• Title/Summary/Keyword: power space

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Influence of Electrical Aging on Space Charge Dynamics of Oil-Impregnated Paper Insulation under AC-DC Combined Voltages

  • Wang, Yan;Li, Jian;Wu, Sicheng;Sun, Peng
    • Journal of Electrical Engineering and Technology
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    • 제8권6호
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    • pp.1512-1519
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    • 2013
  • Oil-impregnated paper is a major type of insulation used in oil-filled converter transformers for both traditional and new energy systems. This paper presents and analyzes the results of the experiment conducted on the electrical aging of oil-impregnated paper under AC-DC combined voltages using the pulsed electro-acoustic (PEA) technique. The formation and dynamics of space charge affected the performance of insulation material. The electrical aged oil-paper insulation was obtained through electrical aged experiments under the voltages. Based on the PEA technique, measurements were carried out when the oil-paper insulation system was subjected to different stressing and aging times. The space charge dynamics in the bulk of the oil-paper insulation system with different aging times were measured and analyzed. Characteristic parameters such as the total charge injection amount, the total charges of fast moving and slow moving, and the distortion factor of electric field were calculated and discussed. Results show that the longer electrical aging time, the more charges trapped in the bulk of aging sample. It leads to larger distortion factor of electric field in the bulk of aging samples and accelerate degradation of oil-paper insulation under AC-DC combined voltages.

Thermal and telemetry module design for satellite camera

  • Kong, Jong-Pil;Yong, Sang-Soon;Heo, Haeng-Pal;Kim, Young-Sun;Youn, Heong-Sik
    • 대한원격탐사학회:학술대회논문집
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    • 대한원격탐사학회 2002년도 Proceedings of International Symposium on Remote Sensing
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    • pp.229-234
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    • 2002
  • Under the hostile influence of the extreme space environmental conditions due to the deep space and direct solar flux, the thermal control in space applications is especially of major importance. There are tight temperature range restrictions for electro-optical elements while on the other hand there are low power consumption requirements due to the limited energy sources on the spacecraft. So, we usually have strong requirement of thermal and power control module in space applications. In this paper, the design concept of a thermal and power control module in the MSC(Multi-Spectral Camera) system which will be a payload on KOMPSATII is described in terms of H/W & S/W. This thermal and power control module, called THTM(Thermal and Telemetry Module) in MSC, resides inside the PMU(Payload Management Unit) which is responsible for the proper management of the MSC payload for controlling and monitoring the temperature insides the EOS(Electro-Optic System) and gathering all the analog telemetry from all the MSC sub-units, etc. Particularly, the designed heater controller has the special mode of "duty cycle" in addition to normal closed loop control mode as usual. THTM controls heaters in open loop according to on/off set time designed through analysis in duty cycle mode in case of all thermistor failure whereas it controls heaters by comparing the thermistor value to temperature based on closed loop in normal mode. And a designed THTM provides a checking and protection method against the failure in thermal control command using the test pulse in command itself.

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소형 연료전지 무인기의 전기추진시스템용 전력원 모델링 및 시뮬레이션 (A Electric Power Source Modeling and Simulation for Electric Propulsion Systems of a Fuel Cell Powered Small UAV)

  • 이보화;박부민;김춘택;김성욱;양수석;안석민
    • 한국항공우주학회지
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    • 제39권10호
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    • pp.959-965
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    • 2011
  • 본 논문에서는 소형 무인기의 전기추진 시스템에 대한 모델링 및 전력 시뮬레이션에 관하여 기술하였다. 각 전력원 모델링 및 시뮬레이션을 위해 Matlab/Simulink를 사용하였고, 연료전지와 배터리를 주 전력원으로 사용하는 200 W급 전기추진 시스템에 대하여 4시간 30분의 비행 시험결과와 시뮬레이션 한 결과를 비교하였다. 그 결과, 시뮬레이션은 각 전력원의 성능 및 동특성을 적절히 모사하였고, 이를 통해 다른 급의 전기추진 시스템에 대한 전력특성변화를 예측하는 도구로 활용 가능함을 알 수 있었다.

