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Equivalent Dynamic Model of the Space Antenna Truss with Initial Stress

机译:初始应力的空间天线桁架等效动力学模型

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摘要

The equivalent modeling approach is one of the key technologies in the design of vibration controllers motivated by the large flexible space truss structure applications. Based on the energy equivalence principle and the classical Timoshenko beam theory, this study establishes a new equivalent dynamic model for the space antenna truss with initial stress by the static condensation method. Compared with previous truss structures of the triangular prism reported in equivalent modeling, the space antenna truss has a more complicated configuration and more members. Meanwhile, this truss structure is in a self-stress state and the connection of the adjacent members is a rigid-jointed. The equivalent anisotropic Timoshenko beam model of the complex space antenna truss with a rigid joints is proposed for the spatial repeating element composed of the beam and cable members in the initial stress state and the joints. According to the kinematic assumptions, displacement expressions of the spatial repeating element are derived using the Taylor series expansion at the center of the spatial repeating element. Then, the stiffness and mass matrices of the equivalent beam model are obtained. The natural vibration characteristics of the equivalent beam model are proved to be in good agreement with those of the original space antenna truss, which indicates that the equivalent beam model has a satisfactory accuracy. As a result, the equivalent dynamic model may serve for the vibration control of the space antenna truss.
机译:等效建模方法是受大型柔性空间桁架结构应用推动的振动控制器设计中的关键技术之一。基于能量等效原理和经典的Timoshenko波束理论,本研究通过静凝结法建立了具有初始应力的空间天线桁架的等效动力学模型。与等效模型中报道的以前的三棱柱桁架结构相比,空间天线桁架具有更复杂的结构和更多的构件。同时,该桁架结构处于自应力状态,并且相邻构件的连接是刚性连接的。针对由初始应力状态下的梁和电缆构件以及节点组成的空间重复单元,提出了具有刚性节点的复杂空间天线桁架的等效各向异性季莫申科波束模型。根据运动学假设,使用空间重复元素中心的泰勒级数展开来导出空间重复元素的位移表达式。然后,获得等效梁模型的刚度和质量矩阵。等效梁模型的固有振动特性被证明与原始空间天线桁架的固有振动特性非常吻合,这表明等效梁模型具有令人满意的精度。结果,等效动态模型可以用于空间天线桁架的振动控制。

著录项

  • 来源
    《AIAA Journal》 |2020年第4期|1851-1863|共13页
  • 作者

  • 作者单位

    Harbin Inst Technol Sch Astronaut 92 West Dazhi St POB 137 Harbin 150001 Peoples R China;

    Shanghai Aerosp Control Technol Inst Shanghai Key Lab Aerosp Intelligent Control Techn 1555 Zhongchun St Shanghai 201109 Peoples R China;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
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