• The Journal of the Korea Contents Association
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• v.9 no.11
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• pp.254-261
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• 2009

This study suggested that the table of CT-simulator and the laser alignment system using diagnostic CT scanner have an efficient method for improvement in alignment between the planned target center of traverse image with CT scanner. It was conducted on the daily QA when presented in the AAPM TG66 with correcting the laser alignment system using geometric trigonometric functions and investigated the effectiveness of correction methods as compared with those before and after correction. Before correction error was 3.82mm between the planned target center of image, the table longitudinal axis was twisted with 0.436o. The laser alignment system using geometric trigonometric functions in after correction was satisfied with tolerance limits of ${\pm}2mm$ when occurred about 0.7mm in errors between the planned target center. The table correction to satisfy the geometric accuracy is very inefficient over against the time and economic loss as well as technical limits in the case of application as only radiation therapy associated with CT-simulator with diagnostic CT scanner in use. But, the method which corrects the laser alignment system is economic and relatively simple with possibility of getting well geometric accuracy and we suppose that it is efficient method for applying in the clinic.

• Proceedings of the Optical Society of Korea Conference
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• 2001.02a
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• pp.92-93
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• 2001

주파수 안정화 레이저 광원은 10-6 이상의 상대 불확도가 필요한 간섭계에서 널리 쓰이고 있으며 특히 변위 측정 시스템에서는 반드시 쓰이고 있다. 상용화된 많은 변위 측정 시스템은 신호 대 잡음비가 우수하고 광학계의 정렬이 더 쉬운 헤테로다인 방식을 채택하고 있으며 이를 위해서 서로 수직 선형 편광인 다른 주파수의 광을 내보내는 광원이 필요하다. 현재 헤테로다인 변위 측정 시스템에 쓰이고 있는 광원은 이중 주파수 광원을 만드는 방식에 따라 지만 효과(Zeeman effect)를 이용한 지만 레이저(HP사)와 음향-광 변조기(Acousto-optic modulator)를 이용한 이중 주파수 레이저(Zy해사)가 있다. (중략)

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.39 no.3
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• pp.279-288
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• 2011

This paper will discuss the alignment techniques and measurement results of geostationary satellite communication antennas for correct antenna pointing and also the fixtures. To get the best performance in terms of antenna pointing and fixtures, zero G condition have been simulated and laser tracker and theodolite system have been applied. As a result, alignment stability was verified within the tolerance, ${\pm}\;0.25mm$ and ${\pm}\;0.013^{\circ}$ and finally Ka-band deployable antenna alignment has been accomplished within the tolerance, ${\pm}\;0.5mm$ and ${\pm}\;0.015^{\circ}$.

• Proceedings of the Optical Society of Korea Conference
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• 1995.06a
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• pp.68-74
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• 1995

한국전자통신연구소에서 개발된 바 있는 KrF 엑시머 레이저 스탭퍼의 개발 과정과 그 결과를 보이고, 동시에 현재 개발중인 ArF 엑시머 레이저 스텝퍼의 진행상황을 보고한다. 본 논문에서는 스탭퍼의 주요 구성요소인 조명계, 투영광학계, 웨이퍼 자동초점 및 자동정렬 시스템을 중심으로 설명하여, KrF와 ArF 에시머 레이저 스탭퍼간의 차이점과 그 특성들을 상호 비교한다.

• Journal of Biomedical Engineering Research
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• v.21 no.4
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• pp.385-390
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• 2000

The alignment of the prosthetics is very important in an amputee's gait. In the present study. a static prosthesis-alignment device was developed. It consisted of a force plate with four load cells, a laser beam controlled by a step motor, and a control part programmed by PCBASIC. Using the static prosthesis-alignment device, we measured the distance between the load line and various joints of 24 normal volunteers in three standing postures. such as neutral, forward leaning, and backward leaning. Only neutral postures were evaluated on four trans-tibial amputees. The load line for the normal person's neutral position located anterior to the ankle, the knee, and the greater trochanter, but posterior to the shoulder joint. Forward and backward leaning of the normal person resulted in a significant anterior and posterior movements of the load line, respectively. The load line for the amputated side of the trans-tibial amputee also located anterior to the ankle, the extremity prostheses, providing a good relative locations of the load line with respect to various joints.

