Vol 18, No 3 (2017)

Articles

IDENTIFICATION OF HYDRAULIC RESISTANCE PARAMETERS IN HYDRAULIC NETWORK MODEL

Antropov N.R., Agafonov E.D.

Abstract

The work is devoted to the identification of hydraulic resistance coefficients in hydraulic network model. The prob- lem raised in the paper is relevant for enterprises dealing with either pipeline transport of fluid hydrocarbons, or water supply and central heating. The proposed algorithm can be implemented for corresponding technological modes calcu- lation and prediction. Complexity of real pipeline networks, uncertainty and instability of their parameters make parameters identification procedure indispensable. The network model under research is a system of nonlinear equa- tions, drawn up in accordance with Kirchhoff’s laws for pipeline networks. Equations describe laws of flows conserva- tion for nodes as well as pump heads and head drops along independent circuits of the network. To solve such system one traditionally implements Newton’s method or its modifications, for instance the successive approximation method. Mentioned methods have numerous disadvantages like instability and sensibility to initial approximation of the roots. The system of equations solving is accompanied with their parameters tuning usually with the Nonlinear Least Square Method. Again, the method can be instable due to overdefined and large-scale problem statement. In the paper we pro- pose to substitute solution of the system with nonparametric estimation of the solution. We implement regression type estimate with respect to residuals of the equations calculated for measured data sample. Simultaneously parameters of the equations are identified. Modification of Kiefer-Wolfowitz procedure is used as an identification algorithm. Iden- tification is performed with simultaneous evaluation of the solution of the system of equations. The use of appropriate algorithms is considered at three-loop pipeline network with a single active pressure. Numerical experiments with proposed algorithm demonstrate its applicability for practical identification problems solution.
Siberian Aerospace Journal. 2017;18(3):492-498
pages 492-498 views

STUDY OF HYDRODYNAMICS FEATURES IN THE APPARATUSES WITH MOVABLE NOZZLE

Danko V.P., Karnauh V.V., Titlov A.S.

Abstract

Apparatuses for the heat and mass transfer processes must be designed so that they have a maximum contact sur- face. Classification of heat-mass exchange apparatuses provides geometric features of the apparatus and the hydrodynamic condition they create. However, the main trend which remains dominant in the design of such apparatus is to create a thin film of liquid on the surface of the nozzle. The work was aimed at choosing the solution in which the MN of the heat-mass exchange apparatuses can be used to implement the contact handling process of gases and liquids with density values clarification of the nozzle elements (ρnе) and the column dynamic height (Нст) and obtain the specified calculated dependences which describe the hydrody- namics and mass transfer in the apparatuses with a movable nozzle, that is to create bases for engineering calculations. Research methods were theoretical study and experimental studies on heat and mass transfer devices with movable nozzle. The best ranger for mass transfer processes implementation is that of ρneІІ (ρ = 200-700 kg/m3), which is distin- guished by a wide working area according to wg, acceptable values of fluid withdrawal and a relatively small dynamic layer height. Within the described mode, we can distinguish the area wg @ 4.7-6.0 m/s, where there is no dependence of Hp on wg. Specified calculated dependence obtained which describes the hydrodynamics and heat and mass transfer in the apparatuses with a movable nozzle.
Siberian Aerospace Journal. 2017;18(3):499-504
pages 499-504 views

POSSIBLE OPTIONS TO IMPROVE CRYPTOGRAPHIC RELIABILITY OF ALGORITHMS BASED ON NYBERG CONSTRUCTION

Dmitriev M.A.

Abstract

Nowadays one of the most used tools to protect data from unauthorized access is block symmetric-key cryptographic algorithms. The rapid growth of computer processing power and significant development of linear cryptanalysis actual- ize the task to continue increasing reliability of the existing algorithms, as well as developing new ones. An important component in determining the stability of a block symmetric-key cryptographic algorithm to the most common types of cryptanalysis is the quality of S-box substitution. This work was aimed at calculating and achieving all possible S-box substitutions, based on irreducible polynomials over the Galois field and their compositions. For this purpose a set of programs to obtain S-box substitutions which have different cryptographic characteristics with its help was developed. Calculation of the quantitative values of these characteristics was performed by presenting S-box substitutions in the form of sets of Boolean functions. Particular attention was paid to such characteristics as nonlinearity of Boolean func- tions, the maximum modulus of the correlation coefficients and the numbers of zeros of the correlation matrix of S-box substitutions, as those are the most important characteristics. These blocks substitutions can be the basis for further study of possible options to improve Rijndael algorithm’s cryptographic reliability.
Siberian Aerospace Journal. 2017;18(3):505-509
pages 505-509 views

NON-PARAMETRIC ALGORITHMS OF RECONSTRUCTION OF MUTUALLY AMBIGUOUS FUNCTIONS FROM OBSERVATIONS

Korneeva A.A., Chernova S.S., Shishkina A.V.

