• Journal of Welding and Joining
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• 제33권4호
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• pp.24-29
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• 2015

The current waveform was analysed to monitor the weld quality in real time process. The acquired current waveform was discretely analysed for the top and bottom limits of peaks as well as the pulse frequency measurement. Fast Fourier Transform was implemented in the program to monitor the pulse frequency in real time. The developed algorithm or program was tested for the validation purpose. The cross-section of weld profile was compared to the current waveform profile to correlate the monitored signal and the actual parts. Pulse frequency was also used as auxiliary tool for the quality monitoring. Based on the results, it was possible to evaluate the quality of welding by measure the current waveform profile and frequency measurement.

• 대한전자공학회논문지TC
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• 제47권12호
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• pp.17-23
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• 2010

모바일 클라우드 컴퓨팅에서 이동 노드는 이동 중에도 끊김없이 서비스를 요청하고 받을 수 있어야 한다. PMIPv6에서 이동 노드가 통신하고자 하는 상대 노드가 동일한 PMIPv6 도메인에 있는 또 다른 이동 노드인 경우에는, 두 이동 노드 간의 패킷이 각 노드가 접속해 있는 Mobile Access Gateway와 Local Mobility Anchor를 통과하여 전송되기 때문에 패킷 전송비용이 증가하는 문제가 발생한다. 이러한 문제점을 해결하기 위해 몇 가지 경로 최적화 기법이 제안되었다. 그러나 제안된 기법들은 최적화된 경로를 결정하기 위해 많은 시그널 메시지가 필요하다. 본 논문은 PFMIPv6의 예측 알고리즘을 활용한 경로 최적화 핸드오버 기법을 제안한다. 이동 노드의 핸드오버가 임박할 경우 PFMIPv6의 예측 알고리즘을 활용하여 경로 최적화에 필요한 컨텍스트 메시지를 이동 노드가 접속할 MAG에 미리 전송한다. MAG는 컨텍스트 메시지를 활용해 최적화된 경로를 미리 성립함으로서 추가적인 경로 최적화 절차를 수행하지 않는다. 제안된 기법은 PFMIPv6의 예측 알고리즘을 활용하여 경로 최적화에 필요한 컨텍스트 메시지를 전송함으로서 시그널 메시지를 줄일 수 있다. 제안된 기법의 효율성을 보여주기 위해 수학적 성능 평가를 수행하였으며, 이를 통해 제안된 기법이 기존의 경로 최적화 기법보다 우수한 성능을 제공함을 보여준다.

• 우주기술과 응용
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• 제2권2호
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• pp.104-120
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• 2022

도요샛(Small Scale magNetospheric and Ionospheric Plasma Experiment, SNIPE)의 과학임무는 전리권 상층부 소규모 플라즈마 구조의 공간적 시간적 변화를 관찰하는 것이다. 이를 위해 4개의 6U 큐브위성(10 kg)이 고도 약 500 km 극궤도로 발사될 예정이며, 상호 위성 간 거리는 편대 비행 알고리즘에 의해 수 10 km에서 수 1,000 km 이상으로 제어된다. 운영 초기에는 4기의 위성이 같은 궤도 평면에 위치하는 종대비행을 하다가 경도상에서 나란히 배치되는 횡대비행으로 전환하여 4기의 서로 다른 지점에서 공간적인 변화를 관측하게 된다. 도요샛에는 입자 검출기, 랑뮈어 탐침, 자력계로 구성된 우주날씨 관측 장비가 각 위성에 탑재된다. 모든 관측기는 10 Hz 이상의 높은 시간 분해능을 가지며 큐브위성에 최적화 설계되었다. 이 외에도 이리디듐 통신 모듈은 지자기 폭풍이 발생할 때 작동 모드를 변경하기 위한 명령을 업로드할 수 있는 기회를 제공한다. 도요샛은 극 지역 플라즈마 밀도 급상승, 필드 정렬 전류, 고에너지 전자의 국소 영역 침투, 적도 및 중위도 플라즈마 거품의 발생 및 시공간적 진화에 대한 관찰을 수행할 예정이며, 이를 통해 태양풍이 우주날씨에 어떠한 영향을 미치는지 탐구하게 된다. 도요샛은 2023년 상반기 러시아 소유즈-2에 의해 카자흐스탄 바이코누르에서 발사될 예정이다.

• 대한전기학회:학술대회논문집
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• 대한전기학회 2002년도 학술대회 논문집 전문대학교육위원
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• pp.166-171
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• 2002

We are in transitional period of welding technique, which has changed from the stage of quantity and quality to the stage of future technique, imported and introduced from many advanced countries. Therefore, many researches and studies for development on high speeding and making welding machines with high effectiveness has been doing vigorously. In this dissertation, I have studied on a pulsed MAG welding machine, with which welding of thin plates may perform high speeding and effecting. First, I produced a phase shifted full bridge DC-DC convert, which is the type of reduced conduction loss and the power supply for welding machine. And then, I found out an output waveform control algorithm about one pulsed one droplet and short waveform control for thin plates with high speed by deriving the circuit model utilizing the circuit averaged method for full bridge converter.

• 대한전기학회:학술대회논문집
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• 대한전기학회 2009년도 춘계학술대회 논문집 에너지변화시스템부문
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• pp.88-90
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• 2009

Extremely-Low-Frequency(ELF) magnetic fields are generated around power cables and bus bars in power systems. Such the stray fields may cause disturbances to nearby electronic apparatus and affect even human health. In order to seeking out a proper way to reducing the fields, the first thing to do is to accurately predict field distribution around analysis models of interest. Then, optimization techniques should be applied for finding a more improved design than the initial one. To achieve this goal, commercial electromagnetic software, MagNet, is combined with evolution strategy algorithm. For verification of the proposed method, three-phase power line cables and busbar systems have been tested.

