CORC

浏览/检索结果: 共10条,第1-10条 帮助

限定条件                
已选(0)清除 条数/页:   排序方式:
Optimal Design of Lightweight Off-Axis Mirror and Flexible Support 期刊论文
Guangxue Xuebao/Acta Optica Sinica, 2020, 卷号: 40, 期号: 19
作者:  Y. Hu,J. Li and X. Jia
收藏  |  浏览/下载:2/0  |  提交时间:2021/07/06
Flexibility calculation and analysis of Bipod reflector support structure 期刊论文
Guangxue Jingmi Gongcheng/Optics and Precision Engineering, 2018, 卷号: 26, 期号: 7, 页码: 1691-1697
作者:  Li, Yu-Peng;  Wang, Zhi;  Sha, Wei;  He, Shuai;  Wu, Qing-Wen
收藏  |  浏览/下载:0/0  |  提交时间:2019/09/17
Ф2 020 mm Aperture Space Infrared Camera Main Reflector Design 期刊论文
Faguang Xuebao/Chinese Journal of Luminescence, 2018, 卷号: 39, 期号: 8, 页码: 1170-1176
作者:  Zhai, Yan;  Mei, Gui;  Jiang, Fan;  Pu, Qian-Shuai
收藏  |  浏览/下载:3/0  |  提交时间:2019/09/17
Structural design of primary mirror subassembly for spatial gravitational wave telescope 期刊论文
Hongwai yu Jiguang Gongcheng/Infrared and Laser Engineering, 2018, 卷号: 47, 期号: 8
作者:  Li, Yupeng;  Wang, Zhi;  Sha, Wei;  Wu, Qingwen;  Zhao, Ya
收藏  |  浏览/下载:2/0  |  提交时间:2019/09/17
Structural design of 2 m-level large-diameter SiC reflector used in space remote sensor 期刊论文
Hongwai yu Jiguang Gongcheng/Infrared and Laser Engineering, 2017, 卷号: 46, 期号: 7
作者:  Wang, K. and J. Dong
收藏  |  浏览/下载:14/0  |  提交时间:2018/06/13
Compound support structure for large aperture mirror of space remote sensor 期刊论文
Guangxue Jingmi Gongcheng/Optics and Precision Engineering, 2016, 卷号: 24, 期号: 7
作者:  Wang, K.-J.;  J.-H. Dong;  M. Xuan;  H.-H. Zhang;  C.-Y. Chi and W.-G. Zhao
收藏  |  浏览/下载:13/0  |  提交时间:2017/09/11
AlGaInP-LED微阵列器件的设计与实验研究 学位论文
博士: 中国科学院大学, 2015
作者:  田超
收藏  |  浏览/下载:42/0  |  提交时间:2015/11/30
航空可见光变焦距镜头自动调焦系统研究 学位论文
博士: 中国科学院大学, 2015
作者:  王昊
收藏  |  浏览/下载:58/0  |  提交时间:2015/11/30
空间光学遥感器次镜及次镜支撑研究 学位论文
硕士: 中国科学院大学, 2015
作者:  于跃
收藏  |  浏览/下载:16/0  |  提交时间:2016/04/11
Design and experimental research of a new type focus mechanism used in space-based telescope (EI CONFERENCE) 会议论文
2012 9th IEEE International Conference on Mechatronics and Automation, ICMA 2012, August 5, 2012 - August 8, 2012, Chengdu, China
Wang D.; Jia X.
收藏  |  浏览/下载:27/0  |  提交时间:2013/03/25
The position of focal plane will be changed because of temperature fluctuation and vacuum environment. In order to make the telescope work well  positioning accuracy of the mechanism is 0.008mm. The performance satisfies the need of precision  a focusing mechanism is needed. To majority of large space-based telescopes  and the scheme design is reasonable and practicable. 2012 IEEE.  the general way to do this would be to use a reflector  which was located in the backfocal distance. One of typical schemes of this mechanism was introduced  however  because of the big axial size  the mechanism can't be used when the size of the enclosure was limited. A new type of focusing mechanism was introduced  which has such advantages of small size  high accuracy and low mass. The design and test methods had been discussed. According to the results  the repeatability positioning accuracy is 0.0025mm  


©版权所有 ©2017 CSpace - Powered by CSpace