Turbo coded double differential phase shift keying in aeronautical channels

C. Neeraja, S. Nandan
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Abstract

In this paper, we present the results of using a turbo decoder to retrieve a serially encoded data stream, which has been transmitted over an aeronautical channel. The transmitted data streams are Double Differential Phase Shift Keying (DDPSK) modulated signals, which are encoded using two rate one-half (1/2) recursive systematic convolutional (RSC) encoders, and then transmitted over the channel. The aeronautical channels are more affected by multipath fading and Doppler shift. The DDPSK modulation scheme is a differential modulation scheme and it can withstand Doppler shift [9]. Also the DDPSK modulation scheme does not require a carrier recovery circuit at the receiving end. The DDPSK can be extended to an nth order differential PSK, i.e. DnPSK. Results show that the performance of the DDPSK signal can be increased by using Turbo code in aeronautical channels.
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航空信道的涡轮编码双差分相移键控
在本文中,我们提出了使用涡轮解码器检索已在航空信道上传输的串行编码数据流的结果。传输的数据流是双差分相移键控(DDPSK)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。航空信道受多径衰落和多普勒频移的影响较大。DDPSK调制方案是一种差分调制方案,可以承受多普勒频移[9]。此外,DDPSK调制方案不需要在接收端使用载波恢复电路。DDPSK可扩展为n阶微分PSK,即DnPSK。结果表明,在航空信道中使用Turbo码可以提高DDPSK信号的性能。
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