Expanding the flexible long element aboard spacecraft with the magnetic damper

1Zakrzhevskii, AE, 2Khoroshylov, VS
1S.P. Timoshenko Institute of Mechanics of the National Academy of Sciences of Ukraine, Kyiv, Ukraine
2Yangel Yuzhnoye State Design Office, Dnipropetrovsk, Ukraine
Kosm. nauka tehnol. 2014, 20 ;(1):28-43
Section: Space-Rocket Vehicles
Publication Language: Russian

A generalized mathematical model is derived and numerical simulation is carried out for studying the dynamics of the spacecraft with the passive stabilization system that contains the compact structure of changeable configuration, which is deploying under a prescribed program into the flexible gravitational stabilizer with the magnetic damper at its end.

Keywords: dynamics of the spacecraft, the passive stabilization system

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