• 한국광학회지
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• 제28권6호
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• pp.263-272
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• 2017

넓은 시야를 가지는 광학계에서는 전반부는 음의 굴절능, 후반부는 양의 굴절능을 가지는 inverted telephoto 구조가 일반적으로 사용되고 있고, 2반사광학계에서는 inverse Cassegrain system이 inverted telephoto 구조에 해당한다. 하지만 통상적인 회전대칭 구성의 inverse Cassegrain system에서는 시야가 가려지고 광선의 차폐가 심한 문제점이 있다. 이 연구에서는 이점을 고려하여 inverse Cassegrain system의 제2면에 조리개를 두어 시야를 넓히고, 광선의 차폐가 없는 비축시야만을 사용하는 광시야 비축 2반사광학계를 설계하였다.

• 한국광학회:학술대회논문집
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• 한국광학회 2009년도 동계학술발표회 논문집
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• pp.407-408
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• 2009

• Journal of the Optical Society of Korea
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• 제17권2호
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• pp.142-147
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• 2013

In order to deduce the difficulty of fixing the Ritchey-Chretien (R-C) dual reflective optical system and enhance the stability of the secondary mirror, a compact integral structure is presented here composed of two transmitting and two reflective aspheric surfaces. The four surfaces were manufactured from a single germanium lens and integrated together. The two reflective surfaces formed by coating the inner reflecting films were assembled in one lens. It makes the installation of the two mirrors easier and the structure of the secondary mirror more stable. A design of mid-wave infrared (MWIR) compact imaging system is presented with a spectral range chosen as $3.7-4.8{\mu}m$. The effective focal length is f=90 mm. The field of view (FOV) for the lens is $4.88^{\circ}$. It has good imaging capability with Modulation Transfer Function (MTF) of all field of view more than 0.55 close to the diffraction limitation. Outdoor experiments were carried out and it is shown that the integral catadioptric optical system performs well on imaging.

• 천문학회보
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• 제38권2호
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• pp.85.1-85.1
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• 2013

GMT(Giant Magellan Telescope)는 25.4m의 주경과 3.2m의 부경으로 이루어진 거대망원경이다. 3.2m의 부경은 빠른 tip-tilt로 망원경을 제어하는 Fast Steering Mirror(FSM)와 적응광학계로 이루어진 Adaptive Secondary Mirror (ASM)로 구분된다. 한국천문연구원은 국내외 협력기관들과 함께 부경 FSM의 시험모델개발을 수행하고 있다. 부경은 1.06m의 반사경 일곱 개로 이루어져 있는데, 한 개의 광축 반사경 주위로 여섯개의 비축 반사경이 둘러싸여서 하나의 3.2m 반사경과 같은 기능을 하고 있다. 비축 비구면 반사경에 대한 시험모델의 반사면을 가공한 결과 표면가공 정밀도가 11.7nm rms의 정밀도를 갖는 반사경을 가공하였다(target : <20nm rms). 또한 test-bed를 제작하여 tip-tilt 정밀도를 제어한 결과 성능요구 조건 값인 0.03arcsec 제어에 성공하였고, 더 나아가 0.01arcsec의 tip-tilt 제어도 가능한 것으로 판단된다.

• 천문학회보
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• 제39권2호
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• pp.120.1-120.1
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• 2014

Fast-steering Secondary Mirror prototype (FSMP) of the Giant Magellan Telescope (GMT) has been developed by the consortium consisting of institutes in Korea and the US. In 2014 we are finalizing the FSMP project as combining two sub-systems, the mirror fabricated by Korea Research Institute of Standards and Science (KRISS) and the mirror cell with tip-tilt controlling system developed by Institute for Advanced Engineering (IAE), in the KRISS facility. In the assembly process we will identify potential difficulties or problems for the process, such that this process can be reflected to the further development of the FSM for GMT. In the presentation, we present how the assembly process can be carried out in safety.

• 천문학회보
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• 제45권1호
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• pp.40.4-40.4
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• 2020

Kyung Hee university invented the Transformable Reflective Telescope (TRT) for optical experiment and education. The TRT kit can transform into three optical configurations from Newtonian to Cassegrain to Gregorian by exchanging the secondary mirror. We designed the Ebert-Fastie spectrograph as an extension of the TRT kit. The primary mirror of the TRT kit serves as both collimator and camera lens, and the reflective grating as the dispersing element is placed along the optical axis of the primary mirror. We designed and fabricated the grating holder and the source units using 3D printer. Baffle was also fabricated to suppress the stray light, which was reduced by 83%. The spectrograph can observe the optical wavelength range (4000Å~7000Å). Measured resolving power (R=λ/Δλ) was ~700 with slit width of 0.18mm. The spectrograph is optimized for f/24, and the spectral pixel scale is 0.49Å/pixel with Canon 550D detector. We present the sample spectra of discharged Ne, Ar and Kr gases. The flexible setting and high performance make this spectrograph a useful tool for education and experiment.

