PART 1. INFORMATICS, COMPUTER TECHNOLOGY AND MANAGEMENT
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Ivanov V. A., Erkaev N. V.
SEMI-ANALYTICAL METHOD FOR CALCULATING ELASTIC-HYDRODYNAMIC CONTACT
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Lvova A. P.
DEVELOPMENT OF METHOD FOR INCREASING SENSITIVITY IN WIRELESS OPTICAL DATA TRANSMISSION CHANNELS IN VISIBLE WAVELENGTH RANGE
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Raskina A. V., Videnin S. A., Chzhan E. A., Yusupova R. R.
PECULIARITIES OF DESIGN SOFTWARE ARCHITECTURE OF ADAPTIVE INFORMATION PROCESSING, MODELING AND CONTROL SYSTEMS
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Romanova D. S.
RESEARCH OF OPTIONS OF TRANSITION FROM UNLIMITED TO LIMITED PARALLELISM ON THE EXAMPLE OF MATRIX MULTIPLICATION
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Shiryaeva T. A., Khlupichev V. A., Shlepkin A. K., Melnikova O. L.
THE USE OF THE INVERSE TRANSFORMATION METHOD FOR TIME SERIES ANALYSIS
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Shiryaeva T. A., Shlepkin A. K., Philippov K. A., Kolmakova Z. A.
ON THE FUNCTION OF TIME DISTRIBUTION OF A COMPLEX COMPUTING SYSTEM UPTIME
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Yareshchenko D. I.
ABOUT NON-PARAMETRIC IDENTIFICATION OF PARTIAL-PARAMETRED DISCRETE-CONTINUOUS PROCESS
PART 2. AVIATION AND SPACECRAFT ENGINEERING
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Akzigitov A. R., Akzigitov R. A., Ogorodnikova U. V., Dmitriev D. V., Andronov A. S.
ANALYSIS OF THE ADS-B AIRSPACE MONITORING SYSTEM
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Begishev A. M., Zhuravlev V. Y., Torgashin А. S.
FEATURES AND MODERNIZATION METHODS OF THRUST MEASUREMENT DEVICES FOR LIQUID ROCKET ENGINE TEST STANDS
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Klyuchnikov A. V.
ELABORATION AND TESTING OF THE ALGORITHM WHICH ENSURES AN ACHIEVEMENT OF MINIMAL DEVIATION ANGLE OF FLYING MODEL’S MAIN CENTROIDAL AXIS OF INERTIA DURING HER COUNTERBALANCING IN A SOLE CORRECTION FLATNESS
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Komlev G. V., Mitrofanova A. S.
TO THE QUESTION OF FORECASTING THE TECHNICAL CONDITION OF LOW-THRUST LIQUID ROCKET ENGINES
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Nepomnyashchiy O. V., Krasnobaev Y. V., Yablonsky A. P., Solopko I. V., Lichargin D. V.
ENSURING EXTREME REGULATION OF POWER OF PRIMARY ENERGY SOURCES AT THEIR JOINT OPERATION FOR TOTAL LOAD
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Filonova M. M.
PROSPECTS FOR THE DEVELOPMENT OF HIGH-VOLTAGE POWER SUPPLY SYSTEMS OF SPACECRAFT WITH A CHARGE-DISCHARGE REGULATOR
PART 3. TECHNOLOGICAL PROCESSES AND MATERIAL SCIENCE