Abstract

We consider the task of reconstruction of the regression function from observations with errors. Under parametric uncertainty conditions this problem is solved in the following sequence: first the type of regression function with accu- racy to parameters is set, then the next stage is the estimation of these parameters based on training sample elements. The main problem that arises is choosing a parametric structure, i. e. the choice of parameters with an accuracy to the vector of parameters. At the same time more or less inaccuracy can be allowed, descriptions of many variables func- tions with accuracy to parameters cause particular difficulties. Another known way of solving such problems, which is the nonparametric estimation of regression function from observations, in this case the stage of choosing a parametric equation of the regression function is missing. A number of publications is devoted to this area including monographs where the results are in most cases related to the asymptotic properties of the regression function. The article considers the task of reconstruction of mutually ambiguous functions of many arguments from observa- tions with random errors in the conditions of nonparametric uncertainty. This problem has been insufficiently studied, although it has a significant importance in the identification and control of objects of a Wiener and Hammerstein class. The control theory widely uses already known mutually ambiguous specifications that describe the work of items with a loop of hysteresis, backlashes and others. Some modifications of nonparametric estimates of mutually ambiguous fea- tures including multidimensional are given. A series of computing experiments have been conducted where for simplic- ity reasons the simpliest mutually ambiguous curves were taken, parametric structure of these curves for the algorithms was unknown, only observation was known. Numerical studies covered two cases: different sample sizes and various disturbances affecting the studied processes. The reconstruction of mutually ambiguous dependency plays an important role in the development of robots and various robotic systems moving on in an undefined or unknown terrain. As sepa- rate blocks the considered algorithms can be useful in devices that are used in the aerospace industry.
Siberian Aerospace Journal. 2017;18(3):510-519
pages 510-519 views

IMPEDANCE MISMATCH INFLUENCE AT INTERNAL DELAY OF NAVIGATION SIGNAL SIMULATOR CALIBRATION

Krat N.M., Savin A.A.

Abstract

This paper is devoted to navigation signal simulator calibration. The description of uncertainty estimation of inter- nal signal simulator delay, which is caused by impedance of measurement equipment (navigation signal simulator, analyzer and measurement cable) mismatch, is shown in the paper. The aim of research is to get expression to count uncertainty of simulator internal delay and to give its quantitative assessment. The uncertainty is caused by presence of reflected signal at the input of signal delay estimation algorithm. Reflected signal has place because input/output impedances of measurement equipment are different. The simplified mathematical model of signal at the signal delay estimation algorithm input is given. Correlation algorithm work for given model of signal has been analyzed. Two expressions for systematic uncertainty of delay estimation count have been derived and their inaccuracy has been esti- mated by means of modelling. The first expression is universal for all variety of navigation signals; the second is more accurate and takes into account spectral characteristics of the concrete navigation signal. The quantitative assessment of uncertainty, based on modern measurement equipment is given - at the length of measurement cable about one meter systematic uncertainty can reach 100-150 picoseconds. Conclusion was made, that at modern requirements to navigation signal simulators calibration, impedance mismatch must be taken into account. The information, mentioned in this paper, can be used at internal delay of navigation receivers’ estimation when receivers are calibrated by means of navigation signal simulator.
Siberian Aerospace Journal. 2017;18(3):520-524
pages 520-524 views

USING HIGH-PERFORMANCE COMPUTATIONS FOR STUDYING MODIFIED BUBBLE-SORT GRAPHS

Kuznetsov A.A., Kishkan V.V.

Abstract

The definition of the Cayley graph was given by the famous English mathematician Arthur Cayley in the XIX century to represent algebraic group defined by a fixed set of generating elements. At present, Cayley graphs are widely used both in mathematics and in applications. In particular, these graphs are used to represent computer networks, including the modeling of topologies of multiprocessor computer systems - supercomputers. This is due to the fact that Cayley graphs have many attractive properties such as regularity, vertex transitive, small diameter and degree at a sufficiently large number of vertices in the graph. For example, such a basic network topology as the “ring”, “hypercube” and “torus” are the Cayley graphs. Using supercomputer computations we obtained the previously unknown characteristics of modified bubble-sort Cayley graphs of dimensions 14 and 15.
Siberian Aerospace Journal. 2017;18(3):525-529
pages 525-529 views

TO GEOSTATIONARY COLLOCATION PROBLEM

Kuprin A.G., Medvedev A.V.

Abstract

This article is about geostationary collocation problem which means problem of cooperative station retention. As part of this task it is assumed that different control centers don’t exchange information about kinematic parameter’s vectors and maneuvers. So there is full information and control possibility for one collocation member only. Sets of kinematic parameter vectors are available for the other collocation members. This situation corresponds to lack of a priority information conditions, so there is f nonparametric uncertainty situation because due to absence of informa- tion on parametric control law which is used to choose maneuvers for other collocation members. Modern collocation theory doesn’t allow to avoid collision and process station retention in this condition. Synthesis of nonparametric regu- lator is in contemplation to solve this problem. First task of this regulator is estimation of previous maneuvers by proces- sing kinematic parameter vectors sets. Second task is estimation of coordinates for every collocation member. Finally, nonparametric regulator must synthesize control which allows to process station retention and collocation. Suggested algorithm belongs to nonparametric class, so it is not necessary to know parametric form of controlling law. It is based on modification of Nadaraya-Watson nonparametric estimation. The geostationary movement model including main perturbations, and most common collocation approaches are suggested. Nonparametric control algorithm is proposed.
Siberian Aerospace Journal. 2017;18(3):530-537
pages 530-537 views

DESIGNING THE PROBLEM-ORIENTED INFRASTRUCTURE FOR SIMULATION MODELING OF SPACECRAFT ONBOARD EQUIPMENT

Nozhenkova L.F., Isaeva O.S.

