• 한국재료학회지
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• 제28권12호
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• pp.732-737
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• 2018

We develop a purification process of $Hg_2Br_2$ raw powders using a physical vapor transport(PVT) process, which is essential for the fabrication of a high performance acousto-optic tunable filter(AOTF) module. Specifically, we characterize and compare three $Hg_2Br_2$ powders: $Hg_2Br_2$ raw powder, $Hg_2Br_2$ powder purified under pumping conditions, and $Hg_2Br_2$ powder purified under vacuum sealing. Before and after purification, we characterize the powder samples through X-ray diffraction and X-ray photoelectron spectroscopy. The corresponding results indicate that physical properties of the $Hg_2Br_2$ compound are not damaged even after the purification process. The impurities and concentration in the purified $Hg_2Br_2$ powder are evaluated by inductively coupled plasma-mass spectroscopy. Notably, compared to the sample purified under pumping conditions, the purification process under vacuum sealing results in a higher purity $Hg_2Br_2$ (99.999 %). In addition, when the second vacuum sealing purification process is performed, the remaining impurities are almost removed, giving rise to $Hg_2Br_2$ with ultra-high purity. This high purification process might be possible due to independent control of impurities and $Hg_2Br_2$ materials under the optimized vacuum sealing. Preparation of such a highly purified $Hg_2Br_2$ materials will pave a promising way toward a high-quality $Hg_2Br_2$ single crystal and then high performance AOTF modules.

• 한국항공우주학회지
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• 제41권4호
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• pp.268-274
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• 2013

항공기 날개 앞전의 레이더흡수구조 최적화를 위한 목적함수를 정의하였으며, 유전체로 구성된 단층형 레이더흡수구조를 설계하였다. 설계변수는 흡수체의 복소유전율이며 반사계수와 레이더반사면적을 각각 목적함수로 사용하였다. 반사계수는 계산이 간단하여 최적화에 효과적으로 사용될 수 있지만 대상물을 평판형태로 가정하기 때문에 구조물의 형상을 충분히 반영하기 어렵다. 반면 레이더반사면적은 형상을 충분히 반영할 수 있지만 계산에 많은 시간이 요구된다. 반사계수는 전송선로이론을 통하여 계산하였으며, 레이더반사면적은 형상조건을 반영하기 위하여 날개 앞전 부분모델에 대해 물리광학법을 사용하여 평가하였다. 최적설계는 유전자알고리즘을 사용하였고, 설계된 레이더흡수구조를 날개 앞전에 적용하여 레이더반사면적을 계산함으로써 레이더흡수 성능을 확인하였다.

• 한국안광학회지
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• 제19권3호
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• pp.407-412
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• 2014

목적: 시분할 장치가 동측성 반맹시 환자의 재활치료용 프레넬 프리즘으로 인한 복시 현상을 최소화하고 안정적인 시야를 확보할 수 있는지 알아보고자 하였다. 방법: 소형 모터와 마분지를 사용하여 시분할 장치를 제작했다. 시분할 장치의 효율성을 검증하기 위해 시분할 장치 전후 걷는 방향과 문자에 대한 인식을 비교 분석했다. 결과: 공간의 이등분할 실험에서 시분할 장치 전 피검자의 방향각은 $+18.14^{\circ}$였으며 장치 후의 방향각은 $+8.91^{\circ}$로 나타났다. 시분할 장치 후 $4{\times}4$시표의 문자 인식 실험에서는 정답률이 9%P, $6{\times}6$시표에서는 15%P가 증가했다. 특히 정답률이 낮은 군에서 효과가 더 뛰어났다. 결론: 시분할 장치는 동측성 반맹시 환자의 방향성이나 운동성에도 좋은 결과를 보였다.

• Journal of Astronomy and Space Sciences
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• 제29권4호
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• pp.351-362
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• 2012

We made a study on real-time determination method for relative position using the laser-measured distance data between satellites. We numerically performed the determination of relative position in accordance with extended Kalman filter algorithm using the vectors obtained through nonlinear equation of relative motion, laser simulator for distance measurement, and attitude determination of chief satellite. Because the spherical parameters of relative distance and direction are used, there occur some changes in precision depending on changes in relative distance when determining the relative position. As a result of simulation, it was possible to determine the relative position with several millimeter-level errors at a distance of 10 km, and sub-millimeter level errors at a distance of 1 km. In addition, we performed the determination of relative position assuming the case that global positioning system data was not received for long hours to see the impact of determination of chief satellite orbit on the determination of relative position. The determination of precise relative position at a long distance carried out in this study can be used for scientific mission using the satellite formation flying.

