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大型空间可展薄膜结构动力学仿真分析

张华 刘汉武 李东颖 彭福军

张华, 刘汉武, 李东颖, 彭福军. 大型空间可展薄膜结构动力学仿真分析[J]. 空间科学学报, 2018, 38(1): 101-108. doi: 10.11728/cjss2018.01.101
引用本文: 张华, 刘汉武, 李东颖, 彭福军. 大型空间可展薄膜结构动力学仿真分析[J]. 空间科学学报, 2018, 38(1): 101-108. doi: 10.11728/cjss2018.01.101
ZHANG Hua, LIU Hanwu, LI Dongying, PENG Fujun. Study of Dynamics Simulation on Large Space Deployable Membrane Structuresormalsize[J]. Journal of Space Science, 2018, 38(1): 101-108. doi: 10.11728/cjss2018.01.101
Citation: ZHANG Hua, LIU Hanwu, LI Dongying, PENG Fujun. Study of Dynamics Simulation on Large Space Deployable Membrane Structuresormalsize[J]. Journal of Space Science, 2018, 38(1): 101-108. doi: 10.11728/cjss2018.01.101

大型空间可展薄膜结构动力学仿真分析

doi: 10.11728/cjss2018.01.101
基金项目: 

上海市自然科学基金项目(16ZR1436200)和国家高性能计算重点专项项目(2016YFB0201604,2016YFB0201600)共同资助

详细信息
    作者简介:

    张华,E-mail:ases_zhang@163.com

  • 中图分类号: V476

Study of Dynamics Simulation on Large Space Deployable Membrane Structuresormalsize

  • 摘要: 相对于传统的航天器平面刚性天线结构,柔性可展薄膜结构因其质量轻、收拢体积小等优点成为大型天线的重要发展方向,特别是在天基合成孔径雷达(SAR)天线高分辨率对地观测技术领域具有广阔的应用前景.为掌握其在轨结构动力学特性,基于温度-结构预应力导入方法建立了大型空间可展薄膜结构的动力学模型,分析了可展薄膜结构的动力学性能参数,同时基于建立的动力学模型开展了可展薄膜结构的优化设计研究,得到主要设计参数对可展薄膜结构动力学性能参数的影响权重,为其工程化实施奠定了理论研究基础.

     

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出版历程
  • 收稿日期:  2017-03-13
  • 修回日期:  2017-10-09
  • 刊出日期:  2018-01-15

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