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The Statics and Dynamics Analysis of High-dynamic Flight Simulator Based on Substructure Method

机译:基于子结构方法的高动态飞行模拟器静态和动力学分析

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In this paper, the most serious loads configuration of High-Dynamic Flight Simulator (HDFS) was found firstly by rigid-body dynamics analysis, then level-by-level finite element analyzing based on substructure method for HDFS under the configuration above was carried out, from which we got the statics characteristic of arm/gondola frame/gondola and the dynamics characteristic of the overall structure respectively. Such analysis strategy couples the stiffness matrix and mass matrix of lower-level structures to upper-level structures, and takes the deformation of upper-level as boundary condition for lower lever by displacement coordinate relationship between them, consequently, the accuracy of this strategy is reliable, and the computational efficiency is evidently improved. Analysis results show that the statics and dynamics characteristic of HDFS could be carried out by the level-by-level analyzing strategy effectively and soundly. This kind of analysis strategy is able to extend to other multi-level structures, such as flight simulator, centrifuge, multi-axis turntable et al.
机译:在本文中,首先通过刚体动力学分析找到了高动态飞行模拟器(HDFS)的最严重负载配置,然后基于上述配置下的HDFS的子结构方法进行逐级有限元分析,我们从中获得了ARM / GONDOLA框架/缆车的静态特征和整体结构的动态特征。这种分析策略将刚度矩阵和质量矩阵耦合到上层结构,并通过它们之间的位移坐标关系来实现上层作为较低杠杆的边界条件的变形,因此这种策略的准确性是可靠,并且计算效率明显改善。分析结果表明,HDFS的特征可以通过逐级分析策略有效,妥善地进行HDFS的特征。这种分析策略能够扩展到其他多级结构,例如飞行模拟器,离心机,多轴转盘等。

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