Cascade Control of SATCOM on the Move (SOTM) Antennas with Jacobian Operator

M. Celik, Oguz Kaan Hancioglu, S. Bogosyan, Michal Bastl, Jan Najman, R. Grepl
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Abstract

Increasing demand in SATCOM systems has led to the development of Satcom on the Move (SOTM) antennas. Performance, light weight, low cost, and high data rate are the required parameters in the designing of SOTM antenna. The designer has to make a suitable system with respect to these design parameters. With this aim, this paper proposes a 4 axes antenna capable of 3 axes stabilization to compensate for the disturbance. With adding the position controller, the antenna can point and track the satellite on the mobile platforms. Due to the singularity problem in this type of antenna, the 3 axes stabilized antenna system is used in this paper. The kinematic equations and Jacobian operator are derived for calculation of the necessary axis feedback and look angles. The Jacobian operator with MEMS sensor which is a cost-effective solution. Furthermore, we propose PI-based stabilization for the stabilization controller and PID based pointing for the position controller. To verify the proposed algorithms, different disturbances are applied to the system.
基于雅可比算子的移动卫星通信(SOTM)天线级联控制
卫星通信系统日益增长的需求导致了移动卫星通信(SOTM)天线的发展。高性能、轻量化、低成本和高数据速率是设计SOTM天线所需要的参数。设计师必须根据这些设计参数做出合适的系统。为此,本文提出了一种具有三轴稳定能力的四轴天线来补偿扰动。通过增加位置控制器,天线可以在移动平台上对卫星进行定位和跟踪。由于该类天线存在奇异性问题,本文采用三轴稳定天线系统。导出了运动学方程和雅可比算子,用于计算所需的轴反馈和视角。采用MEMS传感器的雅可比算子是一种经济有效的解决方案。此外,我们提出了基于pi的镇定控制器和基于PID的指向控制器。为了验证所提出的算法,对系统施加了不同的干扰。
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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