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6-PSS Precision Positioning Stewart Platform for the Space Telescope Adjustment Mechanism

机译:用于太空望远镜调节机构的6-PSS精确定位Stewart平台

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In this paper, the mechanical design, precision control, optimal calibration and experiment of a 6-PSS Stewart adjusting mechanism for space telescope secondary mirror adjustment mechanism is introduced. The modal analysis, static analysis, inverse kinematics modeling and accuracy analysis were performed on the basis of the mechanical design. According to the identification model acquired from the white noise input, the robust controller based on mixed sensitivity is designed for a better robust performance to the model uncertainty and disturbance, and the better disturbance rejection and dynamic characteristics are all verified by the simulation and experiment results. Then, the SMCS optimal method improved by correcting the step size and preventing the crossing of the boundary is applied to the calibration of the Stewart mechanism model. Finally, the effectiveness of the analysis, design and algorithm are all verified by calibration experiments. The results of the system performance test showed that the secondary mirror adjustment system has fine absolute and repeatability positioning accuracy of a single axis, and the system may achieve higher positioning accuracy by decoupling. The precision positioning requirement of Space telescope active optics could be satisfied.
机译:介绍了6-PSS Stewart空间望远镜副镜调节机构的机械设计,精度控制,最佳标定和实验。在机械设计的基础上进行了模态分析,静态分析,逆运动学建模和精度分析。根据从白噪声输入获得的识别模型,设计了一种基于混合灵敏度的鲁棒控制器,以提高对模型不确定性和扰动的鲁棒性能,并通过仿真和实验结果验证了较好的扰动抑制和动态特性。 。然后,将通过校正步长和防止边界交叉而改进的SMCS最优方法应用于Stewart机构模型的校准。最后,通过校准实验验证了分析,设计和算法的有效性。系统性能测试的结果表明,辅助镜调节系统具有良好的单轴绝对和重复精度定位精度,并且该系统可以通过解耦获得更高的定位精度。可以满足太空望远镜有源光学系统的精确定位要求。

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