[1]JOHNSON C D, DAVIS L P. Need for and Benefits of Launch Vibration Isolation[J]. Smart Structures and Materials: Passive Damping and Isolation,1997,3045:14-19.
[2]WINTHROP M F, COBB R G. Survey of State-of-the-art Vibration Isolation Research and Technology for Space Applications[J]. Smart Structures and Materials: Damping and Isolation,2003,5052:13-26.
[3]马兴瑞,于登云,韩增尧,等. 星箭力学环境分析与试验技术研究[J]. 宇航学报,2006,27(3):323-331.
MA Xingrui, YU Dengyun, HAN Zengyao, et al. ResearchEvolution on the Satellite-rocket Mechanical Environment Analysis and Test Technology[J]. Journal of Astronautics,2006,27(3):323-331.
[4]DENOYER K K,JOHNSON C D. Recent Achievements in Vibration Isolation Systems for Space Launch and On-orbit Applications[C]// 52nd International Astronautical Congress. Paris: IAF,2001:4-11.
[5]张军,谌勇,张志谊,等. 一种整星隔振器的研制[J]. 振动与冲击,2005,24(5):35-38.
ZHANG Jun, CHEN Yong, ZHANG Zhiyi, et al. Design and Research of a New Type of Whole-spacecraft Isolator[J]. Journal of Vibration and Shock, 2005,24(5):35-38.
[6]张针粒,李世其,朱文革,等. 新型近等强度高阻尼航天载荷隔振器研究[J]. 振动与冲击,2012,31(11):1-6.
ZHANG Zhenli, LI Shiqi, ZHU Wenge, et al. New Quasi-equal Strength and High Damping Isolator for Spacecraft Payload[J]. Journal of Vibration and Shock,2012,31(11):1-6.
[7]朱石坚,楼京俊,何其伟,等. 振动理论与隔振技术[M]. 北京:国防工业出版社,2008.
ZHU Shijian, LOU Jingjun, HE Qiwei, et al. Vibration Theory and Vibration Isolation[M]. Beijing: National Defense Industry Press,2008.
[8]PARKER P A, DELOACH R. Structural Optimization of a Force Balance Using a Computional Experiment Design[R]. Reno, Nevada: AIAA,2002.
[9]方开泰,马长兴. 正交与均匀试验设计[M]. 北京:科学出版社,2001.
FANG Kaitai, MA Changxing. Orthogonal and Un-iform Experimental Design[M]. Beijing: Science Press,2001. |