1. 毕业设计（论文）的内容和要求
随着航天技术的迅速发展，航天任务需求不断提高，对航天器结构提出了大型化和轻质化的要求。
由于受运载工具空间和运载能力的限制，大型空间结构通常无法直接发射，促使空间可展开结构和空间装配式结构的诞生。
为了便于发射时的折叠收拢和入轨后的展开，空间可展开结构往往包含众多绳、杆、梁等柔性部件。
2. 参考文献
[1] Haddow A G, Barr A D S, Mook D T. Theoretical and experimental study of modal interaction in a two-degree-of-freedom structure. Journal of Sound Vibration, 1984, 97(3): 451-473.[2] Santiago-Prowald J, Baier H. Advances in deployable structures and surfaces for large apertures in space. CEAS Space Journal, 2013, 5: 89-115.[3] Liu L K, Shan J J, Zhang Y. Dynamics modeling and analysis of spacecraft with large deployable hoop-truss antenna. Journal of Spacecraft Rockets, 2016, 53(3): 471-479.[4] Nayfeh T A, Nayfeh A H, Mook D T. A theoretical and experimental investigation of a three-degree-of-freedom structure. Nonlinear Dynamics, 2013, 6(3): 353-374.[5] Balachandran B, Nayfeh A H. Nonlinear motions of beam-mass structure. Nonlinear Dynamics, 1991, 1(1): 39-61.[6] Bian Y, Gao Z, Lv X, et al. Theoretical and experimental study on vibration control of flexible manipulator based on internal resonance. Journal of Vibration Control, 2018, 24(15): 3321-3337.[7] 胡海岩, 田强, 张伟, 金栋平等. 大型网架式可展开空间结构的非线性动力学与控制. 力学进展, 2013, 43(4): 390-414.[8] Misra A K, Kalaycioglu S. Approximate solutions for vibrations of deploying appendages. Journal of Guidance Control Dynamics, 2012, 14(2): 287-293.[9] Chen J, Hu W H, Li Q S. Nonlinear dynamic of a foldable multibeam structure with one to two internal resonances. International Journal of Mechanical Sciences, 2019, 150: 369-378.[10] Zhang W, Chen J, Sun Y. Nonlinear breathing vibrations and chaos of a circular truss antenna with 1:2 internal resonance. International Journal of Bifurcation Chaos, 2016, 26(5): 1650077-1-33.[11] Chen L Q, Zhang G C, Ding H. Internal resonance in forced vibration of coupled cantilevers subjected to magnetic interaction. Journal of Sound Vibration, 2015, 354(1): 196-218.
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