Abstract

The authors develop a subject-oriented environment of the spacecraft onboard equipment simulation modeling. This environment is basing on the Simulation Model Portability standard (SMP), which determines the technology for com- patibility and transferability of simulation models within big simulation projects of software-and-hardware complexes. There is a number of simulation infrastructures in the world space industry. They are used in big technical projects where it is important to integrate simulation models of different purpose, including those of different manufacturers, and to use them together. The support for the import-independence of Russian space developments should include the creation of domestic software products based on the standards of the European Space Agency. Such studies will make it possible to understand the principles of organization of complex projects and their integration into international research. We have designed a software architecture, proposed a division in software subsystems and described the main princi- ples of their interaction. Simulation infrastructure is aimed to support the work of the space systems’ onboard equip- ment designers. Its functions are determined by the basic tasks of the constructing: onboard equipment design support, generation and analysis of designer solutions at different stages of the space equipment production lifecycle. The architecture contains all the necessary components to provide transferability and workability of simulation models in the simulation modeling systems built on the basis of the SMP Standard. Our software extends the ap- proaches provided by the standard with the original methods of information-graphic and intellectual modeling. The authors have developed the methods and software of information-and-graphic modeling for visual building of the models, setting their structure and determining the links between their elements. To specify the methods of func- tioning of models, the authors suggest using condition-action rules. Our special instruments of knowledge base creation allow describing different variants of the modeled object behavior. The publication of the developed approaches and the software architecture opens up the possibilities of using SMP by other researchers in their own development, and also shows the main technological moments which are necessary to meet the requirements of the standard.
Siberian Aerospace Journal. 2017;18(3):538-544
pages 538-544 views

ABOUT TORSION OF PARALLELEPIPED AROUND THREE AXIS

Senashov S.I., Savostyanova I.L., Filyushina E.V.

Abstract

The theory of limit state deals with statically determinate condition of solids. In this case the system is closed due to extreme conditions, such properties of matter such as viscosity, elasticity, etc. cannot influence the limit state. In other words, when reaching the limit state the nature of the relationship between stress and strain has no effect on the ulti- mate state. The study of such systems has been consistently pursued by D. D. Ivlev and his coauthors. To the equilib- rium equations they attached two or an equation relating the components of the stress tensor. This led to the closure of the system of equilibrium equations. In the theory of plasticity equations, which are closed with a single yield stress are studied well. The most well-known system describing the ultimate state of deformable bodies are well-studied equations describing the torsion of the plastic bodies, the two-dimensional stationary problem of the theory of plasticity. The arti- cle discusses some other systems of equations which are closed only by one equation of flow, which corresponds to the classical theory of plasticity. It is assumed that the components of the velocity vector depend only on two spatial coor- dinates. In addition, for the component of velocity vector conditions of deformations compatibility are performed identi- cally. The constructed systems can be used to describe the twisting of the parallelepiped around the three orthogonal axes. For the constructed system of equations point group symmetries, conservation laws have been found. It is shown that the system allows 8 -dimensional Lie algebra. On the basis of the symmetry group some classes of invariant solutions of rank 1 have been constructed. They depend on arbitrary functions of one variable. It is shown that these solutions can be used to describe plastic torsion of a parallelepiped around three orthogonal axes. It is shown that the system admits infinite series of conservation laws. The concluding paragraph describes the construction of elastic solutions to the problem. It is shown that it boils down to finding three harmonic functions.
Siberian Aerospace Journal. 2017;18(3):545-550
pages 545-550 views

AIRCRAFT MONITORING IN REMOTE AREAS VIA THE LOW-ORBIT SATELLITE COMMUNICATIONS SYSTEM “IRIDIUM” ALONG WITH THE GSM DATA TRANSMISSION THROUGH ASC-6 TELEMETRY TERMINAL

Akzigitov A.R., Stacenko N.I., Pisarev N.S., Efimova A.N., Andronov A.S.

Abstract

One of the most important aims of air traffic control is continuous positioning of aircraft, which makes it possible to control a given flight plan and record deviations from the route, along with organizing search and rescue operations in case of an accident or a disaster. Great difficulties arise when performing this task in areas where there is no radar station in the mountains, forests, at high latitudes or at extremely low altitudes. This problem can be solved by using satellite navigation systems, satellite communication systems and automatic vehicle monitoring. In order to communicate with the control center, it is advisable to transmit data packets of up to 340 bytes contain- ing information about the location of the aircraft and its status. This can be done via GSM mobile networks, and in areas where there is no communication of this kind, via the satellite communications system “Iridium”. To put these two possible ways of communication into practice, the aircraft must have on board an ASC-6 GLONASS / GPS terminal (a vehicle-compatible modification), which determines location, speed and heading of the aircraft. It is also able to reg- ister a number of other parameters, such as the status of the analog / discrete inputs, and RS-232 connected sensors indications. This makes it possible to transmit to the control center not only the geographical position data, but also the speed of the aircraft and other operational data. A special communication module SM-1 can be used to support the sat- ellite communication, as it is ASC-6 compatible through RS-232 interface.
Siberian Aerospace Journal. 2017;18(3):552-557
pages 552-557 views

THE ALGORITHM FOR ESTIMATING RESERVES OF THE WORKING PROCESS STABILITY IN COMBUSTION CHAMBERS AND GAS GENERATORS OF LIQUID ROCKET ENGINES

Biryukov V.I., Nazarov V.P., Tsarapkin R.A.

