• 대한전기학회:학술대회논문집
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• 대한전기학회 2006년도 제37회 하계학술대회 논문집 C
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• pp.1733-1734
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• 2006

In recent, it became necessary to develop the technology about electrodeless fluorescent lamp according to demand of the electrodeless fluorescent lamp system that used higher efficiency and advantage of long lifetime. Inductively coupled plasma is commonly used for electrodeless lamp due to its ease of plasma generation. An electric power efficiency of electrodeless fluorescent lamp has big relative property of gas in lamp, gas pressure, lamp formation, ingredients of magnetic substance and shape and action frequency etc. We used magnetic substance that open self-examination material of electrodeless fluorescent lamp antenna. Ferrite that is used in this experiment was Mn-Zn type. We have examined temperature and flux characteristic by frequency. Considering using frequency 2.65[MHz], Frequency was changed from 2.05[MHz] to 3.05[MHz] to recognize flux and temperature change of lamp. I used LMS(Lighting Measurement System) to measure flux and IR Camera to measure temperature of lamp.

• 한국항공우주학회지
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• 제48권6호
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• pp.401-410
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• 2020

본 연구에서는 전술급 무인항공기의 GPS 신호간섭 및 재밍(Jamming)/기만(Spoofing) 공격 시 위치항법 정보의 취약성을 보완하기 위해 개발한 영상정보 기반 실시간 비행체 위치보정 시스템을 기술하고자 한다. 전술급 무인항공기는 GPS 두절 시 항법장비가 GPS/INS 통합항법에서 DR/AHRS 모드로 전환하여 자동비행이 가능하나, 위치 항법의 경우 대기속도 및 방위각을 활용한 추측항법(DR, Dead Reckoning)으로 인해 시간이 지나면 오차가 누적되어 비행체 위치 파악 및 데이터링크 안테나 자동추적이 제한되는 등의 문제점을 갖고 있다. 이러한 위치 오차의 누적을 최소화하기 위해 영상감지기를 이용한 특정지역 위치보정점을 바탕으로 비행체 자세, 영상감지기 방위각/고각 및 수치지도 데이터(DTED)를 활용하여 비행체 위치를 계산하고 이를 실시간으로 항법장비에 보정하는 시스템을 개발하였다. 또한 GPS 시뮬레이터를 이용한 지상시험과 추측항법 모드의 비행시험으로 영상정보 기반 실시간 비행체 위치보정 시스템의 기능 및 성능을 검증하였다.

• Nuclear Engineering and Technology
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• 제54권11호
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• pp.4102-4110
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• 2022

Aiming at high-power and long-pulse operation up to 1000 s, some improvements have been made for both 2.45 GHz and 4.6 GHz lower hybrid (LH) systems during the recent 5 years. At first, the guard limiters of the LH antennas with graphite tiles were upgraded to tungsten, the most promising material for plasma facing components in nuclear fusion devices. These new guard limiters can operate at a peak power density of 12.9 MW/m². Strong hot spots were usually observed on the old graphite limiters when 4.6 GHz system operated with power >2.0 MW [B. N. Wan et al., Nucl. Fusion 57 (2017) 102019], leading to a reduction of the maximum power capability. With the new limiters, 4.6 GHz LH system, the main current drive (CD) and electron heating tool for EAST, can be operated with power >2.5 MW routinely. Long-pulse operation up to 100 s with 4.6 GHz LH power of 2.4 MW was achieved in 2021 and the maximal temperature on the guard limiters measured by an infrared (IR) camera was about 540 ℃, much below the permissible value of tungsten material (~1200 ℃). A discharge with a duration of 1056 s was achieved and the 4.6 GHz LH energy injected into the plasma was up to 1.05 GJ. Secondly, the fully-active-multijunction (FAM) launcher of 2.45 GHz system was upgraded to a passive-active-multijunction (PAM), for which the density of optimum coupling was relatively low (below the cut-off value). Good coupling with reflection coefficient ~3% has been achieved with plasma-antenna distance up to 11 cm for the new PAM. Finally, in order to eliminate the effect of ion cyclotron range of frequencies (ICRF) wave on 4.6 GHz LH wave coupling, the location of the ICRF launcher was changed to a port that is located 157.5° toroidally from the 4.6 GHz LH system and is not magnetically connected.