• The Bulletin of The Korean Astronomical Society
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• v.37 no.2
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• pp.164.2-164.2
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• 2012

인공위성레이저추적(SLR, Satellite Laser Ranging) 시스템은 인공위성까지 레이저를 발사하여 되돌아오는 시간간격을 측정함으로서 위성까지의 거리를 측정하는 시스템으로 현존하는 인공위성 궤도결정 시스템으로는 가장 정밀하다. 한국천문연구원은 우주추적 및 감시의 필요성이 증가함에 따라 2008년부터 40cm급 이동형 인공위성레이저추적 시스템을 개발을 시작하였고, 현재 개발을 완료하여 시험운영 중에 있다. 시스템 개발 과정 중에 발생할 수 있는 문제점들을 최소화하기 위해, 설계 단계에서 부품을 포함한 광기계 구조물에 대한 구조해석과, 실험실 프로토타입 구성 등을 실시하였다. 제작된 각 서브시스템별 조립 및 평가는 한국천문연구원이 보유한 광학계 조립 및 평가 시설을 이용하였다. 개발된 이동형 레이저 추적 시스템의 광학부는 추적마운트에 장착되었고, 현장 시험관측을 통해 수신광학계 및 광신호유도계의 정렬 및 제어항목 교정 등을 실시하였으며, 성공적으로 시험 영상 관측을 완료하였다. 이 발표에서는 이동형 레이저 추적 시스템 광학계의 개발 과정과 그 결과에 대해 보고한다.

• 한국정보통신설비학회:학술대회논문집
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• 2003.08a
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• pp.180-182
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• 2003

200m 이하의 전송거리를 가지며 송신기와 수신기가 일체화된 단거리 무선 광통신용 트랜시버를 제작하고, 그 성능을 평가하였다. 이러한 단거리 무선 광통신 트랜시버는 가격이 저렴한 저출력의 레이저를 광원으로 사용할 수 있고, 능동 정렬이 필요 없을 뿐만 아니라, 작은 구경의 렌즈를 사용할 수 있기 때문에 크기가 작고, 가벼우며, 설치가 쉽다는 장점을 가진다. 특히 패키징 개념을 사용하여 송신기와 수신기의 광축을 미리 수평으로 정렬한 후 영구고정함으로서 기계공작이 최소화되고, 송신기 부분의 정렬만으로 수신기가 정렬되므로 링크의 정렬이 매우 간단하며, 저렴한 무선 광통신 시스템의 구성이 가능하다.

• Journal of Aerospace System Engineering
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• v.16 no.4
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• pp.60-67
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• 2022

An Electro-Optical Tracking System (EOTS) is an electric optical system with EO/IR cameras, laser sensors, and an IMU. The EOTS calculates coordinates of targets, using attitude and acceleration measured by the IMU. In particular for an armed aircraft, the performance of the weapon system depends on how quickly and accurately it acquires the target coordinates. The IMU should be operated after alignment is complete, to meet the coordinate accuracy required by the weapon system so the initial stabilization time of the IMU should be reduced, by quickly measuring the attitude and acceleration. Alignment is the process of determining the initial attitude by resolving the attitude error of the IMU, and the IMU of mission equipment such as an airborne EOTS, uses velocity matching based on the velocity from GPS/INS for aircraft navigation. In this paper, a method is presented to improve the transfer alignment performance of the airborne EOTS, by maneuvering aircraft and the mission equipment. First, the performance factor of the alignment was identified, as a heading error through the velocity matching model and simulation results. Then acceleration maneuvers and attitude changes were necessary, to correct the error. As a result of flight tests applied to an EOTS on a OOO aircraft system, the transfer alignment performance was improved as the duration time was decreased, by more than five times when the aircraft accelerated by more than 0.2g and the EOTS was moving until 6.7deg/s.

• Proceedings of the Korean Society of Laser Processing Conference
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• 2006.06a
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• pp.123-128
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• 2006

We constructed a micro-patterning system that build patterns on a photoresist coated wafer using laser direct writing system. Confocal microscope system was adapted for real-time auto-focusing of the laser writing lens to generate lines of uniform width.

• Korean Journal of Optics and Photonics
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• v.32 no.2
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• pp.49-54
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• 2021

In this paper, we design and construct the equipment to manufacture large-diameter optical fiber end caps, which are the core parts of high-power fiber lasers, and we fabricate large-diameter optical fiber end caps using the home-made equipment. This equipment consists of a CO2 laser as a fusion-splice heat source, a precision stage assembly for transferring the position of a large-diameter optical fiber and an end cap, and a vision system used for alignment when the fusion splice is interlocked with the stage assembly. The output of the laser source is interlocked with the stage assembly to control the output, and the equipment is manufactured to align the polarization axis of the large-diameter polarization-maintaining optical fiber with the vision system. Optical fiber end caps were manufactured by laser fusion splicing of a large-diameter polarization-maintaining optical fiber with a clad diameter of 400 ㎛ and an end cap of 10×5×2 ㎣ (W×D×H) using home-made equipment. Signal-light insertion loss, polarization extinction ratio, and beam quality M2 of the fabricated large-diameter optical fiber end caps were measured to be 0.6%, 16.7 dB, and 1.21, respectively.