• Title/Summary/Keyword: turbo

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Analysis of an Optimal Iterative Turbo Equalizer for Underwater Acoustic Communication (수중 음향통신에 적합한 최적의 반복기반 터보 등화기 분석)

  • Park, Tae Doo;Lee, Seong Ro;Kim, Beom Mu;Jung, Ji Won
    • The Journal of Korean Institute of Communications and Information Sciences
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    • v.38C no.3
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    • pp.303-310
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    • 2013
  • Underwater acoustic communication has multipath error because of reflection by sea-level and sea-bottom. The multipath of underwater channel causes signal distortion and error floor. In order to improve the performance, it is necessary to employ an iterative coding scheme. Among the iterative coding scheme, turbo codes and LDPC codes are dominant channel coding schemes in recent. This paper concluded that turbo coding scheme is optimal for underwater communications system in aspect to performance, coded word length, and equalizer combining. Also, we confirmed the performance in the environment of oceanic experimentation using turbo equalizer based on distance 5Km, data rate 1Kbps.

Optimization of energy saving device combined with a propeller using real-coded genetic algorithm

  • Ryu, Tomohiro;Kanemaru, Takashi;Kataoka, Shiro;Arihama, Kiyoshi;Yoshitake, Akira;Arakawa, Daijiro;Ando, Jun
    • International Journal of Naval Architecture and Ocean Engineering
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    • v.6 no.2
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    • pp.406-417
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    • 2014
  • This paper presents a numerical optimization method to improve the performance of the propeller with Turbo-Ring using real-coded genetic algorithm. In the presented method, Unimodal Normal Distribution Crossover (UNDX) and Minimal Generation Gap (MGG) model are used as crossover operator and generation-alternation model, respectively. Propeller characteristics are evaluated by a simple surface panel method "SQCM" in the optimization process. Blade sections of the original Turbo-Ring and propeller are replaced by the NACA66 a = 0.8 section. However, original chord, skew, rake and maximum blade thickness distributions in the radial direction are unchanged. Pitch and maximum camber distributions in the radial direction are selected as the design variables. Optimization is conducted to maximize the efficiency of the propeller with Turbo-Ring. The experimental result shows that the efficiency of the optimized propeller with Turbo-Ring is higher than that of the original propeller with Turbo-Ring.

Comparison of EXIT chart generation for LDPC and turbo codes (시뮬레이션 기법을 이용한 LDPC 부호와 터보부호에 대한 EXIT 차트 생성 비교)

  • Nyamukondiwa, Ramson Munyaradzi;Kim, Sooyoung
    • Journal of Satellite, Information and Communications
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    • v.10 no.3
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    • pp.73-77
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    • 2015
  • In this paper, we present two simulation methods to investigate the effect of excluding bit errors on generating the extrinsic information transfer (EXIT) chart for low density parity check (LDPC) and turbo codes. We utilized the simulation methods including and excluding bit errors to generate EXIT chart which was originally proposed for turbo codes. The generated EXIT charts for LDPC and turbo codes shows that the presented methods appropriately demonstrates the performance behaviours of iterative decoding for LDPC and turbo codes. Analysis on the simulation results demonstrates that the EXIT chart excluding the bit errors shows only a small part of the curves where the amount of information is too large.

Development of An Integrated Controller for a Direct Drive Turbo Compressor (직접 구동방식 터보 압축기를 위한 통합 제어기 개발)

  • 권정혁;변지섭;최중경
    • Journal of the Institute of Electronics Engineers of Korea SC
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    • v.40 no.4
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    • pp.225-234
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    • 2003
  • Turbo compressors need high speed rotating impeller in structure, high rate gearbox and conventional induction motor. This mechanical system increased moment of inertia and mechanical friction loss. Recently turbo compressor has adopted a super high-speed motor and driver and have made its size smaller and mechanical friction loss at minimum. In this paper, variable super high - speed motor controller, compressor controller and MMI controller are implemented with only one DSP (TMS320VC33) chip for a 150HP, 70,000rpm direct drive turbo compressor. It was required hardware and software integration. The result of integration, Controller hardware became simple and all control software are developed same developing tool. The implements turbo compressor meets the requirements.

The Study on Vibration Isolation of Industrial Turbo-fan (산업용 터보팬의 진동절연에 관한 연구)

  • Park, Ik-Pil;Kim, Dong-Young;Kwon, Yong-Soo;Ahn, Chan-Woo
    • Proceedings of the KSME Conference
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    • 2001.11a
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    • pp.609-615
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    • 2001
  • A turbo-fan is easily exposed to noise and vibration as against other industrial machines and the majority of them is subject to be damaged by vibration. The most usual problem of vibration in a turbo-fan is resonance so the case of being composed of iron sheet structure with low strength like a turbo-fan should be taken seriously. In this paper, FFT(Fast Fourier Transform) and Order tracking method were used to analyze factors of vibration in a turbo-fan and hereby with proper selection of vibration isolator, we wanted to reduce vibration of base. After Order tracking, we knew resonance occurred in rotational frequency 23 Hz(1400 rpm) at the casing and the bearing. After the test of base vibration using vibration isolators, the spring isolator was more effective than the robber isolator in the base vibration and the vibration isolating is more effective in the case that the isolating pad is adhered to the bottom of the isolating spring.

