The on-orbit antenna pointing calibration of Milstar satellite gimbaled parabolic antennas

H.G. Kistosturian
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引用次数: 4

Abstract

To minimize enemy jamming impacts and to maximize communications coverage of friendly forces, the modern military satellite communications systems require accurate determination of the antenna Earth coverage areas. Also, an accurate antenna pointing system is required to satisfy the link budget requirements on the edge of antenna coverage. The antenna pointing accuracy can be improved considerably by on-orbit calibration of the diurnal satellite antenna pointing misalignment error which arises from the combination of several error sources, such as structural thermal deformations, the attitude determination system, the antenna ground alignment procedure, and the antenna gimbal system. This paper describes how an approximately tenfold reduction in pointing error can be achieved from on-orbit antenna pointing calibration of the gimbaled antenna of the Milstar satellite. In addition, the paper describes the process that was implemented to achieve these results.
军星卫星框架抛物面天线在轨指向标定
为了最大限度地减少敌人的干扰影响,并最大限度地扩大友军的通信覆盖范围,现代军事卫星通信系统需要精确确定天线的地球覆盖区域。同时,为了满足天线覆盖边缘的链路预算要求,需要精确的天线指向系统。由于结构热变形、姿态确定系统、天线地面对准过程和天线云台系统等多种误差源的综合作用,对卫星天线日指向误差进行在轨定标可显著提高天线指向精度。本文介绍了如何通过对军星卫星框架天线进行在轨指向标定,使指向误差降低约十倍。此外,本文还描述了实现这些结果的过程。
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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