[1] MATTHEWS G,HAVEY Jr K, EGERMAN R. A paradigm shift to enable more cost effective space science telescope missions in the upcoming decades ［J］. SPIE, 2010, 7738:773824-1-773824-7.
[2] ZHU SH Y, LEI Y J. Vibration reduction of payloads on spacecraft based on structure parameters of spacecraft-bracket system［J］. Journal of National University of Defense Technology, 2014,36(2),41-46. (in Chinese)
[3] TAN T L, ZHU CH Y, ZHU D F, et al.. Overview of micro-vibration testing, isolation and suppression technology for spacecraft［J］. Aerospace Shanghai, 2014,31(6):36-45. (in Chinese)
[4] ZHANG Q J, WANG G Y, ZHENG G T. Micro-vibration attenuation methods and key techniques for optical remote sensing satellite ［J］. Journal of Astronautics, 2015,36(2):125-132. (in Chinese)
[5] WANG G Y，ZHOU D Q，ZHAO Y. Data analysis of micro-vibration on-orbit measurement for remote sensing satellite ［J］. Journal of Astronautics, 2015,36(3):261-267. (in Chinese)
[6] HYDE T T, HA K Q, JOHNSTON J D, et al.. Integrated modeling activities for the James Webb Space Telescope［J］. SPIE,2004,588-599.
[7] BRONOWICKI A J. Vibration isolator for large space telescopes ［J］. Journal of Spacecraft and Rockets,2006,43(1):45-53.
[8] WANG Z Y, ZOU Y J, JIAO A CH, et al.. The jitter measurement and analysis for a remote sensing satellite platform［J］. Spacecraft Environment Engineering, 2015,32(3),278-285. (in Chinese)
[9] HUANG T X, ZHANG Y, XU SH J. Dynamic modeling of combined reaction wheel and vibration isolation platform system［J］. Journal of Beijing University of Aeronautics and Astronautics,2013,39(1)，120-125. (in Chinese)
[11] DONG Y H. Spacecraft Jitter:Theory and Practice ［M］.Beijing: China Aerospace Press,2015. (in Chinese)