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Pool Boiling Heat Transfer Coefficients of R1234yf on Various Enhanced Surfaces (열전달 촉진 표면에서 R1234yf의 풀 비등 열전달계수)

  • Lee, Yohan;Kang, Dong Gyu;Seo, Hoon;Jung, Dongsoo
    • Korean Journal of Air-Conditioning and Refrigeration Engineering
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    • v.25 no.3
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    • pp.143-149
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    • 2013
  • In this work, nucleate pool boiling heat transfer coefficients (HTCs) of R134a and R1234yf are measured, on flat plain, 26 fpi low fin, Turbo-B, Turbo-C and Thermoexcel-E surfaces. All data are taken at the liquid pool temperature of $7^{\circ}C$, on a small square copper plate ($9.53mm{\times}9.53mm$), at heat fluxes from $10kW/m^2$ to $200kW/m^2$, with an interval of $10kW/m^2$. Test results show that nucleate boiling HTCs of all enhanced surfaces are greatly improved, as compared to that of a plain surface. Nucleate pool boiling HTCs of R1234yf are very similar to those of R134a, for the five surfaces tested.

A Novel Adaptive Turbo Receiver for Large-Scale MIMO Communications

  • Chang, Yu-Kuan;Ueng, Fang-Biau;Tsai, Bo-Yi
    • KSII Transactions on Internet and Information Systems (TIIS)
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    • v.12 no.7
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    • pp.2998-3017
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    • 2018
  • Massive (large-scale) MIMO (multiple-input multiple-output) is one of the key technologies in next-generation wireless communication systems. This paper proposes a high-performance low-complexity turbo receiver for SC-FDMA (single-carrier frequency-division multiple access) based MMIMO (massive MIMO) systems. Because SC-FDMA technology has the desirable characteristics of OFDMA (orthogonal frequency division multiple access) and the low PAPR (peak-to-average power ratio) of SC transmission schemes, the 3GPP LTE (long-term evolution) has adopted it as the uplink transmission to meet the demand high data rate and low error rate performance. The complexity of computing will be increased greatly in base station with massive MIMO (MMIMO) system. In this paper, a low-complexity adaptive turbo equalization receiver based on normalized minimal symbol-error-rate for MMIMO SC-FDMA system is proposed. The proposed receiver is with low complexity than that of the conventional turbo MMSE (minimum mean square error) equalizer and is also with better bit error rate (BER) performance than that of the conventional adaptive turbo MMSE equalizer. Simulation results confirm the effectiveness of the proposed scheme.

The Development of the Turbo Generator System with Direct Driving High Speed Generator (고속 발전기 직접 구동 방식의 터보 제너레이터 시스템 개발)

  • 노민식;박승엽
    • Journal of the Institute of Electronics Engineers of Korea SC
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    • v.40 no.6
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    • pp.87-94
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    • 2003
  • This paper presents results of the development of the turbo generator system with structure which is HSG(High Speed Generator) installed directly to gas-turbine engine. Turbo generator with a high speed motor-generator directly has many advantages aspects of weight, size, lubrication system and complexity of the system compared of conventional turbo generator system with a gear box. But because of direct high speed operation of the high speed generator, we have to need stable high speed motor driving algorithm for perfect engine ignition when engine start. Also we have to need the design of the Power conditioning unit(PCU) for converting high speed AC output power to conventional AC power or needed DC power.

Performance of Turbo Codes in the Direct Detection Optical PPM Channel (직접 검파 펄스 위치 변조 광통신 채널에서의 터보 부호의 성능)

  • 이항원;이상민
    • The Journal of Korean Institute of Communications and Information Sciences
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    • v.28 no.6C
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    • pp.570-579
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    • 2003
  • The performance of turbo codes is investigated in the direct detection optical PPM channel. We assume that an ideal photon counter is used as an optical detector and that the channel has background noise as well as quantum noise. Resulting channel model is M-ary PPM Poisson channel. We propose the structure of the transmitter and receiver for applying turbo codes to this channel. We also derive turbo decoding algorithm for the proposed coding system, by modifying the calculation of the branch metric inherent in the original turbo decoding algorithm developed for the AWGN channel. Analytical bounds are derived and computer simulation is performed to analyze the performance of the proposed coding scheme, and the results are compared with the performances of Reed-Solomon codes and convolutional codes.

A 18-Mbp/s, 8-State, High-Speed Turbo Decoder

  • Jung Ji-Won;Kim Min-Hyuk;Jeong Jin-Hee
    • Journal of electromagnetic engineering and science
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    • v.6 no.3
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    • pp.147-154
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    • 2006
  • In this paper, we propose and present implementation results of a high-speed turbo decoding algorithm. The latency caused by (de) interleaving and iterative decoding in a conventional maximum a posteriori(MAP) turbo decoder can be dramatically reduced with the proposed design. The source of the latency reduction is come from the combination of the radix-4, dual-path processing, parallel decoding, and rearly-stop algorithms. This reduced latency enables the use of the turbo decoder as a forward error correction scheme in real-time wireless communication services. The proposed scheme results in a slight degradation in bit-error rate(BER) performance for large block sizes because the effective interleaver size in a radix-4 implementation is reduced to half, relative to the conventional method. Fixed on the parameters of N=212, iteration=3, 8-states, 3 iterations, and QPSK modulation scheme, we designed the adaptive high-speed turbo decoder using the Xilinx chip (VIRTEX2P (XC2VP30-5FG676)) with the speed of 17.78 Mb/s. From the results, we confirmed that the decoding speed of the proposed decoder is faster than conventional algorithms by 8 times.