首页> 外文会议>IEEE International Conference on Communications >NEAR-CAPACITY TRANSCEIVER DESIGN USING EXIT-CURVE FITTING: THREE-STAGE TURBO DETECTION OF IRREGULAR CONVOLUTIONAL CODED JOINT SPHERE-PACKING MODULATION AND SPACE-TIME CODING
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NEAR-CAPACITY TRANSCEIVER DESIGN USING EXIT-CURVE FITTING: THREE-STAGE TURBO DETECTION OF IRREGULAR CONVOLUTIONAL CODED JOINT SPHERE-PACKING MODULATION AND SPACE-TIME CODING

机译:近容量收发器设计采用出口曲线配件:三级涡轮机检测不规则卷积编码联接球包装调制和时空编码

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Conventional two-stage turbo-detected schemes typically suffer from a Bit Error Rate (BER) floor, preventing them from achieving infinitesimally low BER values, especially, when the inner coding stage is of non-recursive nature. We circumvent this deficiency by proposing a three-stage turbo-detected Sphere Packing (SP) aided Space-Time Block Coding (STBC) STBC-SP scheme, where a rate-1 recursive inner precoder is employed to avoid having a BER floor. The convergence behaviour of this serially concatenated scheme is investigated with the aid of 3D Extrinsic Information Transfer (EXIT) Charts. Furthermore, the capacity of the STBC-SP scheme is shown and an algorithm is proposed for calculating a tighter upper bound on the maximum achievable bandwidth efficiency. The proposed three-stage turbo-detected scheme operates within about 1.0 dB of the capacity and within 0.5 dB of the maximum achievable bandwidth efficiency limit.
机译:常规的两级涡轮涡轮涡轮涡轮涡轮涡轮涡轮涡轮涡轮型方案通常遭受误码率(BER)地板,防止它们实现无限的低BER值,尤其是当内部编码阶段是非递归性的时。我们通过提出三阶段涡轮检测到的球体包装(SP)辅助空间 - 时间块编码(STBC)STBC-SP方案来规避这一缺陷,其中采用速率-1递归内部预调床器来避免具有BAR地板。借助于3D外在信息传输(退出)图表,研究了该串联连接方案的收敛行为。此外,示出了STBC-SP方案的容量,并且提出了一种算法,用于计算最大可实现的带宽效率的更严格的上限。所提出的三阶段涡轮涡轮检测方案在容量约1.0 dB的范围内运行,在最大可实现的带宽效率限制的0.5 dB内。

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