C2 柔軟付属物とスロッシングを考慮に入れた衛星のダイナミックスの定式化
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概要
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Spacecraft attitude dynamics equations with the structural modes and liquid sloshing are derived. The effect of the flexible structural vibration modes are converted into coupling vectors and the liquid motion in a tank is modeled as a mass-spring-disk model. Then, they are coupled to the rigid-body attitude dynamics of spacecraft.
- 2007-01-26