic field and in the field of 0.25 T was measured. The shift of maximum in the temperature dependence of magnetic permeability in the vicinity of transition to the magnetically ordered state to high temperature versus frequency was found. Quality factor decreasing when heated and a maximum at a frequency of 10 kHz, and a minimum at a frequency of 50 kHz in the vicinity of Neel temperature was established. Relaxation time depends on the temperature according to the power law in the paramagnetic region. The observed anomalies are explained by the dynamic of the electron orbital magnetic moments. Magnetocapacitance effect in Yb xMn 1-xS with x = 0.05 and x = 0.1 at temperatures above room temperature was found. Changes in sign of magnetocapacitance in the vicinity of 200 K for x = 0.05 was determined. Magnetocapacitive effects are explained in the model of the orbital ordering of electrons. Change in sign of magnetocapacitance on temperature is attributed to the formation of magnetic and orbital ordering at different temperatures.
Siberian Aerospace Journal. 2015;16(3):696-704
pages 696-704 views

INFLUENCE OF DISTRIBUTION OF CONTACT PRESSURE ON LEAKAGE THROUGH CASKET

Аsheichik A.А., Polonsky V.L.

Abstract

The questions of influence of the shape of contact surfaces on leakages through rubber seals in fixed connection of subassemblies of space technics are considered in the article. It is known from practice of operation of seals of various designs of space-rocket hardware that the shape of contact surfaces and consequently also the shape of diagram of stresses in a contact zone, considerably influences the leaks value. The design of test equipment and technique of leaks study through fixed face seal is offered. Object of research is the fixed face ring seal. During the tests into a ring rubber seal the ring indentors of various shape were pressed. The depth of introduction was regulated and measured with split-hair accuracy. Thus various variants of distribution of contact stresses on width of a contact area were modelled. The air was delivered under different pressure through a gas reducer in an internal cavity of seal and measurement of leaks was made. Experimental dependences of leaks value vs external pressure at various values of introduction of the peak into rubber are received. The developed finite-element models of three seals used in experiment with various shapes of indentors and program STAR has allowed to theoretically study distribution of stresses on width of a contact area. The result of this experimentally-theoretical work was creation of the new finite-element program for calculation of leaks through fixed rubber seals LEAKAGES, considering the shape of rubber seals, viscoelastic properties of rubber, including the relaxation and creep phenomenon. As a result of experimental researches on introduction ring indentors of different profiles into a rubber fixed gasket it was found that at the expense of shape optimization of indentor the leaks value can be lowered 10 times. The finite-element program for calculation of leaks which allows optimizing the shape of created rubber seals for the aerospace equipments is developed.
Siberian Aerospace Journal. 2015;16(3):705-713
pages 705-713 views

A METHOD OF RESISTANCE WELDING ELECTRODES MANUFACTURING BY COMBINED CASTING AND STAMPING

Busygin S.L., Tokmin A.M., Bogdanov V.V., Gotovko; Gotovko S.A.

Abstract

The present article describes the main functions of the resistance welding electrodes, as well as areas in which they are applied (engineering, automotive, aerospace industry, construction). With regard to the aerospace industry, the electrodes are used to obtain the compounds of an aircraft structural elements (connection of sheathing with framing members and connecting elements of the frame by resistance welding). Assessed is the complexity of the processes used in the manufacturing of resistance welding electrodes with a given set of physical-mechanical properties, as well as the complexity of managing the macro - and microstructure, strength and operational characteristics, changes in the structural and energetic state of the alloy. The method of introduction of alloying elements prepared in the melt by using tablets Cu-Cr is described. The technology of smelting and further pressing of the electrodes is tested. A subsequent heat treatment after forming the electrodes of resistance welding to achieve the highest level of physical and mechanical properties (hardness and conductivity) is defined. Investigated is the microstructure of the sample electrode in the optical microscope Carl Zeiss Axio Vision, showing a fairly uniform distribution of secondary phases in the bulk electrode. Energy dispersive analysis of samples of electrodes on a scanning electron microscope JEOL JSM-7001Fwas conducted, showing the approximate contents of the main elements in the alloy, as well as the distribution of chemical elements in characteristic radiation on the surface of a cone that has a considerable influence on the hardness and conductivity of the electrodes of resistance welding. The tests of the samples of the electrodes in resistance welding machine, MPTU-300, assessed their quality. As a result of practical tests of the optimal modes of contact welding of bar reinforcement cross of steel 35GS diameters 10+40 mm are chosen. The influence of nanostructured particles of chromium on the hardness, electrical conductivity and resistance of the electrodes of resistance welding is estimated. The dependences of the degree of wear of the electrodes from the number of welded points for various materials used in the manufacture of resistance welding electrodes are formed. Conclusions according to the results of the work are done.
Siberian Aerospace Journal. 2015;16(3):714-719
pages 714-719 views

