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A new hybrid piezo-actuated compliant mechanism with self-tuned flexure arm 会议论文
作者:  Ling, Mingxiang;  Cao, Junyi
收藏  |  浏览/下载：12/0  |  提交时间：2019/11/26
Movement decoupling control for two-axis fast steering mirror 会议论文
2nd international conference on photonics and optical engineering, xi'an, china, 2016-10-14
作者:  Rui, Wang;  Qiao, Yongming;  Tao, Lv
收藏  |  浏览/下载：18/0  |  提交时间：2017/05/15
Current Status of the Hard X-ray Nanoprobe Beamline at the SSRF 会议论文
San Diego, CA, AUG 07-08, 2017
作者:  Li, AG;  Jiang, H;  Wang, H;  Zhang, ZH;  He, Y
收藏  |  浏览/下载：12/0  |  提交时间：2019/12/31
Design and kinematic modeling of a planar piezo-actuated multistage compliant mechanism 会议论文
作者:  Ling, Mingxiang;  Cao, Junyi
收藏  |  浏览/下载：5/0  |  提交时间：2019/12/02
Design and analysis of a compliant parallel pan-tilt platform 会议论文
3rd International Workshop on Recent Progress and Novel Applications of Parallel Mechanisms, Tianjin, PEOPLES R CHINA, 2016-07-01
作者:  Yu, Jingjun;  Lu, Dengfeng;  Hao, Guangbo
收藏  |  浏览/下载：9/0  |  提交时间：2019/12/30
Analysis and Testing of A Novel 2-DOF Nanopositioner 会议论文
Chinese Automation Congress (CAC), NOV 27-29, 2015
作者:  Lu, Songsong;  Sun, Yuqiong;  Yan, Peng
收藏  |  浏览/下载：4/0  |  提交时间：2019/12/31
Space focusing mirror assembly with flexure hinges 会议论文
7th International Symposium on Advanced Optical Manufacturing and Testing Technologies: Design Manufacturing, and Testing of Micro- and Nano-Optical Devices, and Systems, AOMATT 2014, April 26, 2014 - April 29, 2014, Harbin, China
Guo Q.; Li W.; Dong J.-H.; Li Y.; Wang K.
收藏  |  浏览/下载：12/0  |  提交时间：2015/04/27
Structural design of large aperture rectangular mirror for space telescope (EI CONFERENCE) 会议论文
2nd International Conference on Civil Engineering and Transportation, ICCET 2012, October 27, 2012 - October 28, 2012, Guilin, China
Li Z.
收藏  |  浏览/下载：27/0  |  提交时间：2013/03/25
Structural design of large aperture mirror is one of the key technologies for space telescope development. To meet the requirements of high stiffness  strength and thermal dimensional stability  some factors such as support scheme  materials selection  lightweight design and flexible support design were taken into account. The three supports location of the mirror was determined according to the modal analytical solution. By adjusting the parameters of flexure hinge  influences of gravity  assembly stress and thermal stress on the mirror were reduced obviously. Finite element analysis (FEA) results indicate that the surface accuracy reach to rms10.2nm and 10.8nm under the gravity along optical axis direction and 5C uniform temperature rise respectively  the fundamental frequency of the mirror component is 268Hz. Dynamics test shows that the first order natural frequency is 256Hz  which shows an error less than 5% compared to FEA results. (2013) Trans Tech Publications  Switzerland.  
Structural design of large aperture rectangular mirror for space telescope 会议论文
2nd International Conference on Civil Engineering and Transportation, ICCET 2012, October 27, 2012 - October 28, 2012, Guilin, China
Li Z.
收藏  |  浏览/下载：8/0  |  提交时间：2014/05/15
Quasi-static and modal analysis of bridge-type compliant mechanism with flexure hinges 会议论文
2013 SECOND INTERNATIONAL CONFERENCE ON ROBOT, VISION AND SIGNAL PROCESSING (RVSP), 2013-12-10
作者:  Ni, Yuan[1];  Deng, Zongquan[2];  Wu, Xiang[3];  Li, Junbao[4];  Li, Long[5]
收藏  |  浏览/下载：5/0  |  提交时间：2019/04/30

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