[1] ADDARIN D,AGLIETTI G S,REMEDIA M. Experimental and numerical investigation of coupled microvibration dynamics for satellite reaction wheels［J］. Journal of Sound and Vibration, 2017,386: 225-241.

[2] HAN CH Y, XU ZH B, WU Q W, et al.. Optimization design and error distribution for secondary mirror adjusting mechanism of large optical payload［J］. Opt. Precision Eng., 2016, 24(5): 1093-1103. (in Chinese)

[3] LI L, TAN L Y, KONG L, et al.. The influence of flywheel micro vibration on space camera and vibration suppression［J］. Mechanical Systems and Signal Processing, 2018, 100: 360-370.

[4] KIM D K. Micro-vibration model and parameter estimation method of a reaction wheel assembly［J］. Journal of Sound and Vibration, 2014，333（18）: 4214-4231.

[5] WANG Z Y,ZOU Y J, JIAO A C, et al.. The jitter measurement and analysis for a remote sensing satellite platform［J］. Spacecraft Environ Eng, 3 (32) (2015): 278–285.

[6] MASTERSON R A,MILLER D W, GROGAN R L. Development and validation of reaction wheel disturbance models: empirical model［J］. Journal of Sound and Vibration, 2002,249 (3): 575-598.

[7] DAVIS L P, CUNNINGHAM D, BICOS A S, et al.. Adaptable passive viscous damper: an adaptable D-StrutTM［A］. 1994 North American Conference on Smart Structures and Materials［C］. International Society for Optics and Photonics, 1994: 47-58.

[8] DAVIS P, CUNNINGHAM D, HARRELL J. Advanced 1.5 Hz passive viscous isolation system［A］. 35th AIAA SDM Conference［C］. Hilton Head, South Carolina, 1994: 1-11.

[9] LIU X T, KONG X S, SHEN J F, et al.. Vibration isolator with relaxation type damping for micro-vibration isolation from satellite remote sensors［J］. Opt. Precision Eng., 2017, 25(9): 2448-2453. (in Chinese)

[10] WANG J, ZHAO SH G, WU D F, et al.. The mechanism study of a micro-vibration isolator based on viscous fluid［J］. Journal of Vibration Engineering, 2015, 2(4): 237-347. (in Chinese)

[11] ZHANG Y, XU SH J. Dual-stage passive vibration isolation system of optical payloads for high resolution remote sensing satellite［J］. Acta Aeronautica et Astronautica Sinica, 2012, 33(9): 1643-1654. (in Chinese)

[12] VAILLON L, PHILIPPE C. Passive and active microvibration control for very high pointing accuracy space system［J］. Smart Materials and Structures, 1999,8(6): 719-728.

[13] BOYD J, HYDE T T, OSTERBERG D, et al.. Performance of a launch and on-orbit isolator［C］. SPIE’s 8th Annual International Symposium on Smart Structures and Materials. International Society for Optics and Photonics, 2001: 433-440.

[14] ZHANG Y, XU S J. Vibration isolation platform for control moment gyroscopes on satellites［J］. Journal of Aerospace engineering, 2012, 25(4): 641-652.

[15] SULLIVAN J M, GOODING J C, IDLE M K, et al.. Performance testing for an active/passive vibration isolation and steering system［R］. AIAA-1996-1210-CP. Reston: AIAA, 1996.

[16] LI L, WANG D, XU J, et al.. Influence of micro-vibration of flywheel components on optical axis of high resolution optical satellite［J］. Opt. Precision Eng., 2016, 24(10): 2515-2522. (in Chinese)

[17] CHEN T. Research of Viscous Fluid Damping Isolator Used in Space［D］. Beijing: Graduate University of the Chinese Academy of Sciences, 2016. (in Chinese)

[18] OH H U, IZAWA K, TANIWAKI. Development of variable-damping isolator using bio-metal fiber for reaction wheel vibration isolation［J］. Smart materials and Structures, 2005, 14(5): 928-933.

[19] WANG J, ZHAO SH G, WU D F, et al.. A Test Method of Dynamic Damping Coefficient of Micro-vibration Isolators［J］. Acta Aeronautica et Astronautica Sinica. 2014,35(2): 454-460. (in Chinese)