COMPARATIVE ANALYSIS OF UNIVERSAL JOINT STRUCTURES OF UNEQUAL ANGULAR VELOCITY

Eresko S.P., Eresko T.T., Kukushkin E.V., Menovschikov V.A.

Abstract

Presented is the overview of universal joint designs of unequal angular velocities, such as cutting the hinges with a hinge sleeve and a helical coil spring of wire of circular cross section, a cylindrical hinge with a helical spring made of wire, the cross section of which has the shape of a convex polygon, the hinge sleeves of material with high hardness, the hinge with a few bushes, hinge with folding case. The influence of the skew angle of the needle bearing rollers on the value of the contact stresses and the comparative analysis of universal joints structures on needle bearings for use in transport and technological systems has been studied. Patent search revealed a number of methods and devices aimed at solving the problem of failure of the bearing units on needle bearings. Considered are universal joints with a split bushing, universal joints twisted coil spring wire of circular cross section and twisted coil spring wire cross section which has the shape of a convex polygon, universal joints with sleeves of material with high hardness and a few bushes, universal joint cross folding case. The improved designs of universal joints of unequal angular velocities are suggested. Universal joint with replaceable spikes provides the possibility of replacing parts of the universal joint without disassembling the entire driveline and includes body crosses, in which there are spikes in the form of sleeves. Universal joint with a new seal allows to prevent foreign bodies in the work space of the universal joint and leakage of lubricant, improve the reliability of universal joints due to the sealing of the working chamber, sealing in the form of a corrugated tube frustoconical ending by the larger base coaxial washer L -shaped cross section, and from the smaller base ring in the shape of a torus, fixed in response toroidal groove formed in the body of the cross at the base of the spike.
Siberian Aerospace Journal. 2015;16(3):720-728
pages 720-728 views

ATOMIC AND ELECTRONIC STRUCTURE OF CNT/LSMO-BASED NANOCOMPOSITES: A DFT STUDY

Kovaleva E.A., Kuzubov A.A., Kuklin A.V., Mikhalev Y.G., Popov Z.I.

Abstract

Complex half-metallic manganites La 1-xSr xMnO 3 (LSMO) are promising materials for spintronic and spicaloritronic applications due to 100 % of spin polarization. Using spin-polarized currents through LSMO-graphene interfaces a number of LSMO-based high-efficiency organic LED and spin-valve nanodevices have been developed. Large magnetoresistance effects bonded with large output signals were detected in a nanodevice. The device of multiwall carbon nanotube that spans a gap between spin-polarized half-metallic La 0.7Sr 0.3MnO 3 electrodes demonstrated long spin lifetime and high Fermi velocity in the nanotube, the high spin polarization of the manganite electrodes and the resistance of the interfacial barrier for spin injection. The experimental results were supported by density functional theory calculations. Interfaces of La 0,67Sr 0,33MnO 3 with armchair and zigzag carbon nanotubes (CNT) were studied by means of quantum chemistry within density functional theory. All calculations were performed using generalized gradient approximation with Hubbard correction (GGA+U) and Grimme correction of dispersion interaction. Different configurations of composite compartments mutual arrangement were considered. The analysis of partial densities of states (PDOS) reveals the influence of substrate on nanotube’s electronic structure. The possibility of nanotubes’ spin polarization and utilization of such nanocomposites in spintronics is also discussed. It was found that interaction between carbon nanotubes and LSMO slab lead to major deformation of the tube due to the difference in structural parameters of composite compartments. Zigzag (9,0) nanotube is contracted by 9% while armchair (5,5) nanotube is stretched by 5 %. Although this deformation results in significant change in nanotube’s electronic structure, there is no visible difference between spin-up and spin-down PDOSes of the tubes. Composites are then almost totally spin-polarized due to the presence of LSMO.
Siberian Aerospace Journal. 2015;16(3):729-734
pages 729-734 views

