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Backgrounds and trends of all-electric propulsion geostationary satellites creation
Vnukov A.A., Rvacheva E.I.
ANALYSIS OF THE DYNAMIC PERFORMANCE OF THE POINTING AND ATTITUDE CONTROL SUBSYSTEM OF THE RESILIENT SPACECRAFT WITH POWER GYROSCOPIC UNIT ON THE BASIS OF ГД 02-150 GYRODYNE
Yakimov E.N., Raevskiy V.A., Lukyanenko M.V.
THE ALGORITHM FOR ESTIMATING ANGULAR RATE OF SPACECRAFT IN SURVIVABILITY MODE
Latyntsev S.V., Meus S.V., Оvсhinniкоv А.V.
Technical system simulation with Python
Lelekov A.T.
Dynamical workbench for signature analysis and operating conditions of flywheel engine group of pointing and attitude control systems of spacecrafts
Synitskiy D.E., Murygin A.V.
Testing of spacecraft orientation and stabilization systems sing starry sky simulators
Gorelko M.G., Murygin A.V.
MATHEMATICAL MODEL FOR GEOSTATIONARY SPACECRAFT DISTURBING TORQUES DETERMINATION
Latyntsev S.V., Murygin A.V.
“SibCube” - CubeSAT satellite project of SibSAU student
Zuev D.M., Pyatkov A.G., Movchan P.V., Smirnov D.V., Kostyukov A.S.
Using the principle of gravitational stabilization and orientation in the design of small spacecraft
Еsina P.A., Kornev V.M.
The prospects for improving the performance of Electromechanical Executive body of the spacecraft
Kholodilov S.V.
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