[1] [1] ATAD E. Atlast-9.2m: a large-aperture deployable space telescope ［J］. Proc.of SPIE, 2010, 7731, 77312M1-10.

[2] [2] YE W N, DONG J H. Optimized design of lightweight structural parameters for large-aperture primary mirror ［J］. Chinese Optics, 2012, 5(3): 222-228. (in Chinese)

[3] [3] CROCKER J H. Fixing the hubble space telescope ［J］. Space Astronomical Telescopes and Instruments, 1991, 1494: 2-8.

[4] [4] ALLENJ, BRONOWICKI, JOHN W. A family of full spacecraft-to-payload isolators ［J］. Technology Review Journal, 2005: 21-41.

[5] [5] MORIO T, YOSHIHISA T, HIROO K. In-orbit measurements of spacecraft microvibrations for satellite laser communication links［J］. Optical Engineering, 2010, 49(8): 1-10.

[6] [6] YANG X B, CHANG L, JIN G. Influence of dynamic imbalance of SGCMG rotor on remote sensing satellite imaging ［J］. Chinese Optics, 2012, 5(4): 358-365. (in Chinese)

[7] [7] MILLER S D. Investigation of a novel compact vibration isolation system for space applications ［D］. USA: Air Force Institute of Technology, 2010.

[8] [8] WANG P, et al.. Vibration damping design for airborne electro-optical surveillance platform ［J］. Opt. Precision Eng., 2011, 19(1): 83-89.(in Chinese)

[9] [9] FU M G, LIU Y, CUI M L, et al.. Metal-rubber vibration absorber for aerocraft ［J］. Opt. Precision Eng., 2013, 21(5): 1174-1182.(in Chinese)

[10] [10] KARL J P. Use of a passive reaction wheel jitter isolation system to meet the Advanced X-Ray Astrophysics Facility imaging performance requirements ［J］. Proc.of SPIE, 1998, 3356: 1078-1094.

[11] [11] LARRY. Precision telescope pointing and spacecraft vibration isolation for the Terrestrial Planet Finder Coronagraph ［J］. Proc. SPIE, 2005, 589902-1-4.

[12] [12] DASGUPTAB. A newton-euler formulation for the inverse dynamics of the stewart platform manipulator ［J］. Mechanism and Machine Theory, 1998, 33(8): 1135-1152.

[13] [13] KOEKEBAKKER S H. Alternative parameterization in modeling and analysis of a Stewart platform ［J］. Selected Topics in Identification, Modeling and Control, 1996, 9: 59-68.

[14] [14] ZHAO Q, LI H R, HAN J W. Study on vibration of Stewart platform ［J］. Mechanical Science and Technology, 2004, 23(5): 594-597. (in Chinese)

[15] [15] ZHANG Y, ZHANG J R. Analysis of influence of vibrationisolation platform on attitude control system and its parameter selection ［J］. Journal of Astronautics, 2013, 34(5): 657-664. (in Chinese)

[16] [16] GOUGH V E. Universal tyre testing machine ［C］. Proc. Ninth Inter-national Technical Congress, U S, 1962: 117-137.

[17] [17] HANIEH A A. Active isolation and damping of vibrations via stewart platform ［D］. Belgium: Universite Libre de Bruxelles, 2003.

[18] [18] DAVIS L P. Hubble space telescope reaction wheel assembly vibration isolation system ［C］. NASA Workshop on Structural Dynamics and Control Interaction of Flexible Structures. G.C. Marshall Space Flight Center, U S, 1986: BA1-BA22.

[19] [19] LI Z X, ZHANG L, YAO J S, et al.. Design of Cartwheel bi-aixal flexural hinge ［J］. Opt. Precision Eng. , 2013, 21(9): 2317-2325.(in Chinese)

[20] [20] YAN J K. Mechanical Vibration Isolation Technology of ［M］. Shanghai: Shanghai Science & Technical Documentation Press, 1985.(in Chinese)

[21] [21] MICHAEL R H.Vibration Simulation Using MATLAB and ANSYS ［M］. U S: Champman & Hall/CRC Press, 2001.