위성용 고 신뢰성 Proto-type 보조전원 공급기 개발 (High Reliability Proto-type Auxiliary Power Supply Development for Satellite)

  • 추원교;김현구;우형제;구자춘
    • 한국항공우주학회지
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    • 제38권1호
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    • pp.94-98
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    • 2010
  • 위성용 보조전원 공급기는 임무기간 운용 중 위성체 부하에 전원을 안정적으로 공급하여야 한다. 이 보조전원 공급기는 고 신뢰성을 위해 몇가지 제한 사항을 요구한다. 본 논문에서는 이 제한 사항을 모두 만족 시키도록 보조전원 공급기를 설계하였다. 또 보조전원 공급기를 제어하는 회로는 다수결 판정회로를 사용하여 단일 기점 결함이 없도록 설계하였으며, 이를 증명하기 위해 견본을 제작하였고, 시험되었다.

태양광 발전 시스템에서의 벅 컨버터 제어기 설계 (Design of Buck Converter Controller in a Photovoltaic Power Conditioning System)

  • 박봉희;정승환;최주엽;최익;이상철;이동하
    • 한국태양에너지학회 논문집
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    • 제34권2호
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    • pp.1-7
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    • 2014
  • Generally, buck converter controller is designed to control the output voltage of the converter. However, design of the controller in a photovoltaic power conditioning system is different from theoretical design guideline. The controller in a photovoltaic power conditioning system controls the input voltage of the converter (the output voltage of the solar cell) to meet a maximum power point tracking (MPPT) performance. In this study, a new model for buck converter used in a photovoltaic power conditioning system is proposed, which is linearized after state-space averaging in each period. Also, mathematical expression of the modeled buck converter is interpreted separately as small and large signals; therefore its appropriateness is measured to design linear voltage and current controller.

무인항공기용 전원모니터링장치 설계 및 검증에 관한 연구 (A Study on Design and Verification of Power Monitoring Unit for Unmanned Aerial Vehicle)

  • 우희채;김용태
    • 한국항공우주학회지
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    • 제48권4호
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    • pp.303-310
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    • 2020
  • 본 논문은 무인항공기 전기시스템을 위한 전원모니터링장치에 대해서 기술하고 있으며, 무인항공기에 장착되는 AC/DC 발전기, 전원변환기, 배터리 및 기어박스의 데이터 측정과 임무장비의 전원 ON/OFF 장치를 운용하는 전원모니터링장치에 대한 설계를 기술하였다. 전원모니터링장치는 비행체 전원(발전기, 전원변환기 및 배터리)에 대한 전압과 전류를 측정하고, 기어박스의 압력과 온도를 측정하며, 임무컴퓨터로부터 수신된 임무장비의 전원명령을 수행한다. 전원모니터링장치는 무인항공기 비행체 요구사항을 만족하도록 설계하였으며, 구조/열 해석, 환경/EMI 및 지상/비행시험을 통하여 검증을 수행하였다.

POWER SPECTRUM ANALYSIS OF THE OMC1 IMAGE AT 1.1MM WAVELENGTH

  • Youn, So-Young;Kim, Sung-Eun
    • 천문학회지
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    • 제45권4호
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    • pp.93-99
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    • 2012
  • We present a 1.1mm emission map of the OMC1 region observed with AzTEC, a new large-format array composed of 144 silicon-nitride micromesh bolometers, that was in use at the James Clerk Maxwell Telescope (JCMT). These AzTEC observations reveal dozens of cloud cores and a tail of filaments in a manner that is almost identical to the submillimeter continuum emission of the entire OMC1 region at 450 and $850{\mu}m$. We perform Fourier analysis of the image with a modified periodogram and the density power spectrum, which provides the distribution of the length scale of the structures, is determined. The expected value of the periodogram converges to the resulting power spectrum in the mean squared sense. The present analysis reveals that the power spectrum steepens at relatively smaller scales. At larger scales, the spectrum flattens and the power law becomes shallower. The power spectra of the 1.1mm emission show clear deviations from a single power law. We find that at least three components of power law might be fitted to the calculated power spectrum of the 1.1mm emission. The slope of the best fit power law, ${\gamma}{\approx}-2.7$ is similar to those values found in numerical simulations. The effect of beam size and the noise spectrum on the shape and slope of the power spectrum are also included in the present analysis. The slope of the power law changes significantly at higher spatial frequency as the beam size increases.

