航空信道turbo编码BPSK的性能研究

I. Fofanah, A. Cole-Rhodes, R. Dean
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引用次数: 0

摘要

在本文中,我们提出了使用涡轮解码器检索串行编码数据流的结果,该数据流已在多径信道上传输。传输的数据流是二进制相移键控(BPSK)调制信号,使用两个速率二分之一(1/2)递归系统卷积(RSC)编码器进行编码,然后在信道上传输。航空信道是一个快速衰落和时变的信道,它被建模为一个由多普勒和多径决定的复杂信道增益的FIR滤波器。在接收端,我们利用turbo解码来估计信道对传输数据的影响。仿真结果比较了Turbo解码后的BPSK与未编码的BPSK在A WGN和时不变多径信道上发送的误码率。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Performance of turbo coded BPSK for an aeronautical channel
In this paper, we present the results of using a turbo decoder to retrieve a serially encoded data stream, which has been transmitted over a multipath channel. The transmitted data streams are Binary Phase Shift Keying (BPSK) modulated signals, which are encoded using two rate one-half (1/2) recursive systematic convolutional (RSC) encoders, and then transmitted over the channel. An aeronautical channel is very fast fading and time varying, and it has been modeled as an FIR filter with complex channel gains determined by Doppler and the multipath. At the receiver, we utilize turbo decoding to estimate the effect of the channel on the transmitted data. Simulation results are provided comparing the bit error rates of Turbo decoded BPSK to that of un-coded BPSK sent over an A WGN and a time-invariant multipath channel.
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