Dynamics of a deformed space system of bodies with programmed change of the configuration
Heading:
| 1Dranovsky, VI, 2Zakrzhevskii, AE, 3Khoroshylov, VS 1Yangel Yuzhnoye State Design Office, Dnipropetrovsk, Ukraine 2S.P. Timoshenko Institute of Mechanics of the National Academy of Sciences of Ukraine, Kyiv, Ukraine 3Yangel Yuzhnoye State Design Office, Dnipro, Ukraine |
| Kosm. nauka tehnol. 2004, 10 ;(1):045-053 |
| https://doi.org/10.15407/knit2004.01.045 |
| Publication Language: Russian |
Abstract: A generalized mathematical model is developed and computer simulation is performed for the dynamics of a spacecraft carrying an elastic body of variable geometry caused by programmed deployment of compact system in lengthened elastic element like antenna or gravitational stabilizator boom.
|
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, Transl. from Eng., 292 p. (Mir, Moscow, 1980) [in Russian].
4. Lurie A. I. Analytical Mechanics, 824 p. (Fizmatgiz, Moscow, 1961) [in Russian].