ANALYZING THE EFFECT OF CONFIGURATION PARAMETERS ON THE STABILITY OF LAUNCH VEHICLES |
4 | |
2011 |
scientific article | 532.5.013.4 | ||
248-250 |
A technique for analyzing the stability of launch vehicles analysis is proposed to determine stability thresholds in space of the configuration parameters of a rocket, characterizing the position of tanks with a liquid. The analysis takes into account the effect of these parameters on mass-inertial and dynamic characteristics. Also, the effect of some other key parameters of liquid sloshing and control system on the stability thresholds of a closed-loop system is examined. |
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