空间可展薄膜平面结构的动力学建模及在轨参数辨识研究
作者:
作者单位:

1.上海宇航系统工程研究所,上海 201109;2.上海市空间飞行器机构重点实验室,上海 201108;3.上海交通大学 工程力学系,海洋工程国家重点实验室,上海200240

作者简介:

E-mail: Ases_Zhang@163.comE-mail: Ases_Zhang@163.com

通讯作者:

中图分类号:

O326

基金项目:

国家重点研发计划资助(2016YFB0201604)


STUDY OF DYNAMIC SIMULATION AND ON-ORBIT IDENTIFICATION OF MODAL PARAMETERS OF LARGE MEMBRANE STRUCTURE PLANE ANTENNA
Author:
Affiliation:

1.Aerospace System Engineering in Shanghai, Shanghai 201109, China;2.Shanghai Key Laboratory of Spacecraft Mechanisms, Shanghai 201108, China;3.Department of Engineering Mechanics, State Key Laboratory of Ocean Engineering, Shanghai Jiaotong University, Shanghai 200240

Fund Project:

The project supported by the National Key Research and Development Program of China(2016YFB0201604)

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    摘要:

    大尺度薄膜结构平面天线由于轻质、超柔特点,其动力学性能参数较为复杂.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特性.通过建立的动力学模型,采用特征系统实现算法(ERA)对薄膜结构平面天线的模态参数在轨辨识进行研究.辨识结果与仿真分析结果对比表明,ERA方法可以有效辨识薄膜结构平面天线的低阶固有模态,为其工程化实施奠定了理论研究基础.

    Abstract:

    Because of lightweight and super-flexible characteristics of large-scale membrane structure planar antenna, its dynamic performance parameters are complicated. In order to capture its on-orbit structure dynamic characteristics, a dynamic model of large-scale space developable membrane structure is established by the temperature-structure prestress introduction method, and the dynamic characteristics of the developable membrane structure are analyzed. Through the established dynamic model, the Eigensystem Realization Algorithm (ERA) is used to study the on-orbit identification of the modal parameters of the membrane structure planar antenna. The comparison between the identification results and simulation results shows that the ERA method can effectively identify low-order natural modes of the membrane structure plane antenna, which provides a theoretical basis for its engineering implementation.

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引用本文

张华,刘汉武,蔡国平,彭福军.空间可展薄膜平面结构的动力学建模及在轨参数辨识研究[J].动力学与控制学报,2022,20(1):85~90; Zhang Hua, Liu Hanwu, Cai Guoping, Peng Fujun. STUDY OF DYNAMIC SIMULATION AND ON-ORBIT IDENTIFICATION OF MODAL PARAMETERS OF LARGE MEMBRANE STRUCTURE PLANE ANTENNA[J]. Journal of Dynamics and Control,2022,20(1):85-90.

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  • 收稿日期:2020-11-08
  • 最后修改日期:2021-04-29
  • 录用日期:2021-05-12
  • 在线发布日期: 2022-03-04
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