[1] [1] LIU ZH Q. Spacecraft Institutions and Their Reliability ［M］. Beijing: China Aerospace Press, 2012. (in Chinese)

[2] [2] JIANG H L, AN Y, ZHANG Y L, et al.. Analysis of the status quo, development trend and key technologies of space laser communication［J］. Journal of Spacecraft TT&C Technology, 2015, 34(3): 207-217. (in Chinese)

[3] [3] WANG Z S, WU Q W, GUO Q F, et al.. Design of anti-shock vibration isolation for detector module of space optics load［J］. Opt. Precision Eng., 2017, 25(8): 2098-2105. (in Chinese)

[4] [4] WANG SH X,LI J L, QI G, et al.. Protecting device for explosive bolt in space camera［J］. Opt. Precision Eng.,2014, 22(12): 3318-3323. (in Chinese)

[5] [5] XUAN M, ZHANG D W, GU S, et al.. Design of hold-down and release mechanism for solar panel of micro-satellite［J］. Opt. Precision Eng., 2017, 25(4): 447-454. (in Chinese)

[6] [6] ZHANG J L, ZHOU J. Design and verification of kinematic system in deploying mechanism for CubeSats［J］. Opt. Precision Eng., 2017, 25(4): 387-395. (in Chinese)

[7] [7] WANG Y P, WANG K, JIA R D, et al.. Design and application of accurate pointing and auto-unlocking sun tracker on satellite［J］. Opt. Precision Eng., 2016, 24(1): 65-72. (in Chinese)

[8] [8] ERIC D MILLERA, MICHAEL DESPENZAB, ILYA GAVRILYUKB, et al.. A prototype coarse pointing mechanism for laser communication［C］. Free-Space Laser Communication and Atmospheric Propagation XXIX. 2017

[9] [9] HE Z R, ZHOU C, LIU L, et al.. Research progress of shape memory alloys and their applications［J］. Foundry Technology, 2017, 38(2): 257-261. (in Chinese)

[10] [10] ZHANG M D, LI Y G, WU Y B, et al.. Research on dynamic driving characteristic of shape memory alloy actuator［J］. Aeronautical Manufacturing Technology, 2017(17): 49-54. (in Chinese)

[11] [11] QIN X Y, ZHANG X Y, YAN X J, et al.. An SMA-actuated locking device for feed source structure based on self-locking principle［J］. Journal of Astronautics, 2016, 37(3): 357-363. (in Chinese)

[12] [12] BUCKLEY S, FOSNESS E, GAMMILL W. Deployment and release devices efforts at the air force research laboratory space vehicles directorate［C］//AIAA Space 2001 Conference and Exposition, Albuquerque, NM, USA. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2001.

[13] [13] NAVA N, COLLADO M, CAB S R. REACT: resettable hold down and release actuator for space applications［J］. Journal of Materials Engineering and Performance, 2014, 23(7): 2704-2711.

[14] [14] WANG X. Operational modal identification of spacecraft structures［D］. Shanghai: Fudan University, 2008. (in Chinese)

[15] [15] LIU CH, ZHU J T, LIU L H, et al.. Dynamics parameter measurement and analysis of certain satellite platform during the launch and in orbit［J］. Spacecraft Environment Engineering, 2017, 34(3): 270-276. (in Chinese)