Optics and Precision Engineering, Volume. 18, Issue 8, 1833(2010)
Design of flexible support structure of reflector in space remote sensor
[2] [2] WU Q W, YANG H B, YANG J S, et al..Design and analysis for primary mirror and its support of space camera[J]. Optical Technique, 2004,30(2):152-156. (in Chinese)
[3] [3] JIA M, BI SH SH, YU J J, et al..Analysis and application of large-deformation flexible hinge[J]. Journal of Beijing University of Aeronautics and Astronauti, 2005,31(7):740-743. (in Chinese)
[4] [4] HUANG J Y, WEI Y D, ZHANG W. Optimal design of the flexure hinge parameter based on space micro-displacement worktable [J]. Mechanical & Electrical Engineering Magazine,2006,23(1):55-57. (in Chinese)
[5] [5] LOBONTIU N, PAINE JSN,O’MALLEY E, et al..Parabolic and hyperbolic flexure hinges:flexibility,motion precision and stress characterization based on compliance closed-form equations[J]. Precision Engineering,2002,26(2):183-192.
[6] [6] CHEN J H, LI P AN. Deduction of compliance of cosh-flexure hinge[J]. Machinery Design & Manufacture, 2008,7:62-63. (in Chinese)
[10] [10] SUN B Y,XUE J. Design and analysis on the flexible cone-shaped sheath of the optical reflector[J]. Optical Technique, 2008,34(2):230-232. (in Chinese)
Get Citation
Copy Citation Text
WANG Zhong-su, ZHAI Yan1, MEI Gui1, JIANG Fan, CHENG Zhi-feng. Design of flexible support structure of reflector in space remote sensor[J]. Optics and Precision Engineering, 2010, 18(8): 1833
Category:
Received: Nov. 16, 2009
Accepted: --
Published Online: Dec. 7, 2010
The Author Email: Zhong-su WANG (wzs1998@yahoo.com.cn)
CSTR:32186.14.