The dynamics of deployment of the ring antennae on the spacecraft without stabilization

1Zakrzhevskii, AE, 1Tkachenko, VF, 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. 2009, 15 ;(6):57-66
https://doi.org/10.15407/knit2009.06.057
Publication Language: Russian
Abstract: 
There are carried out a construction of a generalized mathematical model and a numerical modelling of the dynamics of a spacecraft with a carried body of changeable geometry. This model describes a deployment of a compact body in ring antennae.
Keywords: body of changeable geometry, numerical modelling, spacecraft
References: 
1. Beletskii V. V. The motion of an artificial satellite around the center of mass, 416 p.  (Nauka, Moscow, 1965) [in Russian].
2. Branets V. N., Shmyglevskii I. P. Use of Quaternions in the Problems of Orientation of Solid Bodies, 320 p. (Nauka, Moscow, 1973) [in Russian].
3. Wittenburg J. Dynamics of Systems of Rigid Bodies, 292 p. (Mir, Moscow, 1980) [in Russian].
4. Lurie A. I. Analytical Mechanics, 824 p. (Fizmatgiz, Moscow, 1961) [in Russian].
5. Zakrzhevskii A. E. Slewing of flexible spacecraft with minimal relative flexible acceleration. J. Guidance, Control, and Dynamics, 31 (3), 563—570 (2008).