Abstract

The experimental evaluation of the working process stability with respect to acoustic oscillations in combustion chambers and gas generators of liquid rocket engines is one of the main methods used in rocket engine construction. External and internal disturbing devices using explosive hexogen often lead to the damage to the fire walls and struc- tural elements of the aggregates The disadvantages of traditional external impulse devices also include a considerable wide range of the pressure pulses values generated by them in the combustion chamber with the same value of the sam- ple of the explosive and with the constant parameters of the atmosphere in the combustion chamber, which is due to the scatter of the explosives characteristics. An alternative approach is proposed for creating a pulse effect on the working process in the combustion chamber by exploding an electrical conductor. The disturbing device is made with an explo- sive chamber connected by a channel with the reaction volume of the combustion chamber. In the electro-impulse dis- turbing device a thin wire fastened to isolated electrodes is used instead of the charge of the explosive. As a substance used to create a pressure pulse, this generator uses gas filling the blasting chamber, the mass of which depends on the pressure in the combustion chamber and in the chamber of the electro-impulse perturbative device. If one immediately heats this gas to a temperature of several thousand degrees, one can get a gas that is close in parameters to the com- bustion products of explosives in traditional external impulse devices. Such heating can be carried out by discharging through a wire of an electric capacitor charged to several thousand volts. First, instantaneous (for several microsec- onds) evaporation of the wire, and then through the plasma channel formed at the site of the wire, the final discharge of the capacitor takes place, with virtually all of the energy stored in the capacitor discharged. The plasma temperature in this case, according to different sources, can reach from several tens of thousands to one million degrees. The gas is also heated by adiabatic compression with a shock wave. The metal particles formed after the evaporation of the wire and the condensation of the vapor have a value of several nanometers and, therefore, do not damage the inner layer of the combustion chamber. The methodological bases are considered and the algorithm for estimating the stocks of stability to acoustic vibrations from the reaction of the combustion process to such pulsed artificial disturbances is developed. There have been developed electro-impulse disturbing devices that reduce the risk of damage to the compo- nents of liquid rocket engine assemblies in full-scale and model test, and have an obvious prospect for widespread use.
Siberian Aerospace Journal. 2017;18(3):558-566
pages 558-566 views

AUTOMATED WEIGHT COMPENSATION SYSTEM FOR GROUND-BASED TRYOUT OF SPACE VEHICLE SOLAR PANELS

Verhoglyad A.G., Kuklin V.A., Makarov S.N., Mihalkin V.M., Halimanovich V.I.

Abstract

In the process of ground-based tryout of solar panels placed aboard the spacecraft there appears the problem of gravity effect compensation. The energy of deployment mechanism is extremely limited, the weight and strength of the structure being calculated for weightlessness conditions. Therefore, under the force of gravity, the power of deployment drives may not be enough to complete the tryout, and the structure itself may be destroyed. Taking into account these difficulties, specialized stands the main part of which is the so-called weight compensation system are designed and created to conduct ground-based pilot tryout. Active weight compensation systems are most effective in this case. In the stands with active weight compensation systems all forces generated by the stand and movements of the stand parts occur through controlled drives. By introducing various sensors into the weight compensation system and by the use of their signals for generation of controlling actions in the control system it becomes possible to significantly increase the level of gravity effect compensation, as well as to minimize the influence of the stand parts inertia. The paper presents the results of the designing, building and testing of the automated active weight compensation system for solar panels. The system provides weight compensation when conducting ground-based experimental tryout of any objects (solar panels, rods, multi-tier spokes, etc.) having a long and transformable in one direction form for distances of the order of 20 m (longitudinal direction). This system also provides movement of the pieces of a tested object in the transverse direction and in height for distances of up to 5 m. The results of departmental tests showed that the weight compensation system with specified parameters described in this paper allows for ground-based tryout of the deployment of solar panels of all constructions, both currently existing and being developed for the future.
Siberian Aerospace Journal. 2017;18(3):567-574
pages 567-574 views

OPERATING TEMPERATURE AND ITS INFLUENCE ON THE RADIATION OF PHASED ANTENNA ARRAYS

Kartsan I.N., Efremova S.V., Shangina E.A., Logacheva A.I., Gorev Y.S.

Abstract

A current mainstream phenomenon is the design of ground based and onboard multifunctional radio electronics complexes, which are based on new technical solutions, including the application of active phased antenna arrays. This boosts the functional integration of the system equipment. Depending on the tasks, such antenna systems contain from hundreds to several thousand active modules. In this regard, the probability of failure of the active module drastically increases in comparison with the passive phased array. In these circumstances, ensuring the efficiency of active phased antenna arrays is a paramount task. In this paper we discuss the influence of operating temperature on the radiation characteristics in active phased antenna arrays onboard spacecraft.
Siberian Aerospace Journal. 2017;18(3):575-579
pages 575-579 views

STUDENT PICOSATELLITE PLATFORM SIBQUBE: DEVELOPMENT OF PROTOTYPE STRUCTURE OF POCKETQUB CLASS PICOSATELLITE

Kravchunovsky A.P., Draganyuk M.N., Zuev D.M., Skorobogatov S.A., Movchan P.V.

Abstract

The article includes the conception and several results of the development of the PocketQub student spacecraft, namely the prototype of the student satellite SibQube is designed. In the article there are some midget spacecrafts stan- dards known for today, their main distinctions which are consisted in dimensions of the satellite and its tasks. The arti- cle defines the goals of the creation of the platform: its usage in the educational sphere and running experiments in the space area. This article presents the most major factors of developing and projected constitution of the service platform of the midget spacecraft. After testing the spacecraft body and its further modifications, it is possible to use it as the base for the range of midget spacecraft bodies intended for the researching of atmosphere top layers and near-the-earth space. We designed and produced the prototype of the spacecraft body. The article describes the body construction of developing PocketQub spacecraft and usage of the structure elements of the construction and their functioning particularities in it. We defined the materials for the model producing. Besides, the article describes reasons for their choice. In addition, we have made a strength analysis of satellite structure, namely mode identification analysis to find normal frequencies, static analysis of the effects of linear accelerations within limits of 20 g, appeared during the flight of the Dnepr launch vehicle, and dynamical analysis of random influences. Based on the results of the analysis preliminary conclusions were made about the construction strength and stability when the determinants discussed above influence.
Siberian Aerospace Journal. 2017;18(3):580-584
pages 580-584 views

SUBSYSTEM OF PHYSICO-CHEMICAL REACTORS OF MINERALIZING WASTES FOR SPACE APPLICATION BIO TECHNICAL LIFE SUPPORT SYSTEMS

Morozov Y.A., Trifonov S.V., Saltykov M.Y., Murygin A.V., Tikhomirov A.A.

