[1] [1] Qin Yuling, Kong Xiangren, Luo Wenbo. RSM-based FEM model updating for a carbon fiber honeycomb sandwich panel [J]. Journal of Vibration and Shock, 2011, 30(7): 71-86. (in Chinese)

[2] [2] Wang Pingping, Luo Wenbo, Zou Jingxiang, et al. Dynamic analysis of the carbon fiber honeycomb sandwich structure [J]. Acta Materiae Compositae Sinica, 2002, 19(6): 134-136. (in Chinese)

[3] [3] Wo Xiyuan, Xia Yingwei, Tu Bin. The property of honeycomb sandwich structure and the destroy mode analyzing [J]. Spacecraft Recovery & Remote Sensing, 2005, 26(4): 45-49. (in Chinese)

[4] [4] Wei Lei, Jin Guang, Xie Xiaoguang, et al. Optimized design of primary load-bearing structure for earth observation micro-satellite [J]. Optics and Precision Engineering, 2015, 23(11): 3183-3191. (in Chinese)

[5] [5] Zhai Guang, Yang Xiaoping, Liang Bin, et al. Model analysis of multi-interlayer honeycomb plate-based on equivalent theory [J]. Journal of Mechanical Strength, 2007, 29(3): 517-520. (in Chinese)

[6] [6] Wang Jiawei, Chen Minsun, Jiang Houman. Experimental study on the temperature effect on the flexural properties of Nomex honeycomb sandwich structure [J]. Infrared and Laser Engineering, 2016, 45(1): 0120004. (in Chinese)

[7] [7] Soliman H E, Makhecha D P, Vasudeva S, et al. On the static analysis of sandwich panels with square honeycomb core [J]. AIAA Journal, 2008, 46(3): 627-634.

[8] [8] Xu Shengjin, Kong Xianren, Wang Benli, et al. Method of equivalent analysis for statics and dynamics behavior of orthotropic honeycomb sandwich plates[J]. Acta Materiae Compositae Sinica, 2000, 17(3): 92-95. (in Chinese)

[9] [9] Xia Lijuan, Yu Yin, Jin Xianding. Optimum design of composite honeycomb sandwich panels subjected to multiple case of load [J]. Journal of Vibration and Shock, 2005, 24(3): 117-120. (in Chinese)

[10] [10] Xiu Yingshu, Cui Degang. Ply optimization design for stability of composite laminates [J]. Engineering Mechanics, 2005, 22(6): 212-216. (in Chinese)

[11] [11] Tan Luyang, Wang Dong, Kong Lin. Suppression of random vibration response of optical satellite by matching honeycomb stiffened plates′ structure parameters [J]. Optics and Precision Engineering, 2016, 24(2): 372-380. (in Chinese)

[12] [12] Xia Yu, Zeng Chunmei, Guo Peiji. Lay-up design of quasi-isotropic CFRP mirror for active forming [J]. Infrared and Laser Engineering, 2012, 41(7): 1885-1892. (in Chinese)