带伸展柔性附件航天器的动力学方程是刚-柔耦合的时变非线性动力学方程,用传统方法求解其动力学响应时会遇到很大的困难。
The dynamic equation of the spacecraft with extensional flexible appendages system is time variable and nonlinear, so it is very difficult to solve this kind of equation with traditional methods.
要想拉出粗细不同的大宽、韭叶、毛细、荞麦棱子,不但要臂力过人,对力道的控制还要刚中带柔。
To pull the dough into noodles of different thickness, a chef needs to have extraordinary strong arms and also exquisite skills in controlling his strength.
研究带中心刚体的作大范围运动的空间曲梁的刚-柔耦合动力学。
In this paper, the coupling dynamics of a Timoshenko beam attached to a central rigid body is investigated.
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