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首页> 外文期刊>電子情報通信学会技術研究報告. 宇宙·航行エレクトロニクス. Space, Aeronautical and Navigational Electronics >Hardware implementation and laboratory performances of X-band nano satellite high-speed downlink receiver based on turbo equalizer/decoder
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Hardware implementation and laboratory performances of X-band nano satellite high-speed downlink receiver based on turbo equalizer/decoder

机译:基于turbo均衡器/解码器的X波段纳米卫星高速下行接收机的硬件实现和实验室性能

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摘要

A high speed downlink communication system is desired for future different applications using nano satellites. We have developed an X-band downlink system for nano satellite employing Consultative Committee for Space Data Systems (CCSDS) 131.2-B-1 signaling formats with a modulation symbol rate of 100 Msps. A compact high efficiency transmitter for wideband satellite communications must be implemented. Some of the tradeoffs cause significant degradation in performances. To overcome the performance loss, a memoryless channel predistortion scheme at the transmitter and a turbo equalizer/decoder has been developed at the receiver. The receiver algorithms are now refined as fixed-point algorithms for a field programmable gate array (FPGA) implementation. Performances of a prototype receiver are evaluated from measured and simulated input IF signals. The details of the receiver implementation and performance analyses are presented in this paper.
机译:对于使用纳米卫星的未来不同应用,需要高速下行链路通信系统。我们已经开发了一种采用空间数据系统咨询委员会(CCSDS)131.2-B-1信令格式,调制符号率为100 Msps的纳米卫星X波段下行链路系统。必须实现用于宽带卫星通信的紧凑型高效发射机。一些折衷会导致性能显着下降。为了克服性能损失,在接收机处开发了无记忆信道预失真方案,并在接收机处开发了turbo均衡器/解码器。现在,将接收器算法改进为用于现场可编程门阵列(FPGA)实现的定点算法。原型接收机的性能可通过测量和模拟的输入IF信号进行评估。本文介绍了接收器实现和性能分析的详细信息。

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