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UPGRADING OF PHOTOVOLTAICARRAY SIMULATORWITH TWO-CIRCUIT CONTROL ELEMENT
Tkachev S.B., Mizrakh E.A., Tkachev S.B., Mizrakh E.A.
TOP-DOWN APPROACH FOR SPACECRAFT DEVELOPMENT
Lihachev M.V.
Designing and constructing of the program-mathematical model for the spacecraft command and measuring system
Nozhenkova L.F., Isaeva O.S., Gruzenko E.A.
The research of effective thermal conductivity coefficient effect on the temperature field of reflector
Burova O.V., Romankov E.V., Tsivilev I.N., Minakov A.V.
SEPARATION DEVICE FOR SPACECRAFT UNPRESSURIZED PLATFORMS BASED ON ISOGRID STRUCTURES
Vehov A.S.
PROGRAM COMPLEX FOR MODELING OF STABILIZED MOTION OF SPACECRAFT WITH TRANSFORMABLE FLEXIBLE PARTS
Ignatyev M.G., Kopylov V.M., Kulakov A.J., Sotnikov M.V.
MATHEMATICAL MODEL FOR GEOSTATIONARY SPACECRAFT DISTURBING TORQUES DETERMINATION
Latyntsev S.V., Murygin A.V.
TWO-DIMENSIONAL THERMAL MODEL OF THE THERMAL CONTROL SYSTEM FOR NONHERMETIC FORMATION SPACECRAFT
Tanasienko F.V., Shevchenko Y.N., Delkov A.V., Kishkin A.A.
SOFTWARE SUPPORT FOR TESTING of large spacecraft REFLECTOR AND EVALUATION OF THE OPERATION PARAMETERS OF COMPONENT WEIGHT COMPENSATION SYSTEM
Kovalev I.V., Badanina J.O.
DOUBLE-CONIC ADAPTER FOR LAUNCHING THE BLOCK OF THREE SPACECRAFTS
Khakhlenkova A.A.
FREQUENCY ANALYSIS OF THE LONGITUDINAL AND TRANSVERSE VIBRATIONS OF LATTICE CYLINDRICAL SHELL WITH OPENINGS
Shatov A.V., Khakhlenkova A.A.
REDUCTION OF SPACECRAFT HARNESS MASS
Dvirnyi V.V., Eremenko N.V., Dvirnyi G.V.
Implementation error of relative measurements
Garin E.N.
THE INFLUENCE OF CONDITIONS FOR PASSING GLONASS AND GPS SATELLITE RADIO NAVIGATION SIGNALS ON THE ERRORS OF DEFINING RELATIVE COORDINATES
Garin E.N.
PLATFORM OF AUTOMATION OF COMPONENT WEIGHT COMPENSATION SYSTEM FOR LARGE SPACECRAFT REFLECTOR
Kovalev I.V., Badanina J.O.
Review of technical solutions for developing of a control and data handling as a system on a chip for ultra small spacecraft
Khanov V.K., Borodina T.V., Antamoshkin A.N.
SOME RESULTS OF “PLASMA-PROGRESS” AND “RADAR-PROGRESS” ACTIVE SPACE EXPERIMENTS
Khakhinov V.V., Potekhin A.P., Lebedev V.P., Kushnarev D.S., Alsatkin S.S.
DEPLOYMENT DYNAMICS MATHEMATICAL MODELS USED FOR THE OVERSIZED TRANSFORMABLE MECHANICAL SYSTEMS DURING ON-GROUND COMPLEX FUNCTIONAL TESTS
Romanenko I.V., Dvirnyy V.V., Kuklin V.A., Perminov M.D.
SIMULATION MODELING OF THE MAIN COMPONENTS OF MOTION CONTROL SYSTEM OF THE SATELLITE
Yelubayev S.A., Jamalov N.K., Alipbayev K.A., Sukhenko A.S., Bopeyev T.M.
METHOD FOR CALCULATING THE ENERGY CHARACTERISTICS AND SOLAR BATTERY PARAMETERS OF HIGH-VOLTAGE POWER SUPPLY SYSTEMS
Chernaya M.M.
VERIFICATION OF FINITE-ELEMENT MODEL SPACECRAFT VIA TEST RESULTS
Balyakov D.F.
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.
LATTICE CYLINDRICAL SHELL WITH A ROUND TRANSVERSE PROFILE AND VARIABLE STIFFNESS
Khakhlenkova A.A.
GEOMETRICAL AND FINITE-ELEMENT MODELING OF LATTICE CONICAL SHELL WITH GEODESIC PATH OF SPIRAL RIBS
Khakhlenkova A.A., Shatov A.V.
The main provisions of the methodology for ensuring the resistance of the onboard equipment of spacecraft to the effects of the radiation effects of outer space
Maximov I.A., Kochura S.G., Avdyushkin S.A.
TECHNIQUE FOR CALCULATION AND SELECTION OF SPACECRAFT ELECTRIC HEATERS PARAMETERS UNDER UNCERTAINTY CONDITIONS
Chebotarev V.E., Zvonar V.D., Fatkulin R.F., Dmitriev G.B.
