The analysis of the influence of design and ballistic parameters nanosatellite on the angular motion during the descent from low circular orbits
Автор: Glukhova Liya, Timbay Ivan
Журнал: Известия Самарского научного центра Российской академии наук @izvestiya-ssc
Рубрика: Механика и машиностроение
Статья в выпуске: 6-1 т.14, 2012 года.
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The planar motion of an uncontrolled nanosatellite around its center of mass under the influence of the gravitational moment and the restoring aerodynamic moment during the descent from low circular orbits is considered. The influence of design and ballistic parameters (initial conditions of angular motion, margin of static stability, ratio of moments of inertia) on the angular motion nanosatellite (rotation, oscillations) is investigated.
Nanosatellite, motion of the center of mass, gravitational moment, aerodynamic moment, aerodynamic features, design and ballistic parameters
Короткий адрес: https://sciup.org/148201630
IDR: 148201630