Abstract

The Department of Closed Ecological Systems of Reshetnev Siberian State University of Science and Technology together with the Institute of Biophysics SB RAS are developing the artificial high-performance physicochemical link of the decomposers for bio technical life support systems for space applications, in particular for the forthcoming experiment BIOS-4 with a crew of 3 people. The physicochemical processing of waste is required because of the very large buffer capacities thus masses for orbital launching of many natural components comprising the biological waste treatment links. A subsystem of physicochemical reactors for the processing of wastes into fertilizers for cultivating edible plants on hydroponics is being periodically improved. Different versions of the similar functional links with dif- ferent characteristics are being developed in parallel. The subject of the article is the subsystem of physical-chemical rectors of organic waste processing in the bio technical life support system BIOS-4. The aim is to present the review of peculiarities of the development of the organic wastes treatment physical-chemical reactors subsystem based on “wet combustion” method, as well as its automation and computer monitoring of the process flow parameters. The consid- ered technological subsystem of organic wastes treatment into fertilizers applied to space application closed ecosystems comprises the reactors of “wet combustion”, urea decomposition, and H2O2 synthesis. The authors develop a united interface of collecting data of the reactors operation parameters, and the reactor’s automation control system. Techni- cal details of the ongoing, developed and projected processes are presented. A holistic view has been given of the physical-chemical reactors waste processing link at the BIOS-4 experimental facility today. To date, existing installa- tions or conceptual solutions for their development, including automation, are presented for all the main links of the technological chain of waste processing with reference to the bio technical life support systems for space purposes, and their optimization and experimental verification are carried out.
Siberian Aerospace Journal. 2017;18(3):585-591
pages 585-591 views

THE STUDY OF THE FLOW IN THE VAPOUR CHANNEL OF SHORT LINEAR HEAT PIPES

Seryakov A.V.

Abstract

E-mail: seryakovav@yandex.ru The results of studies of flow of moist vapour in Laval-like vapour channels of short linear heat pipes (HPs) are pre- sented. The increase in heat transfer coefficient of short linear HPs, intended for creation of the cooling systems of heat-stressed designs of spacecraft, is carried out by making the HPs vapour channel forms similar to the shape of the Laval-like nozzle. Comparison of the heat transfer coefficients of short HPs with the standard cylindrical vapour channel and the channel, made in the form of the Laval-like nozzle with the equality of all dimensions, flat evaporator and the same amount of the working fluid, shows that the HPs with the vapour channel in the form of the Laval-like nozzle exceeds the heat transfer characteristics of the standard HPs with a cylindrical vapour channel under high ther- mal loads. The study of the flow and condensation in such shaped vapour channels of the short HPs at high thermal loads gives an opportunity to analyze in detail the advantages of using such HPs and make the conclusion about the necessity of wide introduction of such HPs for the cooling systems of the spacecraft. Capacitive sensors were addition- ally installed in cooled top covers of the HPs, and electromagnetic pulses with a frequency of 100 kHz were supplied to them from the external generator. At heating the HPs evaporator, starting from a certain thermal power threshold value, electromagnetic pulses became modulated. It is related to the formations of the boiling process in the capillary- porous evaporator and large amount of vapour over it and its discontinuous distribution. It was discovered that the frequencies of the pulsations are more and they occur at lower values of heat load at the evaporator in the HPs with a vapour channel of a Laval-like nozzle, compared to the HPs with the standard cylindrical vapour channel with equal overall dimensions.
Siberian Aerospace Journal. 2017;18(3):592-603
pages 592-603 views

HARDWARE IMPLEMENTATION OF THE UNIT OF THE GNSS CONSUMER

Sokolovskiy A.V., Veisov E.A., Ratushniak V.N., Rizhkov D.N., Vysotsky S.V.

Abstract

Navigational equipment is currently used to solve a variety of tasks, such as providing civil and special aviation, navigating, surveying and mapping, Internet devices and unmanned vehicles perfomance. The level of technological development of digital signal processing devices at first glance removes the need for deep study of computational algorithms, but this is only at first glance. As a result of expanding the scope of navigation tools, there is a need to increase the working channels, increase the dynamic range of the processed signals, and also improve the reconfiguration capabilities of signal processing devices. Any synthesized computational algorithm that can be described in hardware description languages, such as VHDL and Verilog, consists of summation operations and a shift operation of the register. There are several basic architectures of adders, each of which has the advantage of either speed of operation or simplicity of implementation. The development of computational architectures working at frequencies of 100 - 200 MHz requires pipeline calculations. Despite the fact that the pipeline architecture has large overheads for equalizing the delays of the computational blocks, its use is justified when processing and converting signals while solving the navigation task. The architecture of hardware computational blocks for constructing navigation equipment for the GLONASS / GPS consumer is considered in the article. The possible ways of increasing the efficiency of some architectures when implementing them on the basis of programmable gate arrays (FPGA) are given.
Siberian Aerospace Journal. 2017;18(3):604-608
pages 604-608 views

SIMULATION MEANS OF ELECTROSTATIC DISCHARGES IN THE SYSTEM “STATIONARY PLASMA THRUSTER - TRANSFORMATION AND CONTROL SYSTEM”

Trofimchuk D.A., Bezhayev Y.A., Ivanov V.V., Kochura S.G., Maximov I.A.

