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Overview: With the increasing requirements for the sensitivity, resolution and angle of view of space telescopes, the aperture of space mirror are getting bigger and bigger, which greatly increases the difficulty of mirror fabrication support. For the space mirror in the in-situ fabrication and testing, besides the influence of other factors such as temperature, the self-weight deformation has a great influence on mirror surface figure. And the larger the aperture and the higher the precision, the more difficult the support is. The self-weight deformation is mainly affected by factors such as the number of support points, the position of the support points and the stiffness of the support unit. Passive hydraulic support units (PHSUs) are frequently used in the in-situ fabrication and testing. However, some studies have found that the number of supporting units of large-aperture mirrors is too large, resulting in a large difference in the stiffness of each group of hydraulic support units, and has a great influence on mirror surface figure. It has become a hidden danger affecting the accuracy of in-situ fabrication and testing. In order to reduce the number of supporting units and increase the accuracy of the supporting surface, the joint optimization method of layout, stiffness and active correction is studied. Firstly, for the difference of PHUS' stiffness, a hierarchical layout optimization method for support stiffness and support position is proposed to obtain the initial optimization solution of the support system. Then, the mode calibration method and the least square method is used for active correction of support system to obtain the final optimized solution of the mirror surface figure. Finally, the effectiveness of the method is verified by a numerical simulation experiment with specific cases. The results show that, for 4 m thin meniscus mirror, after layout optimization, with the hydraulic passive support system, the root mean square (RMS) of the mirror surface errors of 60 point axial support system is reduced from 150.6 nm to 32.9 nm, and the RMS value of the mirror surface errors of 78 point axial support system is reduced from 45.2 nm to 22.6 nm. The optimization effect is remarkable. After active correction, the RMS value of the mirror surface errors of 60 point axial support system is 14.6 nm, and it is 6.9 nm for 78 point axial support system. The requirement of the RMS value of the mirror surface error is less than λ/40 (λ=632.8 nm). The support systems meet the requirement. Finally, the 60 point axial support system was selected. Through the joint optimization of layout, stiffness and active correction for supporting points, it can greatly increase the applicability, flexibility and reduce the difficulty of implementation for the in-situ support system.
Optimization flow for support system
Schematic diagram of axial layout of two schemes.
The first twenty vibration modes of the mirror
Mirror deformations after active corrections.