COMBINED METHOD OF GONETS-M SPACECRAFT CONTROL MUL TIVERSION SOFTW ARE DESIGN
Antamoshkin O.
ADVANCED UNIFIED MICRO SERIES PLATFORMS
Zimin I.I., Valov M.V., Yakovlev A.V.
Comparison of direct and reverse cycle of the thermal control system for the non-hermetic spacecrafts
Delkov A.V., Hodenkov A.A., Shevchenko Y.N.
INVESTIGATION OF THE SPACE VEHICLES COATINGS FEATURES
Miheev A.E., Girn A.V., Ivasev S.S., Evkin I.V.
SATELLITE MASS CRITERIA OPTIMIZATION WITH THE USE OF CAD “ACAB”
Kochev Y.V., Efremov S.V., Ovchinnikov A.V.
PROCEDURE FOR EVALUATING THE EFFECTIVE USE RANGE OF THE UNIFIED SPACE PLATFORMS
Chebotarev V.E., Zimin I.I.
ANALYSIS OF LED-BASED SOLAR SIMULATOR DEVELOPMENT CAPABILITY FOR SPACECRAFT GROUND TESTING APPLICATIONS
Dvirniy G.V., Shevchuk A.A., Dvirniy V.V., Elfimova M.V., Krushenko G.G.
THE ALGORITHM FOR ESTIMATING ANGULAR RATE OF SPACECRAFT IN SURVIVABILITY MODE
Latyntsev S.V., Meus S.V., Оvсhinniкоv А.V.
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.
DEVELOPMENT OF THE PROPULSION CONSTRUCTION AND THE TRAJECTORY FOR THE SPACECRAFTS OF THE “LAPLACE-L” MISSION FOR THE STUDY OF THE JUPITER PLANETARY SYSTEM
Platov I.V., Simonov A.V.
THERMAL STORAGE TO THE TEMPERATURE CONTROL SYSTEM OF POWERFUL BLOCKS OF ELECTRONIC EQUIPMENT WITH A SHORT ACTION TIME
Vasil’ev E.N., Derevyanko V.A., Chebotarev V.E.
CREATION OF THE FUEL SILPHON TANKS MECHANICAL TEST MODES
Yermoshkin Y.M., Orlov S.A., Usanov A.Y.
The problems of the transform antennas manufacture and development
Dvirny G.V.
About domestic system of space monitoring of emergencies
Testoedov N.A., Dvirnyj V.V., Nosenkov A.A., Elfimova M.V.
ELECTRONIC EQUIPMENT OF SPACECRAFT AND THERMOANALYSIS OF PRINTED-CIRCUIT -BOARDS
Yutkin A.V., Klimkin O.A., Dzyuvina A.
TESTING ELECTRONIC PARTS FROM FLIGHT LOTS ON DOSE EFFECTS FOR THE HARDNESS GUARANTEE OF SPACECRAFT ONBOARD EQUIPMENT
Zykov V.M., Maximov Y.V., Maximov I.A., Kochura S.G., Ivanov V.V., Patskov A.V.
Dynamics forecasting for electrical characteristics of spacecraft solar arrays by means of computational intelligence
Semenkina M.E., Semenkin E.S., Ryzhikov I.S.
PROPULSION OF A SPACECRAFT WITH THE ROTATING BATTERIES
Nadaraia C.G., Chestakov I.Y., Fadejev A.A., Nadaraia K.V.
Estimation of the form of a large-sized transformed reflector surface for a spacecraft
Goldobin N.N.
DESIGN OF A LOW THRAST PROPULSION SYSTEM AND THE TRAJECTORIES OF SPASECRAFT TO THE CENTRE OF THE SOLAR SYSTEM
Platov I.V., Simonov A.V.
THE METHOD OF SYNTHESIS OF THE DIGITAL CONTROLLER FOR A SOLAR ENERGY CONVERSION CHANNEL OF THE SOLAR BATTERY IN THE POWER SUPPLY SYSTEM OF A SPACECRAFT
Shkolnyi V.N., Semenov V.D., Kabirov V.A., Sukhorukov M.P., Torgaeva D.S.
SYSTEM APPROACH OF SELECTION TO PURPOSE DESIGNED EQUIPMENT OF SMALL SPACECRAFT
Kaloshin I.B., Kharlamov A.G., Skripachev V.O., Surovceva I.V., Ivanov V.K.
ANALYSIS OF CLEANING CONCEPTS OF NEAR-EARTH SPACE
Kirillov V.A., Bagateev I.R., Tarleckiy I.S., Balandina T.N., Balandin E.A.
INVESTIGATION OF CHARACTERISTICS OF ELECTRIC FIELD ARISING FROM ELECTROSTATIC DISCHARGE
Tikhomirov R.E., Maximov I.A., Trofimchuk D.A., Ivanov V.V., Maslov E.P.
Thermo-mechanical behavior of FORM-BUILDING EQUIPMENT FROM composite MATERIAL for reflector OF spacecraft antenna
Berdnikova N.A., Belov O.A., Babkin A.V., Belov D.A.
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