Closed-loop mechanism of 3-DOF 三自由度闭环机构
Closed loop configuration (CCL) is commonly used as a synchronous deploying control mechanism of appendages.
绳索联动机构（CCL）是航天器上最常用的附件同步展开控制机构。
The mechanism of dynamic instability of rolling missile was analyzed by describing the dynamics of rolling missile as a closed loop with dynamic negative feedback.
将滚转导弹动力学系统描述为一个具有动态负反馈的闭环系统，分析了滚转导弹动态失稳的机理。
One is for the dynamics of the mechanism for a reference body with rotation, and the other is for the dynamics of a system with closed loop structure.
最后给出了两个分别是参考体具有转动及非树机构动力学分析算例。
应用推荐