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含间隙铰链的非线性动力学建模及数值分析
引用本文:徐彦,王培栋,孙禄君,朱东方,方琴.含间隙铰链的非线性动力学建模及数值分析[J].上海航天,2020,37(1):51-62.
作者姓名:徐彦  王培栋  孙禄君  朱东方  方琴
作者单位:浙江大学 航空航天学院,浙江 杭州310027,浙江大学 航空航天学院,浙江 杭州310027,上海航天控制技术研究所,上海201109;上海市空间智能控制技术重点实验室,上海201109,上海航天控制技术研究所,上海201109;上海市空间智能控制技术重点实验室,上海201109,浙江大学 航空航天学院,浙江 杭州310027
基金项目:国家自然科学基金资助项目(11532011,11402229);上海航天科技创新基金资助项目(SAST2016074)
摘    要:针对空间可展开机构中的含间隙铰链,建立非线性动力学模型,研究其非线性动力学特性。将含间隙铰链实体等效为"T"字型梁模型,针对两侧端部的径向碰撞和侧向碰撞,首次提出了碰撞点的检测算法。针对不同的碰撞类型,建立相应的非线性接触力和摩擦力分析模型,将碰撞点处的作用力等效施加到"T"字型梁模型上。进行"T"字型梁模型在轴向冲击载荷下的动力学特性分析,并与ANSYS软件的分析结果进行比较,验证了含间隙铰链非线性动力学模型的有效性。分析了有多个含间隙铰链的可展开桁架动力学响应特性,研究含间隙铰链对桁架响应的影响机理。结果表明:采用含间隙铰链的动力学模型,可以更加精确地分析可展开桁架结构的非线性动力学响应,为可展开桁架结构的动力学设计提供支撑。

关 键 词:空间可展开机构  含间隙铰链  非线性动力学  碰撞检测算法
收稿时间:2018/7/17 0:00:00
修稿时间:2018/9/10 0:00:00

Nonlinear Dynamic Modeling and Numerical Analysis with Clearance Joints
XU Yan,WANG Peidong,SUN Lujun,ZHU Dongfang and FANG Qin.Nonlinear Dynamic Modeling and Numerical Analysis with Clearance Joints[J].Aerospace Shanghai,2020,37(1):51-62.
Authors:XU Yan  WANG Peidong  SUN Lujun  ZHU Dongfang and FANG Qin
Institution:School of Aeronautics and Astronautics, Zhejiang University, Hangzhou 310027, Zhejiang, China,School of Aeronautics and Astronautics, Zhejiang University, Hangzhou 310027, Zhejiang, China,Shanghai Aerospace Control Technology Institute, Shanghai 201109, China;Shanghai Key Laboratory of Space Intelligent Control Technology, Shanghai 201109, China,Shanghai Aerospace Control Technology Institute, Shanghai 201109, China;Shanghai Key Laboratory of Space Intelligent Control Technology, Shanghai 201109, China and School of Aeronautics and Astronautics, Zhejiang University, Hangzhou 310027, Zhejiang, China
Abstract:A nonlinear dynamic model for the clearance joints in space deployable mechanisms is established, and the nonlinear dynamic characteristics are studied. The clearance joint entity is equivalent to a T-type beam model. For the radial and lateral collision at the ends of two sides, a detection algorithm for collision points is proposed for the first time. The analysis models for the nonlinear contact force and friction corresponding to different collision types are established, and the equivalent force at the collision points is applied to the T-type beam model. The dynamic characteristics of the T-type beam model under axial impact loads are analyzed, and the results are compared with the analysis results from the ANSYS software, by which the effectiveness of the nonlinear dynamic model for clearance joints is verified. The dynamic response characteristics of a deployable truss structure with multiple clearance joints are analyzed, and the influence mechanisms of the clearance joints on the dynamic responses are investigated. The results show that the nonlinear dynamic responses of deployable truss structures can be analyzed more precisely by using the dynamic model with clearance joints, which can provide support for the dynamic design of deployable truss structures.
Keywords:space deployable mechanism  clearance joint  nonlinear dynamics  detection algorithm for collision
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