PART 1. INFORMATICS, COMPUTER TECHNOLOGY AND MANAGEMENT
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A. V. Vakhnin*, E. A. Sopov
A NEW METHOD OF GROUPING VARIABLES FOR LARGE-SCALE GLOBAL OPTIMIZATION PROBLEMS
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O. P. Zolotova*, S. I. Burkov
SIMULATION OF METAL LAYERS THICKNESS INFLUENCE ON PHASE VELOCITIES OF ACOUSTIC WAVES IN THE PIEZOELECTRIC PLATES
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M. E. Kornet, A. V. Shishkina*
TO NONPARAMETRIC IDENTIFICATION OF DYNAMIC SYSTEMS UNDER NORMAL OPERATION
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N. V. Kulyasov*, S. V. Isaev
INVESTIGATION OF THE NETWORK ANOMALIES OF THE CORPORATE NETWORK OF KRASNOYARSK SCIENTIFIC CENTER
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G. I. Rastorguev, A. N. Grishanov , А. D. Matveev*
EFFICIENT METHOD OF CALCULATING LAYERED CONICAL SHELLS WITH LAGRANGE MULTIGRID ELEMENTS USE
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V. I. Senashov, D. K. Belov*
MODELING OF THE LAYER STRUCTURE OF INFINTE GROUPS
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S. I. Senashov*, E. V. Filyushina
MODELING OF PLASTIC FLOW BETWEEN RIGID PLATES APPROACHING TO A CONSTANT ACCELERATION
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F. V. Tanasienko*, Y. N. Shevchenko, A. V. Delkov, A. A. Kishkin
TWO-DIMENSIONAL THERMAL MODEL OF THE THERMAL CONTROL SYSTEM FOR NONHERMETIC FORMATION SPACECRAFT
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A. V. Tereshina, D. I. Yareshchenko*
ON NONPARAMETRIC MODELING SPINNING SYSTEMS WITH DELAY
PART 2. AVIATION AND SPACECRAFT ENGINEERING
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A. R. Akzigitov*, N. I. Stacenko, N. S. Pisarev, A. N. Efimova, R. M. Musin
IMPLEMENTATION OF RUSSIAN SATTELITE COMMUNICATION SYSTEM “GONETS” IN AIRCRAFT MONITORING
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E. N. Belayev, A. G. Vorobyev*
INFLUENCE OF FILLING PROCESSES FOR MIXING HEAD OF GAS GENERATORS ON DYNAMICS OF LIQUID ROCKET ENGINE WITHOUT STARTER DEVICE
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D. S. Gerasimova*, A. V. Sayapin, A. A. Palukhin, A. V. Katsura
APPLICATION OF THE BOOTSTRAP METHOD FOR STATISTICAL CHARACTERISTICS ASSESSMENT OF AIRCRAFT COMPONENTS’ SMALL SAMPLES
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Yu. M. Yermoshkin*, D. V. Volkov, E. N. Yakimov
ON THE CONCEPT OF ALL ELECTRIC PROPULSION SPACECRAFT
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I. N. Kartsan, E. A. Shangina*, G. G. Kiselev, S. V. Efremova
INCREASE RELIABILITY OF ULTRAHIGH-FREQUENCY CHANNELS OF THE ACTIVE PHASED ARRAY ANTENNA MODULES
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A. V. Lopatin, M. A. Rutkovskaya*
OPTIMAL CHOICE OF DESIGN PARAMETERS OF THE UMBRELLA-TYPE ANTENNA SPOKE TO REACH MAXIMAL BENDING STIFFNESS
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L. F. Nozhenkova, O. S. Isaeva, A. Yu. Koldyrev*
ORGANIZATION OF COMPLEX TESTING OF THE SPACECRAFT COMMAND AND MEASURING SYSTEM
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I. V. Platov*, A. V. Simonov
DESIGN OF A LOW THRAST PROPULSION SYSTEM AND THE TRAJECTORIES OF SPASECRAFT TO THE CENTRE OF THE SOLAR SYSTEM
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A. S. Satyshev*, Yu. N. Bezborodov, V. A. Ganzha
MEASURING CONVERTER OF LABORATORY STAND FOR TESTING WORKING BODIES OF SPECIAL MACHINES OF AERODROM-TECHNICAL SUPPORT
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V. E. Chebotarev, I. I. Zimin*
PROCEDURE FOR EVALUATING THE EFFECTIVE USE RANGE OF THE UNIFIED SPACE PLATFORMS
PART 3. TECHNOLOGICAL PROCESSES AND MATERIAL SCIENCE