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STRUCTURAL DESIGN OF A LARGE DEFORMABLE PRIMARY MIRROR FOR A SPACE TELESCOPE.

机译:空间望远镜的大型可变形主镜的结构设计。

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摘要

A 4-meter aperture deformable primary mirror is designed with the mirror and its supports integrated into a single structure. The 2 cm thick, solid ULE mirror is supported by a high modulus graphite epoxy truss structure. The integrated active mirror system is extremely light-weight, making it desirable for a space telescope, as well as for terrestrial applications. Utilizing displacement actuators, the active controls at the mirror's surface include position control and slope control in both the radial and tangential directions at each of the 40 actuator points. Influence functions for each of the controls are nearly independent, reducing the complexity of the control system. Experiments with breadboard models verify the structural concept and the techniques used in the finite element method of computer structural analysis for a system incorporating a solid mirror. The mechanical design of the servo-mechanisms and the flexures to connect the structural members is provided.; The majority of this paper describes the finite element analysis results for the 4-m system with the solid mirror. However, techniques for modeling a lightweight plate with a sandwich core are compared to analytical results, and selected results are included for a lightweight mirror system. Influence functions for various methods of position and slope control are generated with a simplified model to determine the optimum methods of actuation. To evaluate the diffraction limited performance of the 4-m design the complete model is loaded by gravity, a thermal gradient through the mirror thickness, and a uniform thermal soak. Loads are also applied to defocus the mirror and to cause fourth-order astigmatism. Mirror scallop, instigated by the focus shift, has been virtually eliminated with the 40-actuator design. Stresses throughout the system have adequate safety margins for all loads. The structural concept is so effective that it should be considered for uncontrolled primary mirrors as well as active mirrors. Topics for continuing research provide methods of improving both system performance and analysis methods.
机译:设计了一个4米孔径可变形主镜,该镜及其支架集成在一个结构中。 2厘米厚的实心ULE镜子由高模量石墨环氧桁架结构支撑。集成的主动反射镜系统非常轻巧,因此非常适合太空望远镜以及地面应用。利用位移执行器,在镜子表面的主动控制包括在40个执行器点中的每一个的径向和切线方向上的位置控制和倾斜控制。每个控件的影响功能几乎是独立的,从而降低了控制系统的复杂性。面包板模型的实验验证了包含实体镜的系统的结构概念和计算机结构分析的有限元方法中使用的技术。提供了伺服机构的机械设计和连接结构构件的挠曲。本文的大部分内容描述了带有固体镜的4-m系统的有限元分析结果。但是,将具有夹芯的轻质板建模的技术与分析结果进行了比较,并包括了轻质镜系统的选定结果。用简化的模型生成各种位置和坡度控制方法的影响函数,以确定最佳的致动方法。为了评估4-m设计的衍射极限性能,通过重力,通过反射镜厚度的热梯度以及均匀的均热来加载整个模型。还施加负载以使镜子散焦并引起四阶像散。 40致动器设计实际上消除了因焦点偏移而引起的镜扇贝。整个系统的应力对于所有负载都有足够的安全裕度。该结构概念是如此有效,以至于对于不受控制的主镜和主动镜都应考虑使用它。持续研究的主题提供了改善系统性能和分析方法的方法。

著录项

  • 作者单位

    The University of Arizona.;

  • 授予单位 The University of Arizona.;
  • 学科 Physics Optics.
  • 学位 Ph.D.
  • 年度 1981
  • 页码 183 p.
  • 总页数 183
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 光学;
  • 关键词

  • 入库时间 2022-08-17 11:51:32

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