• 제목/요약/키워드: Phase demodulator

검색결과 72건 처리시간 0.026초

CORDIC을 이용한 디지탈 Quadrature 복조기의 VLSI 구현 (VLSI Implementation of CORDIC-Based Digital Quadrature Demodulator)

  • 남승현;성원용
    • 한국통신학회논문지
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    • 제23권7호
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    • pp.1718-1731
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    • 1998
  • 디지탈 quadrature 복조기는 디지탈 통신 시스템에서 변조된 신호의 정확한 위상 복조를 위해 꼭 필요하다. 기존의 방법들은 주로 DDFS(Direct Digital Frequency Synthsizer)를 이용하여 캐리어를 발생시킨 후에 승산기를 이용하여 복조를 수행하였다. 그리고, DDFS에는 주로 ROM(Read Only Memory)을 사용하였는데, 높은 속도와 정확도를 요구하는 경우 ROM의 속도와 크기가 제한이 될 수있다. 이러한 점을 극복하기 위하여 CORDIC(COordinate Rotation Digital Computer) 알고리듬을 사용하여 주파수 합성은 물론 캐리어 복조까지 수행하는 방식을 제안하였다. 최적의 하드웨어 구현을 위해 제한된 단어길이에 의한 영향을 분석하였으며, 하드웨어 비용면에서 ROM을 사용하는 방법과 비교한 결과 약 1/3 정도로 면적이 줄었다. 제안된 구조를 이요한 전주문형 VLSI 구현 결과를 보인다.

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우주발사체 자세제어용 링 레이저 자이로 피에조 구동기 설계 (The Design of Path Length Controller in Ring Laser Gyroscope for Attitude Control in the space launch vehicle)

  • 김의찬;양군호
    • 항공우주기술
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    • 제9권2호
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    • pp.31-35
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    • 2010
  • The Ring Laser Gyroscope makes use of the Sagnac effect within a resonant ring cavity of a He-Ne laser and has more accuracy than the other gyros. The space launch vehicle use require the high accuracy Gyro to control and determine the altitude to deliver the satellite in the space. In this paper, The theory of the Path Length Control is explained. The electrical design of Path Length Controller is described. The Design for Path Length Controller is composed of the demodulator, integrator, phase shifter, high voltage amplifier. We apply the circuit to 28cm square ring laser gyro and get the test results.

위성 자세제어 자이로 센서 피에조 구동기 설계 (The Design of Path Length Controller in Ring Laser Gyroscope for Attitude Control in the LEO satellite)

  • 김의찬
    • 대한전자공학회:학술대회논문집
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    • 대한전자공학회 2009년도 정보 및 제어 심포지움 논문집
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    • pp.341-343
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    • 2009
  • The Ring Laser Gyroscope makes use of the Sagnac effect within a resonant ring cavity of a He-Ne laser and has more accuracy than the other gyros. The Low Earth Orbit satellite for observatory use require the high accuracy Gyro to control and determine the altitude because of the need of payload pointing accuracy. In this paper, The theory of the Path Length Control is explained. The electrical design of Path Length Controller Is described. The Design for Path Length Controller is composed of the demodulator, integrator, phase shifter, high voltage amplifier. We apply the circuit to 28cm square ring laser gyro and get the test results.

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저궤도 위성 자세제어를 위한 자이로의 광경로 제어기 설계 (The Design of Path Length Controller in Ring Laser Gyroscope for Attitude Control in the LEO satellite)

  • 김의찬;이흥호
    • 전기학회논문지
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    • 제57권2호
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    • pp.256-260
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    • 2008
  • The Ring Laser Gyro makes use of the Sagnac effect within a resonant ring cavity of A He-Ne laser and has more accuracy than the other Gyros. The Low Earth Orbit satellite for observatory use require the high accuracy Gyro to control and determine the altitude because of the need of payload pointing accuracy. In this paper, The theory of the Path Length Control is explained. The electrical design of Path Length Controller is described. The Design for Path Length Controller is composed of the demodulator, Integrator, Phase shifter, High Voltage Amplifier. We apply the circuit to 28cm square ring laser gyro and get the test results.

