Low friction rotating technique of spacing docking test bed

Zhang Chong-jun, Lai Yinan, Zhang Guangyu, Zhao Xuezeng
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Abstract

Discusses a two-axis rotating technique using two 5-degrees of freedom (DOF) ground-based docking test beds developed to simulate the dynamics of spacecraft. The friction torque of each DOF should be as small as possible in order to simulate the dynamic characteristics of spacecraft under gravity. Since the mass of the two 5-DOF test beds are 2 tons and 8 tons, a new low fiction and bending resistant structure in pitching and rolling simulation has been designed. The main "bending resistant part" is optimized by an improved fuzzy finite element method. According to the target mass and inertia of the system and deformation, the finite element method with fuzzy constraints is used to optimize the structure of the test bed. The optimization result is remarkable and the mass is obviously reduced. The simulating equipment is designed to verify the relevant parameters according to the dynamic similar theory. Tests show that the maximal bearing friction torque of the passive space docking test bed is 1.97 N m which is small in relation to the 80 N m torque produced by spacecraft in space with the biggest error of 9.3 percent.
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空间对接试验台低摩擦旋转技术
讨论了利用两个5自由度地面对接试验台模拟航天器动力学的两轴旋转技术。为了模拟重力作用下航天器的动态特性,各自由度的摩擦力矩应尽量小。针对两架五自由度试验台的质量分别为2吨和8吨的特点,设计了一种新型的低碰撞、抗弯曲的俯仰和滚转仿真结构。采用改进的模糊有限元法对主要的“抗弯部件”进行了优化。根据系统的目标质量、惯量和变形情况,采用模糊约束的有限元法对试验台结构进行优化。优化效果显著,质量明显降低。根据动态相似理论设计了仿真设备,对相关参数进行了验证。试验结果表明,被动式空间对接试验台的最大轴承摩擦力矩为1.97 N m,与航天器在空间中产生的80 N m扭矩相比较小,最大误差为9.3%。
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