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ANALYSIS OF LED-BASED SOLAR SIMULATOR DEVELOPMENT CAPABILITY FOR SPACECRAFT GROUND TESTING APPLICATIONS
Dvirniy G., Shevchuk A., Dvirniy V., Elfimova M., Krushenko G.
STRESS ANALYSIS OF SOLAR ARRAY DRIVER MECHANISM ACTUATOR OF THE SPACECRAFT “LUNA-RESURS-1”
Tambasova E., Tokarev A., Pavelko S., Таmbаsоv I.
STUDENT PICOSATELLITE PLATFORM SIBQUBE: DEVELOPMENT OF PROTOTYPE STRUCTURE OF POCKETQUB CLASS PICOSATELLITE
Kravchunovsky A., Draganyuk M., Zuev D., Skorobogatov S., Movchan P.
AUTOMATED SIMULATION SYSTEM OF ELECTRICAL CHARACTERISTICS OF SPACECRAFT POWER SYSTEM
Mizrah E., Poymanov D., Balakirev R., Tkachev S.
UNTIGHTENED PLATFORM OF SPACE VEHICLE FOR REMOTESOUNDING OFTHE EARTH
Shangina E., Rybakov A., Pasechnik K., Zaytsev P., Vlasov A., Shangina E., Ribakov А., Pasechnik К., Zaytsev P., Vlasov A.
GEOSTATIONARY SPACECRAFT ATTITUDE AND ORBIT CONTROL BY MOTIONLESS ORBIT CONTROL THRUSTERS
Yermoshkin Y., Raevsky V., Urusov V.
BUNDLED SOFTWARE TO COMPUTE TEMPERATURE FIELDS OF SPACE VEHICLES PANELS WITH LEAKY CONSTRUCTION
Vasiljev E., Derevyanko V.
DISTRIBUTED PARAMETERS ENERGY-HEAT MODEL OF SPACE NICKEL-HYDROGEN STORAGE BATTERY
Sakhnov M., Lelekov A., Galochkin S., Sahnov M., Lelekov A., Galochkin S.
PLATFORM OF AUTOMATION OF COMPONENT WEIGHT COMPENSATION SYSTEM FOR LARGE SPACECRAFT REFLECTOR
Kovalev I., Badanina J.
Designing and constructing of the program-mathematical model for the spacecraft command and measuring system
Nozhenkova L., Isaeva O., Gruzenko E.
RESULTS OF 347K STATIC SUN SENSOR LABORATORY TESTING
Pirogov M., Varlamov V., Tsymbal G., Strizhova N., Demeshko S., Galchinskiy D., Safronov K., Polkunov B., Gebgart A.
DESIGN OF A LOW THRAST PROPULSION SYSTEM AND THE TRAJECTORIES OF SPASECRAFT TO THE CENTRE OF THE SOLAR SYSTEM
Platov I., Simonov A.
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., Semenov V., Kabirov V., Sukhorukov M., Torgaeva D.
THE ALGORITHM FOR ESTIMATING ANGULAR RATE OF SPACECRAFT IN SURVIVABILITY MODE
Latyntsev S., Meus S., Оvсhinniкоv А.
AUTOMATED WEIGHT COMPENSATION SYSTEM FOR GROUND-BASED TRYOUT OF SPACE VEHICLE SOLAR PANELS
Verhoglyad A., Kuklin V., Makarov S., Mihalkin V., Halimanovich V.
SOFTWARE SUPPORT FOR TESTING COMMAND RECEPTION AND TRANSMISSION AND TELEMETRY ANALYSIS IN THE COMMAND-AND-MEASURING SYSTEM
Nozhenkova L., Isaeva O., Vogorovskiy R., Gruzenko E.
AN ELECTROMECHANICAL EXECUTIVE BODY BASED ON THE CONTACTLESS DIRECT CURRENT MOTOR WITH A WINDING PRINTING DISK STATOR FOR SMALL SPACECRAFTS
Balandina T., Balandin E.
SOLAR BATTERIES EXPERIMENTALUNIT WITH CONCENTRATOR:IDEA, CONSTRUCTION, METHODOLOGY OF FLIGHT TESTS
Mel'nikov P., Kudryashov V., Kuzoro V., Shangina E., Melnikov P., Kudryashov V., Kuzoro V., Shangina E.
The problems of telemetric data processingin the loop of spacecrafts computer-aided control system
Pakman D., Nekrasov M., Antamoshkin A.
TECHNIQUE FOR CALCULATION AND SELECTION OF SPACECRAFT ELECTRIC HEATERS PARAMETERS UNDER UNCERTAINTY CONDITIONS
Chebotarev V., Zvonar V., Fatkulin R., Dmitriev G.
MA THEMA TICHAL PROVIDING OF THE PLANNING METHODOF SUPERVISORY EQUIPMENT SYSTEM PREP ARA TION FOR ELECTRONICAND RADIOTESTING OF SPACECRAFTS
Voronkovich V., Iosifov P.
ADVANCED UNIFIED MICRO SERIES PLATFORMS
Zimin I., Valov M., Yakovlev A.
“SibCube” - CubeSAT satellite project of SibSAU student
Zuev D., Pyatkov A., Movchan P., Smirnov D., Kostyukov A.
ORGANIZATION THROUGH CHANNEL TELEVISION SPACE BRIDGES WITH USAGE OF MULTIFUNCTIONAL SPACE SYSTEM RELAYING “LUCH”
Gromov K., Vigonskiy U., Roskin C., Kuzovnikov A., Muhin V.
RESULTS AND PROSPECTS OF JOINT HEAT PHYSICAL RESEARCHES OF ICM OF THE SB RAS AND JSC “ACADEMICIAN M.F. RESHETNEV “INFORMATION SATELLITE SYSTEMS”
Shaidurov V., Derevyanko V., Vasilyev E., Kosenko V., Zvonar V., Chebotarev V.
ORGANIZATION OF COMPLEX TESTING OF THE SPACECRAFT COMMAND AND MEASURING SYSTEM
Nozhenkova L., Isaeva O., Koldyrev A.
THE ANALYSIS OF THE IMPACT OF THE METHOD OF FASTENING ON STRAIN-STRESS BEHAVIOR OF COMPOSITE OVERWRAPPED PRESSURE VESSEL
Mironenko E., Miheev A.
SYSTEM APPROACH OF SELECTION TO PURPOSE DESIGNED EQUIPMENT OF SMALL SPACECRAFT
Kaloshin I., Kharlamov A., Skripachev V., Surovceva I., Ivanov V.
APPLICATION OF THE METHOD OF LOAD TESTING WITH GROUND experimental METHOD of CONTROL UNITS OF antenna GUIDANCE system
Kudryashova G., Babanov D., Galimzyanov A.
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