Modeling and Direct Power Control Method of Vienna Rectifiers Using the Sliding Mode Control Approach

  • Ma, Hui;Xie, Yunxiang;Sun, Biaoguang;Mo, Lingjun
    • Journal of Power Electronics
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    • 제15권1호
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    • pp.190-201
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    • 2015
  • This paper uses the switching function approach to present a simple state model of the Vienna-type rectifier. The approach introduces the relationship between the DC-link neutral point voltage and the AC side phase currents. A novel direct power control (DPC) strategy, which is based on the sliding mode control (SMC) for Vienna I rectifiers, is developed using the proposed power model in the stationary ${\alpha}-{\beta}$ reference frames. The SMC-based DPC methodology directly regulates instantaneous active and reactive powers without transforming to a synchronous rotating coordinate reference frame or a tracking phase angle of grid voltage. Moreover, the required rectifier control voltages are directly calculated by utilizing the non-linear SMC scheme. Theoretically, active and reactive power flows are controlled without ripple or cross coupling. Furthermore, the fixed-switching frequency is obtained by employing the simplified space vector modulation (SVM). SVM solves the complicated designing problem of the AC harmonic filter. The simplified SVM is based on the simplification of the space vector diagram of a three-level converter into that of a two-level converter. The dwelling time calculation and switching sequence selection are easily implemented like those in the conventional two-level rectifier. Replacing the current control loops with power control loops simplifies the system design and enhances the transient performance. The simulation models in MATLAB/Simulink and the digital signal processor-controlled 1.5 kW Vienna-type rectifier are used to verify the fast responses and robustness of the proposed control scheme.

Spectral Analysis of Geomagnetic Activity Indices and Solar Wind Parameters

  • Kim, Jung-Hee;Chang, Heon-Young
    • Journal of Astronomy and Space Sciences
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    • 제31권2호
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    • pp.159-167
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    • 2014
  • Solar variability is widely known to affect the interplanetary space and in turn the Earth's electromagnetical environment on the basis of common periodicities in the solar and geomagnetic activity indices. The goal of this study is twofold. Firstly, we attempt to associate modes by comparing a temporal behavior of the power of geomagnetic activity parameters since it is barely sufficient searching for common peaks with a similar periodicity in order to causally correlate geomagnetic activity parameters. As a result of the wavelet transform analysis we are able to obtain information on the temporal behavior of the power in the velocity of the solar wind, the number density of protons in the solar wind, the AE index, the Dst index, the interplanetary magnetic field, B and its three components of the GSM coordinate system, $B_X$, $B_Y$, $B_Z$. Secondly, we also attempt to search for any signatures of influence on the space environment near the Earth by inner planets orbiting around the Sun. Our main findings are as follows: (1) Parameters we have investigated show periodicities of ~ 27 days, ~ 13.5 days, ~ 9 days. (2) The peaks in the power spectrum of $B_Z$ appear to be split due to an unknown agent. (3) For some modes powers are not present all the time and intervals showing high powers do not always coincide. (4) Noticeable peaks do not emerge at those frequencies corresponding to the synodic and/or sidereal periods of Mercury and Venus, which leads us to conclude that the Earth's space environment is not subject to the shadow of the inner planets as suggested earlier.

SVM 기반 히스테리시스 제어기를 이용한 D-STATCOM 전류 제어에 관한 연구 (A Study on Current Control using a Novel SVM-Based Hysteresis Controller in D-STATCOM)

  • 최정혜;신은철;유지윤
    • 전력전자학회논문지
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    • 제11권4호
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    • pp.293-301
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    • 2006
  • 배전급 STATCOM(Distribution-network STATic synchronous COMpensator)에 적용 가능한 공간 벡터 변조 (Space Vector Modulation, SVM) 기법을 이용한 히스테리시스 전류제어기를 제안하였다. 히스테리시스 전류제어기는 빠른 응답 특성, 쉬운 구현, 파라미터 변화에 대한 둔감성 등 많은 장점에도 불구하고 높은 스위칭 주파수와 제한되지 않는 전류 오차 때문에 스위칭 주파수에 영향을 받는 배전급 STATCOM 전류제어기로는 적합하지 않았다. 또한 전압 벡터의 인가방식에서도 뚜렷한 근거가 없어 전류오차가 제한되지 않았다. 이에 본 논문에서는 구역판별기, SVM, 그리고 외부와 내부 히스테리시스 제어기를 이용하여 높은 스위칭 주파수를 저감하고 특정 밴드 내에서 전류 오차를 줄인 개선된 SVM 기반의 히스테리시스 전류제어기를 제안하고 모의실험을 통해 제안한 기법의 유효성을 입증하였다.