利用开源软件进行空间天线部署建模

S. Khoroshylov, V.K. Shamakhanov, S.E. Martyniuk, O. Sushko
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引用次数: 0

摘要

本文的目标是建立具有受电弓结构的空间天线的动态模型,并利用开源软件研究其部署过程。研究方法包括理论力学、多体动力学、计算力学和计算机建模等。本文以一种适用于小型卫星的新型网格天线作为建模对象。这种天线与其他天线最显著的不同之处在于其支撑环的设计是受电弓的形式。为了建立空间天线动力学模型并使用开源软件实现,由于结构的复杂性,对模型进行了一些简化。天线模型被表示为由铰链连接的刚柔体系统。采用绝对节点坐标法对碳纤维棒进行柔性有限元建模,使其能够模拟结构的大变形。铝铰链组件被建模为几个由传统刚性元件连接的旋转关节。这些铰链组件的主要建模属性是铰链旋转轴的刚度、位置和方向。拉伸网格产生的张力使用弹簧建模。天线展开机构的缆绳驱动被建模为作用在定义局部位置的相应元件上的负载。提出了在HotInt开源软件中建立空间天线模型以模拟反射器部署过程的算法。利用所建立的模型,对不同情况下的天线展开进行了仿真。得到了天线部署时的部署时间、v形折叠杆之间的夹角变化以及天线截面对角线杆的张力值。本文提出的方法可以使用免费软件实现,保证了建模的灵活性,减少了模型开发时间。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Modelling of space antenna deployment using open source software
The goal of this article is to develop a dynamic model of a space antenna with the pantograph structure and to study the processes of its deployment using open-source software. Methods of theoretical mechanics, multibody dynamics, computational mechanics, and computer modeling were used in the research. A mesh antenna of the novel design, which is recommended for mini-satellites, is considered as the object for modeling. The most significant difference between this antenna and others is the design of the support ring in the form of a pantograph. To develop a model of the space antenna dynamics and implement it using open-source software, some simplifications were made due to the complexity of the structure. The antenna model is represented as a system of rigid and flexible bodies connected by hinges. Carbon fiber rods are modeled with the help of a flexible finite element using the method of absolute nodal coordinates, which allows one to model large deformations of the structure. Aluminum hinge assemblies are modeled as several rotation joints connected by conventional rigid elements. The main modeled properties of these hinge assemblies are the stiffness, location, and direction of the axes of rotation of the hinges. The tension forces created by the stretched mesh are modeled using springs. The cable drive of the antenna deployment mechanism is modeled as a load acting on the corresponding elements in defined local positions. An algorithm for building a model of the space antenna to simulate the reflector deployment process in the HotInt open-source software is presented. Using the built model, antenna deployment simulations are carried out for different cases, which differ in the forces used for the deployment. Values of deployment time, variations of angles between the V-folded bars, and tensions in the diagonal rods of the antenna sections during the antenna deployment are obtained. The approach proposed in the article can be implemented using free software, ensures flexibility of modeling, and reduces the model development time.
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