MANUFACTURING TECHNOLOGY AND WELDING OF ALUMINUM ALLOYS ELECTRODES CONTAINING NANOPOWDERS

Krushenko G.G.

Abstract

In the manufacture of aircraft structures made of aluminum alloys used is the welding, physical essence of which is to obtain a permanent connection by melting and co-crystallization of the welding electrode materials and parts to be joined. However, while the structure of the weld and the joined parts of the influence of heat coarsen, which leads to a reduction in the mechanical properties of the welded articles. It is known that metal with fine-grained structure has higher mechanical properties compared to coarse. Thus in practice, for the purpose of foundry castings structure refinement modification is used, the essence of which consists in introducing alloys into the liquid metal using substances which serve as crystallization centers. However, the possibility of modifying such agents has reached the limits in recent years and a new method of modifying the application using nanopowders (NP) chemical compounds (nitrides, carbides, borides, oxides), which gives a high effect of enhancing the mechanical properties of the molded articles has been found. It should be beared in mind that the mechanism of crystallization of molded articles and weld identical technology modifying liquid alloy was used to grind the weld structure in the manufacture of a welded structure of the aircraft from the example sheets of aluminum-magnesium alloy AMg6 with welding rods containing NP. The test results are cut from the welded structure samples showed that s metal at the weld joint during the welding rod comprising NP BN, is 333 MPa, LaB6 - 338 MPa, TiCN - 345 MPa. These values were higher than 4.1, respectively; 5.6 and 7.8 %, than the samples have AMg6 alloy (320 MPa), welded by the standard electrode of the same alloy. The development is protected by patents of the Russian Federation.
Siberian Aerospace Journal. 2015;16(3):735-742
pages 735-742 views

Theoretical study of Si (100) doping influence on lithium sorption and diffusion

Kuzubov A.A., Mikhaleva N.S., Popov Z.I., Krasnov P.O., Nikoleva K.M.

Abstract

Currently, silicon is the most promising anode material for a new generation of lithium-ion batteries due to its very high theoretical specific capacity (4200 mAh/g). However, one of the problems hindering the wider use of this material is the slow diffusion of lithium from silicon surface into volume that can be solved by modifying silicon surface. The simulation of surface processes of sorption and diffusion of lithium in doped Si (100) was carried out by using the density functional method. In the study Si (100) doped with single atoms B, Ga, Ge, found that the silicon replacement compared to adsorption are more profitable for all dopants. The binding energy of dopant to silicon decreases from germanium to gallium. It was found that boron atom substitutes for the third layer of silicon, germanium and gallium occupy positions in the first layer. In comparison with the pure material the trend of initial lithium sorption in the channel between silicon dimmers retain for Si (100) doped with single atoms of B, Ga, Ge. Energy barriers of lithium transition on silicon surface substantially reduce (in the case of boron) and increase (in the case of gallium and germanium). The energy barrier of transition from surface to surface layers L-U during the doping increases by 0.05 eV, this shows a moderation of the stage. According to the study, Si (100) doping with boron, gallium and germanium (concentration of 0.3 atomic %) has not significant influence on sorption and diffusion parameters.
Siberian Aerospace Journal. 2015;16(3):743-749
pages 743-749 views

PROPERTIES OF QUASICRYSTALLINE Al-Cu-Fe COATINGS PREPARED BY PLASMA SPRAYING

Lepeshev A.A., Karpov I.V., Ushakov A.V., Zelenkov P.V., Fedorov L.Y.

