In this paper, we discuss the optimal control problem for an elastic oscillating system of fine-long cube flying object with structure damping coefficient.
本文讨论具结构阻尼系数的细长体飞行器的弹性振动方程支配系统的最优控制问题。
With the finite element analysis techniques the finite element model of the flat-panel is attained, and the model of the main structure of the damping system is built.
利用有限元分析技术得到了平板有限元模型，继而建立了减振系统的主结构模型。
应用推荐