• 천문학회보
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• 제46권1호
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• pp.58.4-59
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• 2021

This presentation introduces Korea's SNIPE (Small scale magNespheric and Ionospheric Plasma Experiment) mission, formation flying CubeSat constellation. Observing particles and waves on a single satellite suffers from inherent space-time ambiguity. To observe spatial and temporal variations of the micro-scale plasma structures on the topside ionosphere, four 6U CubeSats (~ 10 kg) will be launched into a polar orbit of the altitude of ~500 km in 2021. The distances of each satellite will be controlled from 10 km to more than 100 km by formation flying algorithm. The SNIPE mission is equipped with identical scientific instruments, solid-state telescope, magnetometer, and Langmuir probe. All the payloads have a high temporal resolution (sampling rates of about 10 Hz). Iridium modules provide an opportunity to upload changes in operational modes when geomagnetic storms occur. SNIPE's observations of the dimensions, occurrence rates, amplitudes, and spatiotemporal evolution of polar cap patches, field-aligned currents (FAC), radiation belt microbursts, and equatorial and mid-latitude plasma blobs and bubbles will determine their significance to the solar wind-magnetosphere-ionosphere interaction and quantify their impact on space weather.

• 천문학회보
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• 제44권2호
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• pp.74.2-74.2
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• 2019

We present a possible bias in the estimation of velocity dispersions for galaxy groups due to the contribution of subgroups which are infalling into the groups. We execute a systematic search for flux-limited galaxy groups and subgroups based on the spectroscopic galaxies with r < 17.77 mag of SDSS data release 12, by using DBSCAN (Density-Based Spatial Clustering of Application with Noise) and Hierarchical Clustering Method which are well known unsupervised machine learning algorithm. A total of 2042 groups with at least 10 members are found and ~20% of groups have subgroups. We found that the estimation of velocity dispersions of groups using total galaxies including those in subgroups are underestimated by ~10% compared to the case of using only galaxies in main groups. This result suggests that the subgroups should be properly considered for mass measurement of galaxy groups based on the velocity dispersion.

• Journal of Astronomy and Space Sciences
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• 제35권1호
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• pp.31-37
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• 2018

Pc1 pulsations are geomagnetic fluctuations in the frequency range of 0.2 to 5 Hz. There have been several observations of Pc1 pulsations in low earth orbit by MAGSAT, DE-2, Viking, Freja, CHAMP, and SWARM satellites. However, there has been a clear limitation in resolving the spatial and temporal variations of the pulsation by using a single-point observation by a single satellite. To overcome such limitations of previous observations, a new space mission was recently initiated, using the concept of multi-satellites, named the Small scale magNetospheric and Ionospheric Plasma Experiments (SNIPE). The SNIPE mission consists of four nanosatellites (~10 kg), which will be launched into a polar orbit at an altitude of 600 km (TBD) in 2020. Four satellites will be deployed in orbit, and the distances between each satellite will be controlled from 10 to 1,000 km by a high-end formation-flying algorithm. One of the possible science targets of the SNIPE mission is observing electromagnetic ion cyclotron (EMIC) waves. In this paper, we report on examples of observations, showing the limitations of previous EMIC observations in low earth orbit, and suggest possibilities to overcome those limitations through a new mission.

• 천문학회보
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• 제42권1호
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• pp.40.3-41
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• 2017

Korea Astronomy and Space Science Institute The observation of particles and waves using a single satellite inherently suffers from space-time ambiguity. Recently, such ambiguity has often been resolved by multi-satellite observations; however, the inter-satellite distances were generally larger than 100 km. Hence, the ambiguity could be resolved only for large-scale (> 100 km) structures while numerous microscale phenomena have been observed at low altitude satellite orbits. In order to resolve those spatial and temporal variations of the microscale plasma structures on the topside ionosphere, SNIPE mission consisted of four (TBD) nanosatellites (~10 kg) will be launched into a polar orbit at an altitude of 700 km (TBD). Two pairs of satellites will be deployed on orbit and the distances between each satellite will be from 10 to 100 km controlled by a formation flying algorithm. The SNIPE mission is equipped with scientific payloads which can measure the following geophysical parameters: density/temperature of cold ionospheric electrons, energetic (~100 keV) electron flux, and magnetic field vectors. All the payloads will have high temporal resolution (~ 16 Hz (TBD)). This mission is planned to launch in 2020. The SNIPE mission aims to elucidate microscale (100 m-10 km) structures in the topside ionosphere (below altitude of 1,000 km), especially the fine-scale morphology of high-energy electron precipitation, cold plasma density/temperature, field-aligned currents, and electromagnetic waves. Hence, the mission will observe microscale structures of the following phenomena in geospace: high-latitude irregularities, such as polar-cap patches; field-aligned currents in the auroral oval; electro-magnetic ion cyclotron (EMIC) waves; hundreds keV electrons' precipitations, such as electron microbursts; subauroral plasma density troughs; and low-latitude plasma irregularities, such as ionospheric blobs and bubbles. We have developed a 6U nanosatellite bus system as the basic platform for the SNIPE mission. Three basic plasma instruments shall be installed on all of each spacecraft, Particle Detector (PD), Langmuir Probe (LP), and Scientific MAGnetometer (SMAG). In addition we now discuss with NASA and JAXA to collaborate with the other payload opportunities into SNIPE mission.