Abstract

The physical, mechanical, and tribological properties of quasicrystalline coatings based on the Al 65Cu 23Fe 12 alloy prepared by plasma spraying have been investigated. The specific features of the phase formation due to the competitive interactions of the icosahedral ψ and cubic β phases have been elucidated. Сorrelation between the microhardness and the content of the icosahedral phase in the coating has been determined. The decisive role of the quasicrystalline phase in the formation of high tribological characteristics of the coatings has been revealed and tested.
Siberian Aerospace Journal. 2015;16(3):750-757
pages 750-757 views

Determination of particle mean free path Beta decay in the particulate material

Telegin S.V., Saunin V.N., Chesnokov E.Y.

Abstract

We developed a method for the experimental determination of the mean free path of the particles of β-decay in powder materials, to improve the accuracy of calculations when selecting materials for screens. Error in the calculation materials of complex chemical composition by empirical formulas reaches 30 %. For the study, we took a powder PT-NA-01. Selection is based on the fact that the powder is composed of two elements, the mean free path of the electrons can be calculated according to the formulas with high accuracy. Morphological study of the powder showed that the particles are in the shape of fragments and 87 % of their size in the range of 40 to 80 microns. The weight ratio of lacquer in a powder sample was determined experimentally. The best was the composition comprising 3 % lacquer in the dry residue. It has been found that the polymerization of lacquer loses 50 % of the mass. Investigation of factors of manufacturing process of samples showed that the optimal compression pressure of 6 t / cm 2, and the density of the samples do not exceed 65 %. The pressure is chosen depending on the strength properties of the briquettes. We used radiation isotope St-Y with intensity 2,7E + 05 pulses / sec. The proportion of radiation absorption in the binder was investigated on samples of lacquer. The measurements showed that its attenuation coefficient is 1,26 ± 3 % for the thickness of 0.08 cm with a density of 1,07-1,18 g / cm 3. In these studies, the contribution of the binder can be neglected because its content does not exceed 3 % by weight of filler. It was found that dependence of intensity on the thickness of the sample, the value of the extrapolated path of the electrons is equal to (0,21 ± 0,04) cm, it belongs to the region of the confidence interval, the values calculated by empirical formulas 0.14 cm divided by the fill factor was equal to 0.65, the calculation accuracy of 15 %. To increase the fill factor and reduce the thickness of the lacquer on the particles, we examined the effect of the viscosity of the lacquer on the density of the sample. The distance between the particles in the samples with lacquer, which dissolved 1:1 by weight with ethanol is much smaller. The fill factor of these samples reached 0.88, and extrapolated path - (0,16 ± 0,02) cm. The accuracy of calculation of the mean free path of the proposed method does not exceed 10 % in this material.
Siberian Aerospace Journal. 2015;16(3):758-762
pages 758-762 views

Vol. 16, No. 3, P. 763-769 INFLUENCE OF PLASMA SYNTHESIS OF ZrO 2 NANOPARTICLES ON MAGNETIC FLUX PINNING IN GRANULAR YBa 2Cu 3O 7-y

Ushakov A.V., Karpov I.V., Lepeshev A.A., Fedorov L.Y., Shaihadinov A.A.

Abstract

In this work, the effect of ZrO 2 nanoparticles prepared in a low-pressure arc discharge plasma on magnetic flux pinning of granular YBa 2Cu 3O 7-y/nanoZrO 2 composites has been studied. It has been shown that the ZrO 2 nanoparticles do not change the superconducting transition and the microstructure of superconductors. At a temperature of 5 K, the addition of 0.5 and 1 wt % of ZrO 2 nanoparticles may lead to the additional effect of magnetic flux pinning and the increase in the critical current density J c. The J c value for composites with 1 wt % is two times larger than that for the reference sample. The fishtail effect is observed for YBa 2Cu 3O 7-y/nanoZrO 2 composites at the temperatures of 20 and 50 K. The problems associated with the additional effect of magnetic flux pinning of granular YBa 2Cu 3O 7-y/nanoZrO 2 composites and the appearance of the fishtail effect have been discussed.
Siberian Aerospace Journal. 2015;16(3):763-769
pages 763-769 views

MICROMAGNETIC SIMULATIONS OF THE MAIN STATE OF FERROMAGNETIC NANODOTS WITH UNIAXIAL ANISOTROPY

Fel’k V.A., Eroshenko P.E.

