• Proceedings of the IEEK Conference
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• 2000.09a
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• pp.907-910
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• 2000

QPSK 복조기는 위상 오차에 따른 문제점을 극복하기 위해 수신단에서는 반송파의 주파수와 위상을 tracking 하는 Carrier recovery loop부분이 필요하다〔1〕. Carrier recovery loop는 multiplier, arm filter, matched filter, decimator, loop filter, NCO로 구성이 된다〔2〕.기존 Carrier recovery loop의 NCO는 sine과 cosine의 lookup table을 갖는 구조로 되어있어, 전력소모가 크다는 문제점을 가지고 있다. 따라서 본 논문에서는 lookup table을 사용하지 않는 저 전력 구조의 QPSK복조기의 Carrier recovery loop의 NCO를 설계했다.

• The Journal of Korean Institute of Communications and Information Sciences
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• v.19 no.11
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• pp.2067-2080
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• 1994

Recently, joint blind equalization and carrier recovery for digital mobile transmission system is of growing interest. In this paper, we describe new receiver structure of joint godard blind equalizer and various recovery loop for QAM modulated signal. After a brief review of Godard blind equalizer and MAP estimation Costas loop, Generalized Costas loop, Leclert loop, Angular form loop, we present two kinds of receiver structures for joint blind equalization and carrier recovery. Using a Monto Carlo simulation technique, we can confirm that two kinds of receiver structures operate very well in the steady state.

• The Journal of Korean Institute of Communications and Information Sciences
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• v.33 no.4A
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• pp.440-449
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• 2008

In this paper, we propose a 16-QAM carrier recovery loop which is suitable for the implementation of Inmarsat M4 system receiver. Because the frequency offset of ${\pm}924\;Hz$ on signal bandwidth 33.6 kHz is recommended in Inmarsat M4 system specification, carrier recovery loop having stable operation in the channel environment with large relative frequency offset is required. the carrier recovery loop which adopts only PLL can't be stable in relatively large frequency offset environment. Therefore, we propose a carrier recovery loop which has stable operation in large relative frequency offset environment for Inmarsat M4 system. The proposed carrier recovery loop employed differential filter-based noncoherent UW detector which is robust to frequency offset, CP-AFC for initial frequency offset acquisition using UW signal, and 16-QAM DD-PLL for phase tracking using data signal to overcome large relative frequency offset and achieve stable carrier recovery performance. Simulation results show that the proposed carrier recovery loop has stable operation and satisfactory performance in large relative frequency offset environment for Inmarsat M4 system.

• Proceedings of the IEEK Conference
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• 2000.11a
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• pp.85-88
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• 2000

In order to resolve problems according to the phase error in QPSK demodulator of the digital communication systems. The demodulator requires carrier recovery loop which searches for the frequency and phase of the carrier. In this paper the complexity of implementation is reduced by the reduction into half of the number of the multiplier in filter structure of the conventional carrier recovery loop, and as the drawback of NCO of the conventional carrier recovery loop wastes a amount of power for the structure of lookup table , We designed the structure of combinational logic without the lookup table. In the comparison with dynamic power of the proposed NCO, the power of NCO with the lookup table is 175㎼, NCO with the proposed structure is 24.65㎼. As the result, it is recognized that about one eight of loss power is reduced. In the simulation of carrier recovery loop designed QPSK demodulator, it is known that the carrier phase is compensated.

• Proceedings of the IEEK Conference
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• 2001.06e
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• pp.165-168
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• 2001

In this W the complexity of implementation is reduced by the reduction into half of the number of the multiplier in filter structure of the conventional carrier recovery loop, and as the drawback of NCO of the conventional carrier recovery loop wastes a amount of power for the structure of lookup table, We designed the structure of combinational logic without the lookup table. In the comparison with dynamic power of the proposed NCO, the power of NCO with the lookup table is 175${\mu}$W, NCO with the proposed of structure is 24,65${\mu}$W. As if result, it is recognized that about one eight of loss power is reduced In the simulation of carrier recovery loop designed QPSK demodulator, it is known that the carrier phase is compensated.

• Journal of the Korean Institute of Telematics and Electronics C
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• v.36C no.2
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• pp.62-67
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• 1999

Phase rotational is a practical problem in the implementation of coherent demodulation. Large phase noise may intorduce phase rotation in the demodulator which results in repeated decision errors. This paper presents a simple and yet very efficient technique in building a carrier recovery loop which minimizes the phase rotation by improving the stability of the decision-directed carrier recovery loop. Simulation shows this novel technique improves the performance of the carrier recovery loop as well as stability.

• Journal of the Korean Institute of Telematics and Electronics A
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• v.30A no.11
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• pp.1-10
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• 1993

A Study on New Digital In this paper, we propose a new Angular Form Carrier Recovery Loop(AFCR loop) for PSK modulation technique. AF CR loop includes detected angle symbol and Multi Level Hardlimiter. Using zero crossing DPLL, we model 1st 2nd AF CR loop, and also derive SCurve. In order to prove steady state operation of AF CR loop, we evaluate performance of this loop by Monte-Carlo and analytical simulation method. We also compare the performance of AF CR loop to that of other loop in terms of acquisition, S-Curve, and RMS jitter. From the comparison result, we verify that the performance of AF CR loop operates well in steady state.

• Journal of the Korea Institute of Information and Communication Engineering
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• v.11 no.4
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• pp.773-778
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• 2007

In order to resolve problems with the phase error in QPSK demodulator of the digital satellite broadcasting systems, the demodulator requires carrier recovery loop which searches for the frequency and phase of the carrier. In this paper the complexity of implementation is reduced by the reduction into half of the number of the multiplier in Inter structure of the conventional carrier recovery loop, and as the drawback of NCO of the conventional carrier recovery loop wastes a amount of power for the structure of lookup table, We designed the structure of combinational logic without the lookup table. In the comparison with dynamic power of the proposed NCO, the power of NCO with the lookup table is $175{\mu}W$, NCO with the proposed structure is $24.65{\mu}W$. As the result, it is recognized that about one eight of loss power is reduced. In the simulation of carrier recovery loop designed QPSK demodulator, it is known that the carrier phase is compensated.

• The Journal of Korean Institute of Communications and Information Sciences
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• v.26 no.11B
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• pp.1565-1573
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• 2001

In order to resolve problems according to the phase error in QPSK demodulator in the digital satellite broadcasting, the demodulator requires carrier recovery loop which searches for the frequency and phase of the carrier. In this paper the drawback of NCO of the conventional carrier recovery loop is to wastes a amount of power for the structure of Look-up table , we designed the structure of combinational logic without the Look-up table. In the comparison with dynamic power of the proposed NCO, the power of NCO with the Look-up table is 175[${\mu}$W], NCO with the proposed structure is 24.65[${\mu}$W]. As the result, it is recognized that loss power is reduced about one eighth. In the simulation of carrier recovery loop designed QPSK demodulator, it is known that the carrier phase is compensated.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.39 no.1
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• pp.56-62
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• 2011

A Satellite transponder is mounted on the Satellite and performs radio communications with the ground station. A Digital transponder compared to The analog transponder is made easy and accurate performance prediction. Also Modulation Scheme, Data Rate, Loop Bandwidth, Modulation Index and etc. can be changed on orbit, by implementing FPGA can reduce the weight and volume. The core technology of digital transponder is Carrier Recovery loop. Dynamic Range, Frequency Tracking Range, Frequency Tracking Rate and Coherent performance are determined by the performance of the Carrier Recovery loop. In this paper, we proposed the structure of Carrier Recovery loop for the Satellite digital transponder, then tested and verified the structure.