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Reduced Model for Flexible Solar Sail Dynamics

机译:简化的太阳帆动力学模型

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摘要

In this paper, a reduced model for flexible solar sail dynamics was formulated in mixed coordinates. Foreshortening effects due to the foreshortening deformation of sails and booms were considered. For instance, the dynamic responses of a five-point connected square solar sail during maneuvers were investigated using this reduced model. A time-varying modal stiffness matrix was used to simulate time-varying properties of modal frequencies, due to the change of the solar pressure load. The reduced model was highly efficient using the modal reduction techniques. Its accuracy was verified using a high-fidelity finite element model in ABAQUS/Explicit It was illustrated that the reduced model can be both efficient and accurate for engineering applications.
机译:在本文中,在混合坐标系中建立了简化的太阳帆动力学模型。考虑了由于帆和吊杆的节距变形而引起的节距效果。例如,使用此简化模型研究了五点连接的方形太阳帆在操纵过程中的动力响应。使用时变模态刚度矩阵来模拟由于太阳压力负载的变化而引起的模态频率的时变特性。使用模态归约技术,归约模型非常高效。使用ABAQUS / Explicit中的高保真有限元模型验证了其准确性。结果表明,简化后的模型对于工程应用而言既高效又准确。

著录项

  • 来源
    《Journal of Spacecraft and Rockets 》 |2011年第3期| p.446-453| 共8页
  • 作者单位

    Tsirighua University, 100084 Beijing, People's Republic of China;

    China Aerospace Science and Technology Corporation,100037 Beijing, People's Republic of China;

    Tsinghua University, 100084 Beijing, People's Republic of 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
  • 中图分类
  • 关键词

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