Abstract

The work performed numerical simulations of the ground state of the ferromagnetic nanodots with uniaxial anisotropy. The calculation of the ground state was performed using a three-dimensional micromagnetic simulation package OOMMF for two types of sample geometry - cubic and ellipsoidal with a simple cubic lattice. Cases were analyzed as a ferromagnet of the “easy axis” and “easy plane”. In the simulation permalloy material parameters and materials such as SmCo were used. The latter allowed values of the uniaxial anisotropy which is several orders higher than technologically realizable values from permalloy. It is shown that for an ellipsoidal nanodots with permalloy material parameters, there is a transition region, the size of the sample in which the ground state is highly degenerated. It is found that above the upper boundary of the transition region there is a tendency to vortex stabilization of the ground state. For any sample size permalloy effects depending on the topology of the ground state of the system on the magnitude and sign of the constant uniaxial magnetic anisotropy have been identified. For a cubic specimen geometry permalloy existence of a stable vortex in the ground state is possible if the size of nanodots is several times higher than that of the ellipsoidal case. For samples with material parameters SmCo large uniaxial anisotropy has a stabilizing effect on the vortex structure in the ground state nanodots. Vortex state is feasible for much smaller nanodots, in comparison with the permalloy. Under specific size of nanodots SmCo ground state (in the case of easy-axis) acquires skyrmion-like character.
Siberian Aerospace Journal. 2015;16(3):770-775
pages 770-775 views

The electric field intensity INFLUENCE on water CLEANING from METAL IONS at the interphase boundary

Shestakov I.Y., Raeva O.V.

Abstract

In the manufacture an aircraft parts electroplating processes are used which result in the contamination of wastewater metal ions. Currently there is a large number of water and aqueous solutions purification methods - mechanical, chemical, electrical, physical, biological, combined method, etc. For example, for water purification from iron defending from copper, nickel, chromium (VI) is used effectively. Also electro-coagulation, ion exchange technology, biological treatment, etc are widely used. Waste water of electroplating industry contains a collection of different metal ions at concentrations of 0.5 mg/l or less. Research on integrated water purification from metal ions under these conditions is not enough. The article presents the results of experimental studies of water cleaning from metal ions using two different methods - electrochemical and electrochemical air bubbling. Electrochemical effect was to purify water passing through the asymmetric alternating current using insoluble heterogeneous electrodes (stainless steel 12X18H10T, titanium alloy ОТ 4-0). The treated water bubbling used air which has passed through purified water. The highest efficiency of water cleaning is achieved by electrochemical method with air bubbling due to the uneven distribution of the electric field intensity at the interphase boundary. This method increases water cleaning efficiency: from cadmium ions in 2.9 times, copper - 1.1, nickel - 5, chromium - 1.2, and iron - 1.1. Specific power consumption makes up 1.8 (kW∙h)/m 3 while electrochemical cleaning method with the insoluble electrodes and alternating current the specific power consumption is 3.5-4 (kW∙h)/m 3.
Siberian Aerospace Journal. 2015;16(3):776-781
pages 776-781 views

DETERMINATION OF MARKET POTENTIAL AND PRICES OF INNOVATIVE TECHNOLOGY

Erygin Y.V., Belyakov R.A.

