Kinematics and Tracking Control of a Four Axis Antenna for Satcom on the Move

Oguz Kaan Hancioglu, M. Celik, U. Tumerdem
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引用次数: 8

Abstract

In this paper, we propose a 4 axis antenna which is capable of tracking satellites, through the precise real-time control of azimuth, cross-level, elevation and polarization angles. Due to the well-known gimbal lock problem in 2-3 axis antenna systems, our design has a redundant degree of freedom, and this redundancy is utilised to solve the issue of inverse kinematics around singularities. In the paper, we derive the kinematics of the 4 DOF redundant orientation mechanism and propose a method to avoid the gimbal lock issue. Also, utilising satellite position data (from TLE Database) and GPS localisation, we derive the necessary kinematics equations to position the antenna towards any visible satellite from any position on earth. Furthermore, we propose a PI-based cascade controller for tracking the satellites. To verify our analytical results we present experimental results on a 4 axis antenna test platform that we have built and compare our results with the feedback from a satellite in the form of guidance RF signals. The proposed system can find and track satellites with a 1-degree error without satellite signal feedback.
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移动卫星通信四轴天线的运动学与跟踪控制
本文提出了一种能够实时精确控制卫星方位、横向、仰角和极化角的四轴天线。由于众所周知的2-3轴天线系统的万向环锁问题,我们的设计具有冗余自由度,并利用这种冗余来解决围绕奇点的逆运动学问题。本文推导了四自由度冗余定向机构的运动学,提出了一种避免万向节锁紧问题的方法。此外,利用卫星位置数据(来自TLE数据库)和GPS定位,我们推导出必要的运动学方程,以便从地球上的任何位置将天线定位到任何可见的卫星。此外,我们还提出了一种基于pi的串级控制器来跟踪卫星。为了验证我们的分析结果,我们在我们建立的四轴天线测试平台上给出了实验结果,并将我们的结果与卫星以制导射频信号形式反馈的结果进行了比较。该系统可以在没有卫星信号反馈的情况下,发现并跟踪误差为1度的卫星。
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