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A Study on Dynamic Characteristics of Satellite Antenna System considering 3D Revolute Clearance Joint

机译:考虑3D旋转间隙关节卫星天线系统动态特性研究

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Clearances in the joints of real mechanisms are unavoidable due to assemblage, manufacturing errors, and wear. The dual-axis driving and positioning mechanism is one kind of space actuating mechanism for satellite antenna to implement precise guidance and positioning. However, in dynamics analysis and control of the satellite antenna system, it is usually assumed that the revolute joint in the satellite antenna system is perfect without clearances or imperfect with planar radial clearance. However, the axial clearance in an imperfect revolute joint is always ignored. In this work, the revolute joint is considered as a 3D spatial clearance joint with both the radial and axial clearances. A methodology for modeling the 3D revolute joint with clearances and its application in satellite antenna system is presented. The dynamics modeling and analysis of the satellite antenna system are investigated considering the 3D revolute clearance joint. Firstly, the mathematical model of the 3D revolute clearance joint is established, and the definitions of the radial and axial clearance are presented. Then, the potential contact modes, contact conditions, and contact detection of the 3D revolute clearance joint are analyzed. Further, the normal and tangential contact force models are established to describe the contact phenomenon and determine the contact forces in the 3D revolute clearance joint. Finally, a satellite antenna system considering the 3D revolute clearance joint with spatial motion is presented as the application example. Different case studies are presented to discuss the effects of the 3D revolute clearance joint. The results indicate that the 3D revolute clearance joint will lead to more severe effects on the dynamic characteristics of the satellite antenna system. Therefore, the effects of axial clearance on the satellite antenna system cannot be ignored in dynamics analysis and design of the satellite antenna system.
机译:由于组装,制造错误和磨损,实际机制关节的间隙是不可避免的。双轴驱动和定位机构是用于卫星天线的一种空间致动机构,以实现精确的引导和定位。然而,在卫星天线系统的动态分析和控制中,通常假设卫星天线系统中的旋转接头在没有间隙或平面径向间隙的情况下完美。然而,始终忽略了不完全旋转关节的轴向间隙。在这项工作中,旋转接头被认为是具有径向和轴向间隙的3D空间间隙接头。介绍了一种用间隙建模3D旋转关节及其在卫星天线系统中的应用方法。考虑到3D旋转间隙接头,研究了卫星天线系统的动力学建模和分析。首先,建立了3D旋转间隙关节的数学模型,并提出了径向和轴向间隙的定义。然后,分析了潜在的接触模式,接触条件和3D旋转间隙关节的接触检测。此外,建立正常和切向接触力模型以描述接触现象并确定3D旋转间隙关节中的接触力。最后,作为应用示例呈现考虑具有空间运动的3D旋转间隙关节的卫星天线系统。提出了不同的案例研究以讨论3D旋转间隙关节的影响。结果表明,3D旋转间隙接头将导致对卫星天线系统的动态特性产生更严重的影响。因此,在卫星天线系统的动力学分析和设计中,不能忽视轴向间隙对卫星天线系统的影响。

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