Abstract

The innovative development of Russian economy, defined as a priority for economic policy in the conditions of market relations formation and development, is impossible without the formation of appropriate market instruments, among which one of the main is the formation of market innovation. The most important characteristics of the innovation economy is the innovative activity of enterprises and the level of demand and supply of different types of innovation. For the economy of modern Russia, the most pressing problem of technological development is the one which causes the increased demand for technological innovation. The solution to this problem largely depends on the underdevelopment of the market of innovative technologies and low demand from business. The problem is both caused by the development as well as by the situation in the country with business requirements. Technology Commercialization has determined their commercial potential, representing the economic value of improving the competitiveness of enterprises and production competitiveness on the domestic and foreign markets of innovative products. Defined are the requirements to innovative technologies as goods; given is the definition of the commercial potential of innovative technologies; the factors, influencing the market value of innovative technologies are sorted out, as well as the formation conditions of the prices for innovative technologies. Consideration of the commercial potential and pricing of innovative technology should contribute to the understanding of their importance for the stabilization of problems in business on the competitive market.
Siberian Aerospace Journal. 2015;16(3):782-786
pages 782-786 views

HUMAN CAPITAL AS A SYSTEM OF AEROSPACE ECONOMIC DEVELOPMENT

Oshchepkova D.S.

Abstract

Currently, the strategically important sector of Russian economy - aerospace industry - needs modernization and reorientation on the needs of modern economy - the knowledge-based economy. To implement this transformation there is a need in qualified creative personnel involved in the relationship with the human capital. The object of this study is the relationship of human capital (in the aerospace industry). This paper presents the analysis of the main approaches to define the essence of human capital, their classification (activity, income, investment, historical). Through the general properties of systems (hierarchy, integrity, emergence) was proved that the relationship of human capital is a system in which occurs the transformation of human resources (total health, knowledge, skills, etc.) into the asset of the enterprise. Scientific novelty lies in the allocation of system-forming element of human capital - intellectual property. In the author's definition of intellectual property lies the creative approach to the implementation of employee work, non-standard use of the means of production, resulting in the increased efficiency of the production process, and formation of competitive advantage. The presence of intellectual property can be expressed in the responsible attitude to work (the desire of the employee to perform labour operations efficiently and on time), pioneering (rationalization proposals), innovation activity. According to the article, the human capital management (as a system of economic relations) is beyond the scope of personnel management and requires a fundamentally new integrated approach that can improve the competitiveness of the aerospace industry. The results of this study are of scientific and applied character and can be used in the educational process and practices focused on the management of aerospace organizations.
Siberian Aerospace Journal. 2015;16(3):787-791
pages 787-791 views

CLASSIFICATION OF SOURCES OF INNOVATION IN THE MILITARY-INDUSTRIAL COMPLEX

Podverbnykh O.E., Sandanova B.D.

Abstract

The transition to innovative development of enterprises of the military-industrial complex suggests a wide distribution of innovation activity. Its role in the economy is improvement of management quality, its technological and commercial structure, marketing and sale of products, goods, services, forms of organization and production management. The military-industrial complex (MIC) is a part of the industrial complex in the country specializing on research, development and manufacturing of defense products and components for the Russian Armed Forces and other security agencies of the state. Innovative activity for the enterprises of defense industry is an important means of adaptation of economy in accordance with requirements of the time. Innovative activity in modern conditions is the most costly for the development of the perfect models of equipment on the existing level of knowledge, but with far-reaching possibilities in field equipment and in product sales. The first step in organization and management of innovation processes generating the use of science is the formation of ideas. Ideas can come from many different sources. The article is devoted to the study and classification of sources of innovation for enterprises of military-industrial complex. For classification of sources a matrix that includes both internal and external, and collective and individual sources of ideas has been developed. The classification of sources of innovation can effectively help to manage the company staff, including motivation of employees to further promotion of certain employees or groups of employees who are able to make the greatest contribution to the process of generating new ideas. The results will allow company managers to make a choice of strategy of innovative development of enterprises based on the availability of sources of innovation for companies. In the article the reasons of the choice between strategy technology push and market pull are given.
Siberian Aerospace Journal. 2015;16(3):792-796
pages 792-796 views

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