卫星间链路(ISL)系统中立方体卫星微带天线与翻滚仿真

2018 International Conference on Control, Electronics, Renewable Energy and Communications (ICCEREC) Pub Date : 2018-12-01 DOI:10.1109/ICCEREC.2018.8712100

Fariz Henzal Bafadhal, B. S. Nugroho, H. Wijanto

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引用次数: 0

摘要

考虑到卫星轨道运行时的翻滚情况，卫星间链路(ISL)系统中立方体卫星的天线设计具有很大的挑战性。微带天线是一种尺寸小、重量轻、满足立方体卫星要求的天线。其简单的结构简化了装配和调整过程与立方体卫星的条件。拟议的ISL系统将在近地轨道(600-1000公里)上运行。在近地轨道上经常发生离子旋转，通常称为法拉第旋转效应，它会导致极化损失因子(PLF)。天线设计采用截断贴片产生圆极化。在天线下方放置电磁带隙(EBG)以抑制表面电流并减小旁瓣和后瓣。电磁带隙(EBG)的存在增加了天线的增益，拓宽了天线的带宽。卫星原型是一颗3U卫星，由3颗钢合金制成的立方体卫星组成。通过翻滚模拟，得到了翻滚方案所需的最小高波速和增益。

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Microstrip Antenna and Tumbling Simulation for CubeSat on Inter-Satellite Link (ISL) System

Designing antenna for CubeSat on Inter-Satellite Link (ISL) system is very challenging by considering the tumbling scenario when satellite orbiting. Microstrip antenna is a type of lightweight antenna with a small dimension that meet the requirements of a CubeSat. Its simple configuration simplifies the assembly and adjustment process with the condition of the CubeSat. The propose ISL systems will orbiting on LEO orbits (600–1000 km). On the LEO orbits often occurs an ionic rotation that commonly referred as faraday rotational effect and it can cause Polarization Loss Factor (PLF). The antenna Design use truncated patch to produce circular polarization. Electromagnetic Band Gap (EBG) is placed under the antenna to suppress the surface current and reduce the side lobe and back lobe. Electromagnetic Band Gap (EBG) will increase the gain and widen the bandwidth of the antenna. The satellite prototype is a 3U satellite consist of three CubeSat made of steel alloy. The tumbling simulation produce the minimum HPBW and gain required for the tumbling scheme.

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2018 International Conference on Control, Electronics, Renewable Energy and Communications (ICCEREC)

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