Multi mission low earth orbit equatorial satellite for Indonesian regions

E. N. Nasser
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引用次数: 8

Abstract

Low earth orbit (LEO) equatorial satellite has become a favorable option for developing countries like Indonesia. Low propagation delay, low transmission power and also low cost in term of satellite development and launch are the main attraction of the LEO satellite system. In this paper, we propose multi mission satellite LEO equatorial satellite for telecommunication, surveillance and vessel monitoring based on AIS (Automatic Identification System). First iteration was the tradeoff between communication payload mission and other missions in defining the orbit constellation type and altitude. Simulation was done for orbit constellation, orbit environment, antenna pattern, and coverage analysis. The simulation result will become input for link budget calculation, ITU constraint (PFD and EPFD) and handover mechanism scheme selection. The result shows that single plane 1500 km LEO equatorial with 14 satellites was able to provide dual satellite diversity for all Indonesian region. It also shows that C-band and Ku-band Frequency will exceed the EPFD limit with 10 dbi antenna gain and 30 W transmit power. The optimum configuration of Ext C-band with hemispherical patch antenna shows that the minimum fading margin > 1 dB is required to implement the hard handover scheme.
印尼地区多任务近地轨道赤道卫星
近地轨道(LEO)赤道卫星已成为印度尼西亚等发展中国家的有利选择。低传播延迟、低传输功率以及卫星研制和发射的低成本是低轨道卫星系统的主要吸引力。本文提出了一种基于AIS(自动识别系统)的多任务低轨道赤道卫星,用于通信、监视和船舶监测。第一次迭代是在通信载荷任务和其他任务之间进行权衡,确定轨道星座类型和高度。进行了轨道星座仿真、轨道环境仿真、天线方向图仿真和覆盖分析。仿真结果将作为链路预算计算、ITU约束(PFD和EPFD)和切换机制方案选择的输入。结果表明,单平面1500 km近地轨道赤道带14颗卫星可为印尼全境提供双星分异。当天线增益为10 dbi,发射功率为30 W时,c波段和ku波段频率将超过EPFD极限。采用半球形贴片天线的Ext c波段优化配置表明,实现硬切换方案需要最小衰落余量> 1 dB。
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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