블라인드 신호 감청기술 (The Listen-in Technique for Blind Signals)

  • 나선필;박철순;장원
    • 한국군사과학기술학회지
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    • 제8권4호
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    • pp.102-109
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    • 2005
  • In this paper, we propose a new listen-in technique to overcome the problems and the shortcomings which could possibly meet in the previous listen-in methods to deal with the blind signal manually according to operator's decision. In the proposed listen-in method, receiving the signals, classifying the modulation types, and demodulating the signals can be done automatically without operator's intervention. We realize the listen-in technology by developing the high speed frequency tuner, the automatic modulation recognizer, and the signal demodulator. In conclusion, we confirm and show that the developed equipment has a good performance in classifying the modulation type through the computer simulation and the field test.

저궤도 위성 자세제어 센서 RLG 피에조 구동기 설계 (The Design of Path Length Controller in Ring Laser Gyroscope for Attitude Control in the LEO satellite)

  • 김의찬;이흥호
    • 전기학회논문지
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    • 제57권9호
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    • pp.1584-1588
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    • 2008
  • The Ring Laser Gyroscope makes use of the Sagnac effect within a resonant ring cavity of a He-Ne laser and has more accuracy than the other gyros. The Low Earth Orbit satellite for observatory use require the high accuracy Gyro to control and determine the altitude because of the need of payload pointing accuracy. In this paper, The theory of the Path Length Control is explained. The electrical design of Path Length Controller is described. The Design for Path Length Controller is composed of the demodulator, integrator, phase shifter, high voltage amplifier. We apply the circuit to 28cm square ring laser gyro and get the test results.

위성방송용 QPSK 복조기를 위한 DPLL구조의 Carrier Recovery Loop 설계 (Design of Carrier Recovery Loop in DPLL Structure for QPSK Demodulator Satellite Broadcasting)

  • 하창우;이완범;김형균;김환용
    • 대한전자공학회:학술대회논문집
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    • 대한전자공학회 2001년도 하계종합학술대회 논문집(5)
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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.

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Phase Control Optimization at Waveguide Crossover and Its Application to 45° Optical Hybrid for Demodulating 8DPSK Optical Signals

  • Jeong, Seok-Hwan
    • Current Optics and Photonics
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    • 제5권6호
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    • pp.711-720
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    • 2021
  • A novel optical hybrid device that doubles the multilevel demodulation resolution by adding the optical interferometer with a waveguide crossover is proposed, theoretically analyzed and experimentally verified. We report two types of all-passive phase control schemes that will be referred to as a phase compensation scheme and a phase optimization scheme. We also apply the proposed phase control schemes to a 45° optical hybrid consisting of two parallel 90° optical hybrids together with the proposed phase control scheme for demodulating 8-level differential phase shift keying optical signals. Octagonal phase response with low wavelength sensitive excess loss of <0.8 dB over 31-nm-wide spectral range will be demonstrated in the InP-based material platform.

Blind Hopping Phase Estimator in Frequency-Hopped FM and BFSK Systems

  • Kim, Myungsup;Seong, Jinsuk;Lee, Seong-Ro
    • ETRI Journal
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    • 제37권1호
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    • pp.1-10
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    • 2015
  • A blind hopping phase estimator is proposed for the demodulation of received signals in frequency-hopping spread spectrum systems. The received signals are assumed to be bandwidth limited with a shaping filter, modulated as frequency modulation (FM) or binary frequency shift keying (BFSK), and hopped by predetermined random frequency sequences. In the demodulation procedure in this paper, the hopping frequency tracking is accomplished by choosing a frequency component with maximum amplitude after taking a discrete Fourier transform, and the hopping phase estimator performs the conjugated product of two consecutive signals and moving-average filtering. The probability density function and Cramer-Rao low bound (CRLB) of the proposed estimator are evaluated. The proposed scheme not only is very simple to implement but also performs close to the CRLB in demodulating hopped FM/BFSK signals.