Kinematics modeling analysis of the geostationary satellite monitoring antenna system

D. X. Bien, P. Hoang, LeDang Hung, D. M. Tung, Nguyen Tai-Hoai Thanh, N. H. Phong, Vuong Tien Trung, P. Tuan
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引用次数: 1

Abstract

The trend of scientific development in the future cannot fail to mention the great influence of the space field, but in the immediate future, the observational satellite systems are related to communication technology. In fact, in some countries with strong development of communication technology and space technology, the mechanical system of geostationary satellite monitoring antennas has certainly been thoroughly resolved. However, because of a specific technology, the sharing and transferring of design and manufacturing technology to developing countries is a great challenge. It is almost difficult to find published works related to mechanical design calculation and manufacture of geostationary satellite monitoring antenna systems. The problem of proactive grasping of technology, step by step autonomy in manufacturing technology of telecommunications equipment related to space technology has always been the goal of developing countries like Vietnam to limit technology dependence, minimizing technology transfer costs, ensuring national security. The first step in these problems is the autonomous construction of terrestrial transceivers such as geostationary satellite monitoring antennas. This paper presents the kinematics modeling analysis of the mechanical system of the geostationary satellite monitoring antenna. Each component of the antenna system is assumed a rigid body. The mathematical model is built based on multi-bodies kinematics and dynamics theory. The DENAVIT-HARTENBERG (D-H) homogeneous matrix method was used to construct the kinematics equations. The forward kinematics problem is analyzed to determine the position, velocity, acceleration, and workspace of the antenna system with given system motion limits. The inverse kinematics problem is mentioned to determine the kinematics behaviors of the antenna system with a given motion path in the workspace. The numerical simulation results kinematics were successfully applied in practice, especially for dynamics and control system analysis of geostationary satellite antenna systems.
静止卫星监测天线系统运动学建模分析
未来科学发展的趋势不能不提到空间领域的巨大影响,但在不久的将来,观测卫星系统与通信技术有关。事实上,在一些通信技术和空间技术发展较强的国家,对地静止卫星监测天线的机械系统肯定已经得到了彻底的解决。然而,由于技术的特殊性,设计和制造技术向发展中国家的共享和转让是一个巨大的挑战。与地球同步卫星监测天线系统的机械设计、计算和制造相关的出版著作几乎很难找到。主动掌握技术,逐步自主制造与空间技术相关的电信设备技术,一直是越南等发展中国家限制技术依赖、降低技术转移成本、保障国家安全的目标。解决这些问题的第一步是自主构建地球同步卫星监测天线等地面收发器。本文对静止卫星监测天线的机械系统进行了运动学建模分析。假设天线系统的每个部件都是刚体。基于多体运动学和动力学理论建立了该系统的数学模型。采用DENAVIT-HARTENBERG (D-H)齐次矩阵法构建运动学方程。分析了天线系统的正运动学问题,在给定系统运动极限的情况下确定天线系统的位置、速度、加速度和工作空间。为了确定天线系统在工作空间中给定运动路径时的运动学行为,提出了逆运动学问题。运动学的数值模拟结果已成功地应用于实际,特别是对地球同步卫星天线系统的动力学和控制系统分析。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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