Abstract

The elements of construction of electric propulsion system of spacecraft (SC) correction can accumulate electro- static charge due to interaction with the magnetospheric plasma. The impact of electrostatic discharges on the electri- cal circuit of the correction system can lead to failures of the transformation and control system (TCS). Particular attention is currently being paid to solving the problems related to the impact of electrostatic discharges on electric circuits of the power conditioning units, designed for power supply and control electric propulsion thrusters of space craft correction. Due to the design of the propulsion subsystem thrusters it is impossible to solve the problem of electric charge impact on TCS electric circuits through shielding these circuits. Therefore the impact of electrostatic discharges on electric circuits from the propulsion subsystem thruster is considered to be one of the factors determining the reliability and failure-free operation of TCS and, consequently, of the overall spacecraft propulsion subsystem. This problem is important today due to the following: the widespread use of electric propulsion thrusters in GEO spacecraft correction systems, the implementation of new TCS design and technical solutions suitable for spacecraft unpressurized platforms, the implementation of new electronic component base. The paper addresses the simulation means of electrostatic discharges occurring on the ceramics of the stationary plasma thruster and impacting TCS electric circuits, in particular the test equipment for generating high-voltage pulses, which allows replacing long-term and expensive tests performed on vacuum test benches. The paper contains the review of validation test results for TCS means of protection from electrostatic charge effects using high-voltage pulse generat- ing (HVPG).
Siberian Aerospace Journal. 2017;18(3):609-616
pages 609-616 views

STUDY OF DUAL CONTROL ELECTRONIC LOADS FOR SPACECRAFT ELECTRICAL POWER SYSTEM TESTS

Fedchenko A.S., Mizrah E.A., Lobanov D.K.

Abstract

In the article the possible topologies of electronic loads consisting of linear regulator and switched-mode converter are studied. During developing and testing of spacecraft power supply systems, there is a need for devices that simulate various electrical characteristics of the spacecraft payload. This problem can be solved using specialized electronic loads that allow reproducing static and dynamic characteristics of the simulated payload with required accuracy. In addition, using electronic loads it is possible to return unused electrical energy into a DC or AC power supply network, which, in turn, makes it possible to improve the quality of power supply system tests. The development of a device that simultaneously provides both specified accuracy of reproduction of payload electrical characteristics and the recovery of surplus electric power is associated with a number of technical difficulties that can be solved by using an electronic load that includes two controllable stabilizers: a high-speed linear regulator and a switched-mode converter which limits the dissipated power of the linear regulator and provides recovering an excess electrical energy to the supply network. Various properties of dual control electronic load topologies were considered, the most promising topologies that can be used as electronic loads for spacecraft power systems tests were highlighted. A mathematical description of the electronic load used in the test setup was developed, an analysis of the admittances and the quality of noise suppression for various topologies was performed. The aspects of the electronic load operation related to the input current interfer- ing mode, the parameters determining the frequency range of the interfered noise, and the conditions for the possibility of the interference were determined for four topologies under the same conditions.
Siberian Aerospace Journal. 2017;18(3):617-627
pages 617-627 views

IMPROVEMENT OF INSULATION RESISTANCE MEASUREMENT ACCURACY DURING SPACECRAFT POWER SYSTEM TESTS

Shtabel N.V., Samotik L.A., Mizrah E.A.

Abstract

Modern spacecraft power systems features connection of ground power bus with satellite body, which aims to im- prove noise immunity and protect power system and its modules from possible breakdown due to static charge accumu- lation on spacecraft body, which can lead to high voltages between spacecraft body and power system sensitive elec- tronic components. The main disadvantage of this solution is a possibility of short circuit between any high voltage power system bus and spacecraft body, which can easily lead to breakdown of power system modules, payload elements and wire harness, making satellite dysfunctional. To prevent such malfunction situations during terrestrial testing and spacecraft lifetime the authors developed automatic insulation resistance continuous monitoring device based on con- tactless leakage current measurements on every spacecraft power system line. In the device magnitude of measured differential currents can be very low, in order of microamperes. Modern magnetic modulation based leakage current sensors has a major flaw which leads to great influence of high current magnetic field on a measurement result and highly increased insulation resistance measurement error. The authors has studied magnetic modulation based leakage current sensors, proposed the method of error compensation for studied measurement errors using additional current sensor, developed and tested device using proposed principles and done experimental study of device development version. Developed automatic insulation resistance continuous monitoring device implemented on the laboratory spacecraft power system test bench, at present the authors are preparing additional experiments to improve methodo- logy, quality, accuracy and convenience of recently introduced insulation resistance measurement methods.
Siberian Aerospace Journal. 2017;18(3):628-632
pages 628-632 views

INVESTIGATION OF THE POSSIBILITY OF USING A DEFLECTING SYSTEM FOR MAGNETIC FIELDS IMPACT COMPENSATION DURING ELECTRON-BEAM WELDING

Druzhinina A.A., Laptenok V.D., Laptenok P.V., Murygin A.V.

