The dynamics of the spacecraft with gyro-gravity stabilization in the deployment of a flexible ring antenna

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. 2011, 17 ;(5):03-18
https://doi.org/10.15407/knit2011.05.003
Publication Language: Russian
Abstract: 
We constructed a generalized mathematical model and performed a numerical simulation of the dynamics of a stabilized spacecraft which carries a body of changeable geometry. This model describes the deployment of a compact body into a flexible ring antenna.
Keywords: gyro-gravity stabilization, numerical simulation of the dynamics, spacecraft
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