Achieving spacecraft rapid rotation using minimally redundant coplanar gyrodyne system
|1Yefymenko, MV, 2Lutsenko, HV, 2Paromova, TO |
1«Hartron-UKOM» scientific manufacturing company, Limited Liability Company, Zaporizhia, Ukraine
2National Technical University, Zaporizhia, Ukraine
|Kosm. nauka tehnol. 2015, 21 ;(5):48–56|
|Publication Language: Russian|
The subject of this article is to consider a minimally redundant coplanar gyrodyne structure for the spatial reorientation of the spacecraft. The proposed orientation algorithm provides a required reorientation of the spacecraft and optimal gyrodyne configuration. The results of the computer modeling of proposed algorithm are shown.
|Keywords: attitude control, gyrodyne, spacecraft|
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