Abstract

The impact of magnetic fields caused by thermoelectric currents and residual magnetization of the welded parts on the accuracy of an electron beam positioning along the welded joints is a complicated scientific and technical problem to achieve high quality of welds in the aerospace industry, shipbuilding and power engineering. Presented in the article mathematical models of distribution of magnetic fields of interference in the space between the electron beam gun and the surface of a welding workpiece and also inside a workpiece allow to culculate the quantitative characteristics of the electron beam deflection from welded joints. The authors propose to use a deflection system for compensation of mag- netic interference impact. The deflection system must be set to a certain height above the workpiece to be welded. The authors obtained a mathematical model of the magnetic field induction of the deflecting system distribution along its axis which coincides with the optical axis of the electron beam gun. The coordinates of installation of the deflection system concerning the surface of the parts to be welded are determined using the presented mathematical models. Cal- culations showed that the height of installation of deflection system depends on the thickness of the welded components. Using the deflection system installed at a certain height above the workpiece to be welded allows to eliminate the impact of magnetic fields caused by thermoelectric currents and residual magnetization of the welded parts on the quality of welded joints.
Siberian Aerospace Journal. 2017;18(3):634-641
pages 634-641 views

METAL LAYER THICKNESS INFLUENCE ON THE DISPERSION CHARACTERISTICS OF SH-WAVES IN THE STRUCTURES “ME/ZNO/ME/DIAMOND” AND “ME/ALN/ME/DIAMOND”

Zolotova O.P., Burkov S.I.

Abstract

The research paper presents the results of computer simulation of the influence of mass loading represented by two metal layers on variations in the phase velocity of the dispersion shear modes of the elastic wave in the piezoelectric layered structures Me/ZnO/Me/diamond and Me/AlN/Me/diamond depending on the frequency and the ratio of the metal layer thickness to the piezoelectric crystalline layer thickness. The materials of the piezoelectric layers and the substrate have a set of such significant properties as the large values of the electromechanical coupling coefficient for piezoelectric and the significant values of the phase velocities for bulk waves and surface acoustic wave in diamond. Aluminum (Al), molybdenum (Mo) and platinum (Pt) are considered as the metal layer materials, which are most often used in the manufacturing of acoustoelectronic devices. It was found that variation in the elastic wave phase velocity depends on the acoustic impedance of metal layer and its thickness. More significant changes in Δv/v values at low acoustic impedance values of the metal layer occur due to a change in the thickness of the lower electrode. However, if the acoustic impedance of the metal layer is comparable with the acoustic impedance of the substrate, the increase in Δv/v values is largely due to the thickness of the upper metal layer. The results of the simulation can be used in the development of various acoustoelectronic devices, including components of the electronic base of rocket and space technology.
Siberian Aerospace Journal. 2017;18(3):642-650
pages 642-650 views

NANO MODIFICATION OF POLYMER BINDER WITH THE AIM OF IMPROVING THE PROPERTIES OF CARBON FIBRE MATERIALS

Krushenko G.G., Iseeva O.A.

Abstract

One of the problems in space engineering is the reduction of masses parts, assemblies and mechanisms as the actual spacecraft, and the means to deliver it to the orbit, i. e. booster. Progressive solution of this problem is the use of so- called net (anisogrid) structures. And currently mesh structure, the material for which is carbon fiber, are widely used in space technology for the manufacture of hollow tubular and conical designs of the spacecraft. The most common method of making carbon mesh designs is the winding of carbon fibers. However, with all the positive qualities of CFRP structures, in connection with the pointedness of their structure, and their effective use is possible only under uniaxial loading when tensile and compressive stresses coincide with the fiber direction. In the case of complex resis- tance or bending when the material occurs in the complex stress state can cause the destruction, as from the action of shear stresses and normal stresses. Strict fiber orientation in one direction leads to anisotropy of physical and mechanical properties of unidirectional composites. When the load applied normal to the direction of the fibers is destroyed by carbon fiber construction practically without preliminary plastic deformation. The problem of improving the mechanical properties of the CFRP materials was successfully solved by introducing in the polymer binder nano- powders of different chemical compounds - a process called nanomodification. And, in this regard, the most effective was the carbon nanopowders, including nanodiamonds.
Siberian Aerospace Journal. 2017;18(3):651-657
pages 651-657 views

IMPLEMENTATION OF AUTOMATED SYSTEM FOR MANUFACTURING OF PIPELINES OF ROCKET ENGINES

Yartsev E.N., Nazarov V.P., Teryaev N.S.

Abstract

Production and assembling of pipelines to liquid rocket engines is a difficult technological challenge associated with the placement of pipelines in confined spaces. Currently, the industry standards describe the main method by which developed a set of technical documentation for the manufacture and placing of pipes into rocket engine. Thus this technology requires large amounts of manual labor and does not guarantee the optimal configuration software and the quality of products. The solution of these problems is introducing in the production process of liquid rocket engine automated manufac- turing of pipes system, which use 3D-modeling. It allows to eliminate the complex and time-consuming process of manufacturing pipe’s model, reduce labor in the process of production liquid rocket engine, improve accuracy of manufacturing and assembly of the pipeline, to eliminate the need to tuck a pipeline during assembling to liquid rocket engines, be excluded from the design of the engine compensating units. The article proposes the solution for the modernization of technological assembly process liquid rocket engine, aimed at increasing productivity and product quality. The paper presents the algorithm of the automated manufacturing system of pipelines, considers the technical conditions for the development of the control program (technology) bending pipes on machines with numerical program management.
Siberian Aerospace Journal. 2017;18(3):658-662
pages 658-662 views

PROJECT MANAGEMENT OF INNOVATIVE ACTIVITY IN TOSER

Avramchikova N.T., Danilchenko Y.V., Poochkin M.B.

