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10 May 2019 Design of motion equations for dynamic support structure of space-on-orbit segmentation mirror
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Proceedings Volume 11068, Second Symposium on Novel Technology of X-Ray Imaging; 110681B (2019) https://doi.org/10.1117/12.2524443
Event: Second Symposium on Novel Technology of X-Ray Imaging, 2018, Hefei, China
Abstract
In order to realize the on-orbit expansion of the space segmentation mirror and the fine adjustment of the mirror surface, a dynamic support mechanism is designed. And its adjustment mechanism is analyzed. Firstly, the dynamic support mechanism is designed and modeled. Then, the inverse calculation of the support mechanism pose is analyzed. Finally, a finite element analysis of the established model is carried out, and compared with the experimental results. The results show that the space segmentation mirror has the ability to be assembled into a large-caliber telescope on orbit and to ensure image quality.
© (2019) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Dapeng Wang, Zong Chen, Yun Wang, and Ruimin Fu "Design of motion equations for dynamic support structure of space-on-orbit segmentation mirror", Proc. SPIE 11068, Second Symposium on Novel Technology of X-Ray Imaging, 110681B (10 May 2019); https://doi.org/10.1117/12.2524443
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