基于带状弹簧的空间望远镜精密展开技术进展
[1] 陈务军,张淑杰. 空间可展结构体系与分析导论(第一版)[M]. 北京:中国宇航出版社,2006.
CHEN W J,ZHANG S J. Deployable Space Structures and Analysis Theory(The 1st edition)[M]. Beijing:China Astronautic Publishing House,2006.(in Chinese)
[2] SEFFEN K A,PELLEGRINO S. Deployment dynamics of tape springs[C]. Proceedings of the Royal Society of London,A,London:UK,1999,455:1003-1048.
[3] YEE J C H,SOYKASAP O,PELLEGRINO S. Carbon fibre reinforced plastic tape springs[C]. Collection of Technical Papers-AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics and Materials Conference. Gossamer Spa.,2004,3305-3313.
[4] . . Development and testing of an actively-controlled large aperture Cassegrain telescope for spacecraft deployment[J]. SPIE, 2004, 5487: 1042-1053.
[5] BOONE B G,BRUZZI J R,MILLARD W P,et al.. Optical communications development for spacecraft applications:recent progress at JHU/APL[C]. IEEE Aero. Conf.,2005:1570-1582.
[6] . . High resolution deployable telescope for satellite application[J]. SPIE, 2004, 5234: 531-538.
[7] . Realization and preliminary tests on an innovative deployable structure for a high resolution telescope for microsatellite[J]. SPIE, 2004, 5570: 411-422.
[8] BLACK J T,WHETZAL J A,DEBLONK B J,MASSARELLO J J. Deployment repeatability testing of composite tape springs for space optics applications[C]. Collection of Technical Papers-AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics and Materials Conference. 2006
[9] WHETZAL J A,DEBLONK B J. Dynamics of meter-class deployable composite structures for optical systems[C]. Collection of Technical Papers:49th AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics and Materials Conference,2008.
[10] BLANCHARD L,FALZON F,DUPUIS J,MERLET J P. Deployable hexapod using tape-springs[C]. ESA/CNES Symposium,Marseille,2005.
[11] . On the correction capability of a deployed tape-spring hexapod[J]. Mech. Mach. Theory, 2008, 43(8): 1009-1023.
[12] . . A self-deployment hexapod model for a space application[J]. J. Comput. Nonlinear Dynam., 2009, 4: 011002.
[13] 杨东武,段宝岩,仇原鹰.空间可展开望远镜结构动力优化设计[J].中国机械工程,2006,17(增刊):241-245.
YANG D W,DUAN B Y,QIU Y Y. Dynamics optimization design of a deployable space telescope structure[J]. China Mechanical Eng.,2006,17(supp.):241-245.(in Chinese)
[14] 刘磊,高明辉.空间可展开式望远镜反射单元镜支撑技术[J].光学技术,2006,32(3):343-345.
[15] 李瀛搏,傅丹鹰,王永辉,等.空间光学精密展开机构展开方法的初步探讨[J].航天返回与遥感,2007,28(3):11-18.
LI Y B,FU D Y,WANG Y H,et al.. The preliminary discussion on deployment approach of space optical-precision deployable mechanisms[J]. Spacecraft Recov. R. Sen.,2007,28(3):11-18.(in Chinese)
[16] 王翔,张广宇,初昶波,等.空间大口径望远镜可展开镜片系统的概念设计[J].机械设计与研究,2004,20(6):49-52.
WANG X,ZHANG G Y,CHU C B,et al.. Concept design for deployable large-aperture optical structure of space telescopes[J]. Machine Design and Research,2004,20(6):49-52.(in Chinese)
[17] 刘志全,孙国鹏.空间光学遥感器主镜展开机构重复定位精度分析[J].中国空间科学技术,2008,28(1):27-34.
LIU Z Q,SUN G P. Analysis of repeatability of the primary mirror deployment mechanism for space optical remote sensors[J]. Chinese Space Science and Technol.,2008,28(1):27-34.(in Chinese)
[18] 王俊,关富玲,周志钢.空间可展结构卷尺铰链的设计与分析[J].宇航学报,2007,28(3):720-726,746.
WANG J,GUAN F L,ZHOU Z G. Design and analysis of tape hinge for deployable structures[J]. J. Astronautics,2007,28(3):720-726,746.(in Chinese)
李创, 王炜, 樊学武. 基于带状弹簧的空间望远镜精密展开技术进展[J]. 中国光学, 2009, 2(2): 85. LI Chuang, WANG Wei, FAN Xue-wu. Advance in precision deployment techniques for space telescopes based on tape springs[J]. Chinese Optics, 2009, 2(2): 85.
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