THE EFFECT OF THE AERODYNAMIC MOMENT INSTABILITY ON THE SPACECRAFT MOTION IN THE GRAVITATIONAL-STABILIZATION MODE |
| 4 | |
| 2011 |
| scientific article | 629.78 | ||
| 225-227 |
| The motion of a gravity-stabilized spacecraft relative to the centre of the mass at the height of 550?750 km under the action of variable aerodynamic moment is considered. The variability of the moment is conditioned by atmospheric density changes in the orbit, dependence of the aerodynamic moment on the spacecraft orientation relative to the incident flow, and rotation of the atmosphere. |
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