ISSN 0021-3454 (print version)
ISSN 2500-0381 (online version)
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Summaries of the issue

SPACE INFORMATICS

13
Questions of infrared spectroscopic devices application for atmosphere monitoring from small space vehicle are considered. It is shown that using of tunable interferometers with sub-nanometers spectral resolution is more preferable.
SIMULATION OF INPUT INFORMATION OF SMALL SPACE VEHICLES OPTIC SYSTEM Vyacheslav F. Fateev, Vladimir N. Lagutkin, Alexander P. Lukyanov, Evgeny N. Podkorytov, Yury V. Slynko, Aleksey M. Starostenko
18
Detailed model of forming input information of small space vehicle equipment at observation of natural objects is developed, and takes into account dynamics of atmospheric processes, optical properties of clouds with various microphysical compositions, of Earth surface.
22
Considered principles of building of the perspective cosmic system base on small multispectral satellites of the observation. The particularity of the system is a cluster orbital building, increasing its functional possibilities at decision of the problems of the remote flexing of Earth. Happen to the features of the onboard multispectral equipments of the small space vehicle of the observation.
29
An emergency composition and basic requirements for the efficiency of their solutions are defined. An automated system structure to emergency monitoring is proposed. The ecological monitoring results in North- West region got with use satellite remote sensing and estimations of the monitoring efficiency are represented.
METHOD OF SIGNAL PROCESSING IN SPACE-BASED MULTIPOSITION SAR SYSTEMS Alexander V. Ksendzuk, Vyacheslav F. Fateev, Sergey A. Popov
34
Optimal processing method in multiposition synthetic aperture SAR based on microsatellites considered. Main definitions, optimal processing algorithms and modeling results presented. Quality of radar images in multiposition and monostatic radar compared.
SMALL SPACE VEHICLE OF SEA SURFACE OBSERVATION WITH USE OF SIGNALS FROM GENERAL NAVIGATION SATELLITE SYSTEMS Igor V. Sahno, Eugeny A. Tkachev, Denis A. Gavrilov , Konstantin K. Uspensky
40
In paper the opportunity of creation of the passive radar-tracking system of a marine surface review is considered on the basis of SSV with usage of signals GNSS GLONASS, GPS and Galileo; power calculation of a radiolink „the transmitter—a surface—the receiver“ is resulted.
TECHNICAL-ECONOMICAL APPROACH TO THE CHOICE OF SMALL SPACE VEHICLES SYSTEM Vladimir I. Gorbulin, Valery V. Panchenko, Nickolay V. Radionov
46
On the basis of small spacecrafts system application for specified area observation by complex of varied utility airborne hardware for the first time is defined the correct mathematical set of technical and economic task for choice a list of system and airborne hardware that implements desired validity of information obtained when funding is limited. The task decomposition was allowed preparing a method of separate solution for technical task with admissibility criterion and economical optimization task.
PERSPECTIVE NETWORK FOR A LOCAL GROUP OF SMALL SPACE VEHICLES Vyacheslav F. Fateev, Каргу Д. Л.
52
A practical experience of creating a wireless data network on the basis of two-transmission systems, microwave in a small weight performance, designed to expand the local orbital grouping of small spacecraft. An alternative structuring rekonfiguriruemoy distributed payload. The results of the analysis of technical solutions to existing hardware range ISM.

MONITORING AND DIAGNOSING OF A CONDITION SMALL SPACE VEHICLES

ONBOARD MONITORING AND DIAGNOSTIC SYSTEM OF SMALL SPACE VEHICLES Anatoly M. Baranovsky, Alexander E. Privalov
57
The authors consider the structure and principles of operation of the monitoring and diagnostic system as a part of the onboard control complex of satellite, that provide off-line solution task of estimation and control of satellite operating conditions in compliance with current situation.
62
The authors consider the new indexes authenticity control technical condition complex systems on the basis of model hardware the theory probability and possibility. The article contains formulas for determination authenticity control.
68
There are comparative values of automatic management system process of rocket launch and spacecraft launch. There are rational automatic management system structure choice recommendations and apparatus and programme means surplus limits definition recommendations also performed. The real automatic management system — structure, which can be used with little spacecrafts launches is considered. The came out results better use on complicated informational management systems.

ONBOARD EQUIPMENT AND RESEARCH OF DRIVING SMALL SPACE VEHICLES

SMALL DIMENSIONAL CONTROL ONBOARD SYSTEM OF SPACE VEHICLE Каргу Д. Л., Georgy V. Kremez, Eugeny P. Minakov, Peter V. Nikolaev, Sergey А. Fedorov
72
The shape of an onboard complex of management low orbital the microsatellite of remote sounding of the Earth is proved. The complex integrates in itself functions of reception, decoding and realization of working programs and single commands of management, gathering and transfer of the telemetering information, management of functioning of the onboard equipment, definition of parameters of orientation and management of movement of the microsatellite.
UPGRADING OF RELIABILITY OF SMALL SPACE VEHICLE ONBOARD COMPUTER BY EXPERIMENTAL RESULTS Alexander G. Basyrov, Vladimir A. Goncharenko, Vyacheslav S. Zabuzov, Georgy V. Kremez, Konstantin A. Esaulov
76
With reference to construction of onboard computing systems the expediency of the multimodular approach with the adaptive organization of service is proved. Opportunities of maintenance of the set productivity in conditions of influence of destabilizing factors are considered. Results of the natural experiments are taken into account.
81
There is analytical method of calculation of realative tethered motion of spacecraft and mini-, microsatellite during the different laws of strength tether. Stretch tether with microsatellite direct the orbit flat of motion centre mass of space tether system. Relative motion microsatellite investigate in mobile orbit system.
THE MODELING STAND FOR SMALL SPACE VEHICLES ONBOARD OPTOELECTRONIC SYSTEMS TESTS WITH TARGET-OBJECT MAP IMITATION DEVICE USE Dmitry V. Kirichenko, Andrey A. Gluschenko, Konstantin K. Maslov, Konstantin I. Upitis
84
The example of development of the modeling stand for onboard optoelectronic systems tests with use target-object map imitation device on TFT-monitor basis. Results of the given modeling stand application and it’s information model structure are presents.