The paper presents a practical method for satellite inertial sensor assembly consisted of single-degree-of-freedom rate integrating gyros.
介绍了一种用单自由度速率积分陀螺组成的卫星用惯性敏感器陀螺漂移系数测试的实用方法。
Determined by calculating the parameters of the state assembly and freedom of the arc springs and free high curvature.
通过计算出的参数确定总成和自由状态下板弹簧的弧高和自由曲率。
Then, the method of building the assembly model, recognizing mating constraint type based engineering knowledge, the algorithm of inferring relative freedom of mating feature are given.
并给出装配模型的建立过程及基于工程知识的装配配合约束类型识别方法、配合特征相对自由度推理算法。
An assembly feature matrix was established, the elements of which denote the degree of freedom (DOF) of assembly features of a part in its reference frame.
通过建立产品的装配特征矩阵，确定了装配零、部件在各个方向的自由度。
Oblong shape assembly mark:The shape of the most universal cabaret banquet hall, the table bit pendulum puts degree of freedom higher -, the main time of the guest distinguish non constat.
长方形会场：最普遍的酒店宴会厅的形状，桌位摆放自由度吧高，宾客的主次分别不明显。 。
Oblong shape assembly mark:The shape of the most universal cabaret banquet hall, the table bit pendulum puts degree of freedom higher -, the main time of the guest distinguish non constat.
长方形会场：最普遍的酒店宴会厅的形状，桌位摆放自由度吧高，宾客的主次分别不明显。 。
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