• 한국분무공학회지
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• 제4권1호
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• pp.13-18
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• 1999

It has been known that spray characteristics have an important effect on the mixture formation and directly influence the engine performances and the emissions. Up to now, the measurement of droplet size is well developed such as PDPA and PMAS though the behavior of small droplets during secondary atomization is not clear. Particle image velocimetry(PIV), a planar measuring technique, is a very efficient tool for studying complicated behavior and a fast and reliable method to track numerous droplets during injection. In this study, two-color scanning PIV is designed to obtain quasi-instantaneous two dimensional velocity data by using he-ion laser, rotating mirror and beam splitter. This PIV method which has high temporal and spatial resolution provides the information about the small complex droplet behavior.

• 한국광학회지
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• 제26권3호
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• pp.155-161
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• 2015

본 논문에서는 연안 지역 저고도 원격측정을 위한 소형 무인항공기 용 초분광센서 개발의 일환으로 비축 삼반사경 전단광학계의 설계와 성능분석 결과를 제시하였다. 이 광학계는 수 cm의 공간해상도(4cm@500m 운영고도)와 $4^{\circ}$의 시야각, 그리고 신호대 잡음비 100(@660 nm) 이상의 요구사항을 만족시키기 위하여, 70 mm의 입사동 크기와 개구수 5.0으로 설계 사양을 가지는 비구면의 주경과 부경이 포함된 비축 삼반사경 형태로 설계되었다. 본 설계의 광학성능은 $1/15{\lambda}$ 이하 RMS 파면오차 성능과 0.75이상의 MTF 성능(@660 nm)이 기대된다. 제작과 조립 단계를 고려하여 민감도 분석을 통해 3 반사경을 정렬 보상자로 선정하였으며, 경사 공차범위는 요소별로 0.17 mrad 으로 결정되었다. 이 비축 삼반사경 광학설계는 기존 초분광센서의 전단광학계에 비해 높은 광학성능을 보이고, 소형 무인항공기에 맞추어 경량화가 가능하도록 제작 기반을 설정하여, 향후 연안 원격탐사 연구에 활용될 예정이다.

• Current Optics and Photonics
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• 제6권2호
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• pp.171-182
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• 2022

A single-photon laser and mid-wave infrared (MWIR) common aperture optical system was designed and developed to detect and range a long-distance civil aviation aircraft. The secondary mirror of the Ritchey-Chretien (R-C) optical system was chosen as a dichroic lens to realize the design of a common aperture system for the laser and MWIR. Point spread function (PSF) ellipticity was introduced to evaluate the coupling efficiency of the laser receiving system. A small aperture stop and narrow filter were set in the secondary image plane and an afocal light path of the laser system, respectively, and the stray light suppression ability of the small aperture stop was verified by modeling and simulation. With high-precision manufacturing technology by single point diamond turning (SPDT) and a high-efficiency dichroic coating, the laser/MWIR common aperture optical system with a 𝜑300 mm aluminum alloy mirror obtained images of buildings at a distance of 5 km with great quality. A civil aviation aircraft detection experiment was conducted. The results show that the common aperture system could detect and track long-distance civil aviation aircraft effectively, and the coverage was more than 450 km (signal-to-noise ratio = 6.3). It satisfied the application requirements for earlier warning and ranging of long-range targets in the area of aviation, aerospace and ground detection systems.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2004년도 Proceedings of ISRS 2004
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• pp.452-455
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• 2004

MSC (Multi-Spectral Camera) system is a remote sensing instrument to obtain high resolution ground image. EOS (Electro-Optic System) for MSC mainly consists of PMA (Primary Mirror Assembly), SMA (Secondary Mirror Assembly), HSTS (High Stability Telescope Structure) and DFPA (Detector Focal Plane Assembly). High performance of EOS makes it possible for MSC system to provide high resolution and high quality ground images. Temperature of the EOS needs to be controlled to be in a specific range in order not to have any thermal distortion which can cause performance degradation. It is controlled by full redundant CPU based electronics. The validity of thermistor readings can be checked because a few thermistors are installed on each control point on EOS. Various kinds of thermal control logics are used to prevent 'Single Point Failure'. Control logic has a few set of database in order not to be corrupted by SEU (Single Event Upset). Even though the thermal control logic is working automatically, it can also be monitored and controlled by ground-station operator. In this paper, various ways of thermal control logic for EOS in MSC will be presented, which include thermal control mode and logic, redundancy design and status monitoring and reporting scheme.