Xue Mingde, Xiang Zhihai. Thermal-dynamic coupling problem of large space structures and its FEM analyses [J]. Chinese Journal of Solid Mechanics, 2011, 32(S1): 318―328. (in Chinese)
[3]
Thornton E A. Thermal structures for aerospace applications [M]. Virginia: AIAA, 1996: 343―346.
[4]
Boley B A. Approximate analyses of thermally induced vibrations of beams and plates [J]. Journal of Applied Mechanics-Transactions of the Asme, 1972, 39(1): 212―216.
Chen Wujun, Zhang Shujie. Deployable space structures and analysis theory [M]. Beijing: China Astronautic Publishing House, 2006: 3―25. (in Chinese)
[7]
Xue M D, Duan J, Xiang Z H. Thermally-induced bending-torsion coupling vibration of large scale space structures [J]. Computational Mechanics, 2007, 40(4): 707―723.
[8]
Johnston J D, Thornton E A. Thermally induced dynamics of satellite solar panels [J]. Journal of Spacecraft and Rockets, 2000, 37(5): 604―613.
[9]
Park S Y. Thermally induced attitude disturbance control for spacecraft with a flexible boom [J]. Journal of Spacecraft and Rockets, 2002, 39(2): 325―328.
[10]
Jiang J P, Li D X. Finite element formulations for thermopiezoelastic laminated composite plates [J]. Smart Materials and Structures, 2008, 17(1): 015027.
Jiang Jianping, Li Dongxu. Finite element modeling and shape control for piezoelectric composite plates under thermal load [J]. Chinese Journal of Theoretical and Applied Mechanics, 2007, 39(4): 503―509. (in Chinese)
[13]
Thornton E A, Kim Y A. Thermally-induced bending vibrations of a flexible rolled-up solar-array [J]. Journal of Spacecraft and Rockets, 1993, 30(4): 438―448.
[14]
Gulick D W, Thornton E A. Thermally-induced vibrations of a spinning spacecraft boom [J]. Acta Astronautica, 1995, 36(3): 163―176.
[15]
Ko K E, Kim J H. Thermally induced vibrations of spinning thin-walled composite beam [J]. Aiaa Journal, 2003, 41(2): 296-303.
[16]
Xue M D, Ding Y. Two kinds of tube elements for transient thermal-structural analysis of large space structures [J]. International Journal for Numerical Methods in Engineering, 2004, 59(10): 1335―1353.
[17]
Li W, Xiang Z, Chen L, et al. Thermal flutter analysis of large-scale space structures based on finite element method [J]. International Journal for Numerical Methods in Engineering, 2007, 69(5): 887-907.
[18]
Duan J, Xiang Z H, Xue M D. Geometric nonlinear analyses for large space frames considering thermal-structural coupling [J]. Journal of Thermal Stresses, 2007, 31(1): 40―58.
Li Wei, Xue Mingde, Xiang Zhihai. Stability analysis of coupled thermal-dynamic systems in space structures based on FEM [J]. Journal of Tsinghua University (Science and Technology), 2007, 47(11): 2076―2080. (in Chinese)
Xue Mingde, Li Wei, Xiang Zhihai. Thermal flutter analysis of a spacecraft with a flexible appendage based on FEM [J]. Journal of Tsinghua University (Science and Technology), 2008, 48(2): 270―275. (in Chinese)
Li Wei, Xue Mingde, Xiang Zhihai. Thermal-dynamic stability analysis of structural appendages attached to satellite [J]. Journal of Zhejiang University (Engineering Science), 2009, 43(7): 1288―1292. (in Chinese)
[25]
Tsuchiya K. Thermally induced vibrations of a flexible appendage attached to a spacecraft [J]. Aiaa Journal, 1977, 15(4): 505―510.
[26]
Wasfy T M, Noor A K. Computational strategies for flexible multibody systems [J]. Applied Mechanics Reviews, 2003, 56(6): 553―613.
[27]
Liu J Y, Lu H. Thermal effect on the deformation of a flexible beam with large kinematical driven overall motions [J]. European Journal of Mechanics A-Solids, 2006, 26(1): 137―151.
Liu Jinyang, Lu Hao. Parallel manipulator dynamics with thermal strain [J]. Chinese Journal of Applied Mechanics, 2007, 24(3): 391―395, 503. (in Chinese)
[30]
Li T J, Wang Y. Deployment dynamic analysis of deployable antennas considering thermal effect [J]. Aerospace Science and Technology, 2009, 13(4/5): 210―215.
[31]
Wu J, Zhao Z, Ren G. Dynamic analysis of space structure deployment with transient thermal load [J]. Advanced Materials Research, 2012, 479/480/481: 803―807.
[32]
Hairer E, Wanner G. Solving ordinary differential equations II: Stiff and differential-algebraic problems [M]. Berlin: Springer-Verlag, 1996: 451―563.
[33]
王勖成. 有限单元法[M]. 北京: 清华大学出版社, 2003: 447―448.
[34]
Wang Xucheng. Finite element methos [M]. Beijing: Tsinghua University Press, 2003: 447―448. (in Chinese)
[35]
Zhao Z, Ren G. A quaternion-based formulation of euler-bernoulli beam without singularity [J]. Nonlinear Dynamics, 2011, 67(3): 1―11.
[36]
Shabana A A. Dynamics of multibody systems [M]. New York: Cambridge University, 2005: 244―248.
[37]
Dmitrochenko O N, Pogorelov D Y. Generalization of plate finite elements for absolute nodal coordinate formulation [J]. Multibody System Dynamics, 2003, 10(1): 17―43.