• 한국광학회지
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• 제16권4호
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• pp.345-353
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• 2005

포토 다이오드(photodiode) 조정 방식을 이용해서, 비전 시스템을 장착한 고가의 정밀 자동 조립조정 장비 없이 홀로그램 픽업 모듈을 제작하는 새로운 방법을 제안하였다. 저가격화를 위해서 리드 프레임형의 반도체 레이저와 COB(Chip on Board)형의 포토 다이오드를 사용했고, 초점 에러 신호(focus error, FES) 검출방법은 스팟 사이즈 검출법(spot size detection, SSD), 트랙 에러 신호(tracking error, TES) 검출방법은 삼빔법(3 beam method)을 이용했다. 이를 만족하는 픽업 홀로그램 모듈 광학계를 설계하고, 조립조정 프로세스 수립 및 시스템을 제작하였으며, 조립된 홀로그램 모듈을 이용하여 CD에서 데이터를 검출하는 실험을 통해 제안된 포토 다이오드 조정방식의 유용함을 입증하였다.

• 한국마이크로전자및패키징학회:학술대회논문집
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• 한국마이크로전자및패키징학회 2006년도 ISMP 2006
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• pp.67-73
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• 2006

A system in package (SiP) generally contains a variety of systems such as analog, digital, optical and micro-electro-mechanical systems, integrated in a system-level package connected through a substrate. However, there are many electrical and mechanical reliability issues including the reliability issue for embedded structures. A mismatch of thermal coefficients of expansion among packaging materials and devices can lead to warping or delamination in the package. In this study, the effect of material properties of underfill, such as Young's modulus and CTE, are investigated through FEM simulation. Experimental investigation on the warpage of the package is also carried out to verify the simulation results. The results show that the reliability of the system in package is closely related to the material properties of underfill. The results of this study provide a good guidance for the material selection when designing the system in package.

• 한국세라믹학회지
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• 제47권2호
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• pp.117-121
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• 2010

$SnO_2-(1-x)P_2O_5-xB_2O_3$ glass system were prepared by melt-quenching technique in the compositional series containing 50, 55 and 60 mol% of $SnO_2$. Local structure of the glasses was investigated by Raman and FT-IR measurements. A large glass-forming region was found at the phosphate side of the ternary system with homogeneous glasses containing up to 5~25 mol% of $B_2O_3$. According as content of $B_2O_3$ increases, theraml expansion coefficient of glass decreased but transition temperature and softening temperature increased. Because these phenomenon changed local structure of glass. According as content of $B_2O_3$ increases, quantity of bridging oxygen increased. Also, according as content of $SnO_2$ increases, confirmed that quantity of non-bridging oxygen increases.

• 전기학회논문지
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• 제67권10호
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• pp.1395-1400
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• 2018

EO TGP(Electro-Optical Targeting Pod) is an optical tracking system which has various functions such as target tracking and image stabilization and LOS(Line of Sight) change. Especially, it is very important to move the LOS into a interest point for joystick command. When pilot move joystick in order to observe different scene, EO TGP gimbals should be operated properly. Generally, most EOTS just operate corresponding gimbal for joystick command. For example, if pilot input horizontal command in order to observe right hand screen, it just drive azimuth gimbal at any position. But in the screen, the image dosen't move in a horizontal direction because gimbal structure is Euler angle. And image rotation is occurred by elevation gimbal angle. So we need to move Pitch gimbal. So in the paper, we designed LOS moving algorithm which convert LOS command to gimbal velocity command to move LOS properly. We modeled a differential kinematic equation and then change the joystick command into velocity command of gimbals. This algorithm generate velocity command of each gimbal for same horizontal direction command. Finally, we verified performance through MATLAB/Simulink.

• 항공우주기술
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• 제10권2호
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• pp.101-104
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• 2011

고해상도 전자광학 탑재체의 주 반사경과 제2 반사경 간 조립 정렬은 전체 카메라 시스템의 조립 단계 중 가장 중요한 단계이다. 제 2 반사경의 정렬에는 파면센서와 콜리메이터를 사용하였는데 간섭계 보다는 크기가 작고 다루기가 편하기 때문이다. 본 논문에서는 고해상도 전자광학 탑재체의 제 2 반사경에 대한 정렬 방법과 절차에 대해 소개 하고자 한다.

• 한국진공학회지
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• 제7권s1호
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• pp.149-155
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• 1998

The linear electro-optic (EO) effect is one of the second-order nonlinear optical effects existing in a noncentrosymmetric macroscopic system. In a polymer thin film, the noncentrosymmetry is achieved by electric field poling. The magnitude of the linear EO response is determined through the orientational distribution function of hyperpolarizable molecular dipoles. The relation between the linear EO coefficient and the second-order nonlinear optical susceptibility is explained. Three different methods of measuring the linear EO coefficient of a poled nonliner optical polymer thin film are introduced and discussed. All of them make use of the interferometric technique, the difference being in the optical parameters which are interfering.

• 대한의용생체공학회:학술대회논문집
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• 대한의용생체공학회 1990년도 추계학술대회
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• pp.33-37
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• 1990

Endoscope system is the device that observe interior the body. It has some demerits because it use of optical fibers. The resolution of images depends on the number of optical fibers, it is impossible that several people observe at the same time and it needs special camera in order to record images. In order to overcome these demerits, electro endoscope system using CCD(Charge Coupled Device) has been developed recently. If the diameter of insertion tube is thinner, it is easier to be examined by thin endoscope system. At the present time, we develope these type of electro endoscope system in the department of SNU biomedical engineering. Moreover, we are researching an algorithm of the 3D-reconstruction of interior of the gaster. In this paper, a method for 3D information detection using electroendoscopic image sequence has been presented.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2008년도 International Symposium on Remote Sensing
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• pp.232-235
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• 2008

The mission of the EO(electro-optical) based low earth orbit satellite is provision of the high-resolution images required for GIS(Geographical Information Systems) establishment and the applications for environmental, agriculture and ocean monitoring. AEISS(Advanced Earth Imaging Sensor System) which is the main payload on the satellite consists of EOS(electro-optical subsystem) and PDTS(Payload Data Transmission Sub-system). IDHU(Image Data Handling Unit) which is one of the major unit in PDTS is capable of compression, storage, encryption and encoding. In this paper, the payload system of the EO based satellite is briefly introduced and the influence of the compression on AEISS is analyzed.

• 지능정보통신
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• 제7권2호
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• pp.68-74
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• 2006

• 한국항공우주학회지
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• 제37권8호
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• pp.798-804
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• 2009

(주)쎄트렉아이는 400kg 급 지구관측 위성의 주 탑재체로 사용될 고해상도 전자광학카메라, EOS-C 시스템을 개발 중이다. 이 시스템은 DubaiSat-1 위성의 주 탑재체 개발을 통해 획득한 경험을 토대로 보다 향상된 광기계 및 열적 성능을 갖도록 설계되었다. 민감한 광학부품의 운용상 성능을 유지하기 위해 히터를 이용한 능동 열제어 방식이 적용되었고, 이와 더불어 히터 소모 전력을 최소화하기 위해 열 코팅 및 다층박막단열재(MLI)를 사용한 수동 열제어 방식이 적용되었다. 열해석 모델을 이용해 임무궤도에 대한 열해석을 수행하였으며, 해석 결과를 바탕으로 이 시스템의 열제어계가 설계 요구조건을 만족하는 것을 확인하였다.