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DOI:
飞控与探测:2025,8(3):40-54
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大型空间结构大规模柔性铰链问题处理的新策略
(1.上海交通大学 工程力学系;2.上海航天控制技术研究所;3.上海市空间智能控制技术重点实验室)
A New Strategy for Dealing with Large Scale Flexible Hinges in Large Space Structures
(1.Department of Engineering Mechanics, Shanghai Jiao Tong University;2.Shanghai Aerospace Control Technology Institute;3.Shanghai Key Laboratory of Aerospace Intelligent Control Technology)
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中文摘要: 以一种大型空间二维平面相控阵天线结构为对象,提出一个大规模铰链柔性参数确定问题处理的新策略。首先,介绍了大型空间二维平面相控阵天线的结构形式,该天线是一种通过在轨装配方式进行构建的天线;然后,采用有限元方法对天线结构进行了动力学建模,并且给出铰链柔性对系统整体动力学方程的贡献;为了解决大规模铰链存在个体差异性的问题,提出一种基于分群策略的大规模铰链柔性问题优化处理方法,将铰链进行分组,进而采用最优化方法确定最优的分组数量以减少优化问题的规模;最后,通过数值仿真对所提方法的有效性进行了验证。仿真结果表明,铰链柔性会大幅降低天线结构的固有频率,并且造成天线振型的改变,所提方法能够有效地处理大规模铰链柔性问题。
Abstract:This paper proposes a new strategy for addressing the large-scale flexible hinge parameter determination problem, using a large-scale planar phased array antenna structure as the study object. First, it introduces the structural form of the large-scale two-dimensional planar phased array antenna, an antenna assembled in orbit. Then, using the finite element method, the paper models the antenna structure's dynamics, highlighting the impact of hinge flexibility on the overall system dynamics equations. To address individual differences among the numerous hinges, a grouping-based optimization method is proposed, which classifies hinges into groups and optimizes the number of groups to reduce the problem's complexity. Finally, numerical simulations validate the proposed method’s effectiveness. The results indicate that hinge flexibility significantly reduces the antenna structure's natural frequency and alters its vibration modes, demonstrating that the proposed method effectively addresses large-scale hinge flexibility issues.
文章编号:20250304     中图分类号:V474.2    文献标志码:A
基金项目:国家自然科学基金(U23B6001);上海航天创新基金(USCAST2023-25);上海交通大学大学生创新实践计划项目(IPP28001)
引用文本:
宋光浡,颜世恒,郑棋夫,金潮郴,蔡国平,郑翰清.大型空间结构大规模柔性铰链问题处理的新策略[J].飞控与探测,2025,8(3):40-54.

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