• Journal of Biomedical Engineering Research
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• v.7 no.1
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• pp.67-74
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• 1986

We have implemented data compression and reconstruction by using a fast Walsh transform. The ECG signals were generated by an ECG BimLllator (KONT- RON). The sampling frequency was 480 Hz and the data point number used was 512. In order to eliminate the 60 Hz noise and baseline drift, a digital notch filter was designed. We obtaine!1 a compression ratio of 5 : 1 and at this ratio it was possible to obtain a true diagnosis and an ECG morphology analysis.

• Proceedings of the KIPE Conference
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• 2004.07b
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• pp.494-497
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• 2004

계통연계형 태양광발전 시스템의 확대보급에 따라 단독운전 검출기법의 검출 성능에 대한 검증의 필요성이 대두되고 있다. 본 논문에서는 단독운전 검출기법의 대표적인 능동적 검출기법인 무효전력 변동기법 (reactive power variation method)과 주파수 쉬프트기법(active frequency drift method)을 IEEE Std 929-2000에서 명시된 단독운전검출 시험 방법을 이용하여 단독운전검출기법의 성능 및 불검출 영역(non-detection zone)에 대하여 비교 분석하였다.

• Proceedings of the KIPE Conference
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• 2014.11a
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• pp.52-53
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• 2014

계통이 차단되었음에도 태양광 발전 시스템이 발전을 지속하는 상황을 단독운전이라 하는데, 이런 단독운전은 배전 설비의 손상, 선로 유지 및 보수자의 감전사고 우려가 있으므로 이를 신속히 인지하여 시스템을 정지시켜야 한다. 본 논문에서는 최악의 상황에서도 단독운전 현상을 신속히 검출하여 시스템을 정지시킬 수 있도록 주파수 변동을 통한 단독운전 검출 기법에 대하여 새롭게 제안하고, 이를 시뮬레이션과 실험을 통해 단독운전 검출 성능 및 정상 상태 시 PCS 출력 전력의 품질에 대하여 분석하도록 한다.

• Journal of Ocean Engineering and Technology
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• v.16 no.6
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• pp.25-31
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• 2002

A system identification method is introduced to increase the prediction accuracy of a ship's maneuverability in PMM test, analysis. To improve the accuracy of linear hydrodynamic coefficients, the analysis techniques of pure sway and yaw tests are developed, and confirmed. In the analysis of sway tests, accuracy to linear hydrodynamic coefficients depends on the frequency of sway motion. To obtain nonlinear hydrodynamic coefficients for large drift angles, a combined yaw test is introduced. Using this system identification method, runs of PMM test can be reduced while retaining sufficient accuracy, compared to the Fourier integration method. Through the comparisons with sea trial results and the Fourier integration method, the accuracy and efficiency of the newly proposed system identification method, based on least square method, has been validated.

• Proceedings of the Korean Nuclear Society Conference
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• 1998.05b
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• pp.963-966
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• 1998

The KOMAC(KOrea Multi-purpose Accelerator Complex) linac is composed of RFQ(Radio Frequency Quadrupole), CCDTL(Coupled Cavity Drift Tube Linac) and SC(Superconducting)-linac. The required CW output power of RF system is about 25㎿ for 20㎿ proton beam power. Therefore high power RF sources are necessary for cost saving and reliability improvement. The number of klystrons for 0.5 ㎿ at 350MHz and 1 ㎿ at 700MHz are 1 and 31, respectively. In this paper, the design parameters of the klystron system including power supply and energy recovery system are presented.

• Journal of Ocean Engineering and Technology
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• v.11 no.1
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• pp.95-105
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• 1997

This paper presents a Inertial Measuring Unit(IMU) for motion measurement of an AUV. The IMU is composed of three parts: inertial sensors with three servo accelerometers and three rate gyros, an analog/digital interface board, and a signal processing board with TMS320C31 DSP processor. The IMU is a class of strap-down inwetial navigation system does not applicable directly to the navigation system in consequence of the AUV and integrated sensors for an integrated navigation system of the AUV. Fast calculstion of direction cosine matrix for the coordinate transformation body to reference is obtained through the DSP processor. A switching algotrithm is used to lessen the low frequency drift effect of the gyros in the vertical plane with use of low pass filtering of the signal of the accelerometers.

• Proceedings of the IEEK Conference
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• 2000.06e
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• pp.113-116
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• 2000

In this paper presents the portable wireless ECG data detection and diagnosis system based on discreet wavelet transform. An algorithm based on wavelet transform suitable for real time implementation has been developed in order to detect ECG characteristics. In particular, QRS complex, S and T waves may be distinguished form noise, baseline drift or artifacts. Proposed telemetry system that a transmitting media using radio frequency(RF) for the middle range measurement of the physiological signals and receiving media using optical for electromagnetic interference problem. A standard hi-directional serial communication interface between the telemetry system and a personal computer or laptop, allows read-time controlling, diagnosing and monitoring of system. A portable telemetry system within a size. of 65${\times}$125${\times}$45mm consists of three parts: a digital signal processing part for physiological signal detect or diagnose, RF transmitter for data transfer and a optical receiver for command receive. Advantages of proposed telemetry system is wireless middle range(50m) FM transmission, reduce electromagnetic interference to a minimum. which enables a comfortable diagnosis system at home.

• Proceedings of the KIPE Conference
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• 2010.07a
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• pp.172-173
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• 2010

본 논문은 신 재생에너지원 중 태양광을 이용한 계통연계형 PV PCS의 단독운전 검출 성능을 극대화하고, 출력전력의 품질 외곡을 최소화 할 수 있는 개선된 능동 주파수 변이기법의 최적 외란의 크기를 모델링, 시뮬레이션 및 실험을 통하여 검증하고, 이를 근거로 계통 보호 협조 및 안전을 위한 단독운전 검출 기법의 설계방법을 제시하고자 한다.

• Proceedings of the KIPE Conference
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• 2010.07a
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• pp.381-382
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• 2010

계통 연계형 시스템은 상용계통과 연계하여 운전되기 때문에 계통 보호 협조, 전력품질, 고조파 전류의 발생, 제어, 단독운전 검출 문제 등이 해결해야 할 문제들로 제기된다. 그 중에서 특히 단독운전 검출의 경우 필요성이 요구되면서 검출의 신뢰성이 보장되는 기법들에 대한 연구가 꾸준히 진행되고 있다. 본 논문에서는 이러한 단독운전 현상을 능동적 주파수 변동 기법에서 주파수의 변화량과 cf(chopping fraction)의 변화량으로 주파수 변동의 상관관계를 이용한 새로운 단독운전 검출 기법을 제안하고 시뮬레이션을 통하여 타당성 및 유효성을 검증하였다.

• Journal of Astronomy and Space Sciences
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• v.14 no.2
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• pp.355-366
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• 1997

This paper presents a comprehensive analytical approach for determining key maneuver parameters associated with the acquisition and maintenance of the ground track for a low-earth orbit. A livearized model relating changes in the drift rate of the ground track directly to changes in the orbital semi-major axis is also developed. The effect of terrestrial atmospheric drag on the semi-major axis is also explored, being quantified through an analytical expression for the decay rate as a function of density. The non-singular Lagrange planetary equations, further simplified for nearly circular orbits, provide the desired relationships between the corrective in-plane impulsive velocity increments and the corresponding effects on the orbit elements. The resulting solution strategy offers excellent insight into the dynamics affecting the timing, magnitude, and frequency of these maneuvers. Simulations are executed for the ground track acquisition and maintenance maneuver as a pre-flight planning and analysis.