• 한국항공우주학회지
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• 제47권7호
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• pp.479-488
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• 2019

순항 유도탄은 비행기처럼 날개와 제트엔진을 사용하여 상당 거리를 순항한 후 최종 목표에 도달하는 유도탄이다. 적의 레이더에 쉽게 포착되지 않을뿐더러 아음속 장거리 순항이 가능해야 하므로, RCS 저감과 향상된 공력성능을 고려한 통합 설계가 필수적이다. 본 연구에서는 Taurus 유도탄과 유사한 순항 유도탄 모델을 설계한 후, Physical Optics (PO; 물리적 광학) 기법과 Navier-Stokes CFD 코드를 사용하여 비행체의 RCS와 공력특성을 분석하였다. 이를 바탕으로 공력성능 향상과 RCS 저감 기술이 적용된 순항 유도탄의 최적 형상을 도출하였다.

• 천문학논총
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• 제22권4호
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• pp.201-209
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• 2007

We have preliminarily designed two infrared optical systems of the multi-purpose infrared camera system (MIRIS) which is the main payload of STSAT-3. Each optical system consists of a Cassegrain telescope, a field lens and a 1:1 re-imaging lens system that is essential for providing a cold stop. The Cassegrain telescope is identical for both of two infrared cameras, but the field correction lens and re-imaging lens system are different from each other because of different bands of wavelength. The effective aperture size is 100mm in diameter and the focal ratio is f/5. The total length of the optical system is 300mm and the position of the cold stop is 25mm from the detector focal plane. The RMS spot size is smaller than $40{\mu}m$ over the whole detector plane.

• Current Optics and Photonics
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• 제6권5호
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• pp.445-452
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• 2022

We developed an adaptive optics test bench using an optical simulator and two rotating phase plates that mimicked the atmospheric turbulence at Bohyunsan Observatory. The observatory was reported to have a Fried parameter with a mean value of 85 mm and standard deviation of 13 mm, often expressed as 85 ± 13 mm. First, we fabricated several phase plates to generate realistic atmospheric-like turbulence. Then, we selected a pair from among the fabricated phase plates to emulate the atmospheric turbulence at the site. The result was 83 ± 11 mm. To address dynamic behavior, we emulated the atmospheric disturbance produced by a wind flow of 8.3 m/s by controlling the rotational speed of the phase plates. Finally, we investigated how closely the atmospheric disturbance simulation emulated reality with an investigation of the measurements on the optical table. The verification confirmed that the simulator showed a Fried parameter of 87 ± 15 mm as designed, but a little slower wind velocity (7.5 ± 2.5 m/s) than expected. This was because of the nonlinear motion of the phase plates. In conclusion, we successfully mimicked the atmospheric disturbance of Bohyunsan Observatory with an error of less than 10% in terms of Fried parameter and wind velocity.

• 한국광학회지
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• 제15권4호
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• pp.391-396
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• 2004

인공위성용 지구관측 카메라나 우주관측 망원경에는 크기와 무게의 제약 때문에 Cassegrain 방식의 망원경이 많이 쓰인다. 이와 같은 우주광학계의 성공적인 임무수행을 위해서는 망원경부의 정밀한 광학정렬이 매우 중요하다. 본 논문에서는 정렬 정밀도에 따른 Cassegrain 방식 망원경부의 광학정렬 방법 중, 간섭무늬를 이용한 방법, 파면오차를 이용한 방법, 역최적화 광학정렬 방법 등을 모사를 통해 제시하고, 현재 개발 중인 구경 300 mm급 소형 위성용 카메라에 적용한 광학정렬 실험 결과를 정리한다.

• 전기학회논문지P
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• 제63권4호
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• pp.283-289
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• 2014

A Fresnel lens is an optical component which can be used as a cost-effective, lightweight alternative to conventional continuous surface optics. Fresnel lens solar concentrators continue to fulfill a market requirement as a system component in high volume cost effective Concentrating Photovoltaic (CPV) electricity generation. The basic principles of the fresnel lens are reviewed and some practical examples are described. To investigate the performance space of the Fresnel lens, a fast simulation method which is a hybrid between raytracing and analytical computation is employed to generate a cache of simulation data. Injection molders are warming up to the idea of cycling their tool surface temperature during the molding cycle rather than keeping it constant. Heat and cool process are now also finding that raising the mold wall temperature above the resin's glass-transition or crystalline melting temperature during the filling stage and product performance in applications from automotive to packaging to optics. This paper deals with the suitability of Fresnel lenses of imaging and non-imaging designs for solar energy concentration. The concentration fresnel lens confirmed machinability and optical transmittance and roughness measure through manufactured the prototype.

• 반도체디스플레이기술학회지
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• 제18권2호
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• pp.58-62
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• 2019

Diffractive Optical Elements(DOEs) diffracts incident light using the diffraction phenomenon of light to generate a desired diffraction image. In recent years, the use of diffraction optics, which can replace existing refractive optical elements with flat plates, has been increased by implementing various optical functions that could not be implemented in refractive optical devices and by becoming miniaturized and compacted optical elements. Direct laser lithography is typically used to effectively fabrication such a diffractive optical element in a large area with a low process cost. In this study, the process conditions for fabricating patterns of diffractive optical elements in various shapes were found using direct laser lithographic system, and optical performance evaluation was performed through fabrication.