Стратегия технического обслуживания систем управления
The policy of maintenance support of a complicated engineering system, providing the maximum effectiveness of its service, is considered. The solved optimization problem of integer programming allows combining the structural elements of a project into groups, optimal from the position of minimization of inter-group connections.
System ASONIKA-K-MF is a VJ-visual environment reliability electron modules designed to automate the activities and management of the reliability of electronic equipment on the stages of projection-tirovaniya, manufacture, operation and scraps-tion . The system is designed as a client-server application that allows Playback izvodimost calculations and ease of operation.  Despite the fact that the software, similar to the system ASONIKA-K-MF, has not yet been created either in Russia or abroad, constant updating of operating systems has led to the fact that the client part of the system ASONIKA-K-MF-mouth RELA in the sense that was not compatible with modern operating systems Windows Vista / 7/8. Therefore, there was a task processing times, the new version of the client side (interak-tive interface) system ASONIKA-K-MF under the operating systems Windows Vista / 7/8, using modern methods and programming tools.
In article the analysis of architecture of control systems is carried out by computer networks, architecture of control systems with the built-in function of a forecast of conditions of a computer network are offered, the structure of modules and algorithms of functioning is described.
New electro-thermal simulation subsystem was introduced into Mentor Graphics IC Design flow. The subsystem incorporates IC thermal simulation tool “Overheat”, dispatcher “ETh SimCoupler” as the simulation manager and layout converter “ETh Model Generator”. Application example of power voltage regulator IC simulation is described. A good agreement between simulated and IR-camera measured temperature pictures is achieved.
Materials for the International Workshop on “Networked embedded and control system technologies: European and Russian R&D cooperation”
The automatic electro-thermal simulation has been implemented in Mentor Graphics PCB Design Flow. New program-dispatcher TransPower has been developed to control the electro-thermal calculation process, combining the programs of the electric (Analog Designer) and thermal (BETAsoft) simulation into a single cycle. As a result, the labor consumption and the PCB electro-thermal simulation time have been significantly reduced, the accuracy and reliability of calculations have been improved and the human errors have been eliminated.
Generalized error-locating codes are discussed. An algorithm for calculation of the upper bound of the probability of erroneous decoding for known code parameters and the input error probability is given. Based on this algorithm, an algorithm for selection of the code parameters for a specified design and input and output error probabilities is constructed. The lower bound of the probability of erroneous decoding is given. Examples of the dependence of the probability of erroneous decoding on the input error probability are given and the behavior of the obtained curves is explained.
The dynamics of a two-component Davydov-Scott (DS) soliton with a small mismatch of the initial location or velocity of the high-frequency (HF) component was investigated within the framework of the Zakharov-type system of two coupled equations for the HF and low-frequency (LF) fields. In this system, the HF field is described by the linear Schrödinger equation with the potential generated by the LF component varying in time and space. The LF component in this system is described by the Korteweg-de Vries equation with a term of quadratic influence of the HF field on the LF field. The frequency of the DS soliton`s component oscillation was found analytically using the balance equation. The perturbed DS soliton was shown to be stable. The analytical results were confirmed by numerical simulations.
Radiation conditions are described for various space regions, radiation-induced effects in spacecraft materials and equipment components are considered and information on theoretical, computational, and experimental methods for studying radiation effects are presented. The peculiarities of radiation effects on nanostructures and some problems related to modeling and radiation testing of such structures are considered.