Abstract

A project management differs from management in the classical meaning of the word. It's an issue of flexibility de- pending on the scale, the specificity and novelty of the projects. Especially these differences become visible regarding the innovative activity management in the system of state Executive bodies in the territories of priority socio-economic development (TOSER). TOSER is a part of the territory of the Russian Federation. It includes closed administratively- territorial formations (ZATO), which in accordance with the decision of the Government of the Russian Federation established a special legal regime of business activities. Project management is essentially a combination of process and functional approach to management. But it has its special advantages, to more effectively manage such a complex process as innovation. The definition of the project management of innovative activities in TOSER takes into account the specifics of innovation development ZATO. It is a management discipline that defines the coordinated work of state bodies, local authorities and business representatives to create preferential treatment to conduct innovative activities in the territories of priority socio-economic development, taking into account the interests of their residents, the state, region and municipal community and ensuring the rational use of budget resources. The flexibility of project manage- ment depending on the scale, the specificity and novelty of the projects allows you to choose the optimal governance structure - functional, matrix or project. Design management of the innovative activities in the TOSER is conducted by the operating company. It is a joint-stock company, which is defined by the Government of the Russian Federation in order to carry out the functions for managing territories of priority socio-economic development. Tasks to further improve the system of project management of innovative activities in TOSER are the harmonization of the regulatory framework, sustainable funding for innovative projects and accelerated training of qualified personnel.
Siberian Aerospace Journal. 2017;18(3):664-672
pages 664-672 views

COMMERCIALIZATION INNOVATIVE POTENTIAL OF DEFENSE INDUSTRY ENTERPRISES: FORMS AND METHODS OF NETWORK INTERACTION WITH OBJECTS OF INNOVATIVE INFRASTRUCTURE

Erygin Y.V., Borisova E.V.

Abstract

The role of innovative infrastructure in the solution of problems of commercialization of innovative capacity of the enterprises of the defense industry complex in the article is defined. The article is devoted to the formation of the mechanism of commercialization of innovative capacity of defense industry enterprises. The essence of this mechanism consists of forming of network interaction between objects of innovative infrastructure and defense industry enterprises which possess unique elements of innovative potential. These objects of innovative infrastructure include objects of market, investment and financial infrastructure of national and international level. Involvement of objects of innovative infrastructure and defense industry enterprises in a commercial turnover allows carrying out fully commercialization of innovative products, technologies, services. Creation of network interaction of defense industry enterprises and objects of innovative infrastructure is based on combination of their efforts and coordination in the uniform chain. This association is carried out on the basis of mutual interest for achievement of the general end results of implementa- tion of innovative projects in the course of commercialization. Criteria of the choice of forms of network interaction are offered: the nature of interaction of objects of innovative infrastructure, sufficiency of resources for realization of busi- ness processes. The method of the choice of forms of network interaction of objects of innovative infrastructure is developed. This method provides achievement of the minimum expenses at realization of portfolios of business proc- esses and decrease in risks of functioning of objects of innovative infrastructure. The use of the offered organizational forms of network interaction allows involving the state, banks, innovative funds and objects of innovative infrastructure. It participates in the distribution of risks of realization of portfolios of business processes of innovative projects between all participants of network interaction. It promotes diversification of risks and allows considering organiza- tional interaction as one of the ways of decrease in the innovative risks arising in the course of commercialization of innovative capacity of defense industry enterprises. The author’s instruments of creation of network interaction of objects of innovative infrastructure can be used by federal and regional authorities when developing the directions of further development and increase in efficiency of functioning of innovative infrastructure of regions and also all par- ticipants of process of commercialization in general.
Siberian Aerospace Journal. 2017;18(3):673-679
pages 673-679 views

SOCIAL AND ECONOMIC POLICY OF KRASNOYARSK TERRITORY AS A REGION OF INNOVATIVE DEVELOPMENT

Sochneva E.N., Voronin E.A., Zyablikov D.V.

Abstract

The paper presents the relevance of regional planning. It proves that the innovative way of regional economy devel- opment is the most effective at the present stage. Each region follows its own way of innovative development and each one has its own peculiar characteristics. Krasnoyarsk Territory is one of the regions of innovative development, which is proved by various researchers and independent research agencies classifying the regions of Russia on different grounds. Thus, the region with the focus on innovative economic development requires a special social and economic policy, consisting of two aspects - social and economic. Social policy should reproduce human capital as the main fac- tor in the social and economic development of the region. Human capital, in turn, is formed from three interconnected components: reproduction of human resources (demographic policy), their formation and focus vector (employment policy on the labor market) and development of human resources or transformation of human capital into human poten- tial (education policy). For each of the three specified directions, particular recommendations are given within the framework of innovative development. It is necessary, for instance, to introduce a number of benefits that enable moth- ers to combine their work (study) and their main female function to stimulate the demographic policy. Within the framework of the employment policy, it is proposed to strengthen vocational guidance work to help young people’s choice in the labor market. The education system should be made more accessible to all segments of population in order to increase its efficiency and quality. As for creating economic basis for innovative development, various forms of business associations and consolidations, such as strategic scientific alliances, investment public-private partner- ships and technology platforms are proposed. Technological platforms can become an effective form of business for Krasnoyarsk Territory, since they will make it possible to use the scientific potential of large universities in the region. The place of small businesses and self-employment in the regional economy of innovative type is defined as an auxiliary infrastructure of large industrial associations in the region.
Siberian Aerospace Journal. 2017;18(3):680-689
pages 680-689 views

This website uses cookies

You consent to our cookies if you continue to use our website.

About Cookies