• 제목/요약/키워드: MTF1

검색결과 208건 처리시간 0.027초

Digital Image Simulation of Electro-Optical Camera(EOC) on KOMPSAT-1

  • Shim, Hyung-Sik;Yong, Sang-Soo;Heo, Haeng-Pal;Lee, Seung-Hoon;Oh, Kyoung-Hwan;Paik, Hong-Yul
    • 대한원격탐사학회:학술대회논문집
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    • 대한원격탐사학회 1999년도 Proceedings of International Symposium on Remote Sensing
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    • pp.349-354
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    • 1999
  • Electro-Optical Camera (EOC) is the main payload of the KOMPSAT-1 satellite to perform the mission of cartography that builds up a digital map of Korean territory including a digital terrain elevation map. This paper discusses the issues of the digital image simulation of EOC for the generation of EOC simulated scene as taken by EOC at 685km altitude on orbit. For the purpose, simulation work has been performed with the sensor models of EOC and the satellite platform motions models through image chain analysis from the illumination source (Sun) to a simulated image output in digital number. MODTRAN fur radiance calculation, MTF models of optics, detector and motions of EOC for system point spread function (PSF), and signal chain equations for digital number output are described. Several noise models of EOC are also considered. The final output is the EOC simulated image in digital number. The simulation technique can be used in several phase of a spaceborne electro-optical system development project, feasibility study phase, design, manufacturing, test phases, ground image processing phases, and so on.

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극소전자 디바이스를 위한 박막배선재료 개선에 관한 연구 (A Study on the improvement of Thin Film Interconnection Materials for Microelectronic Devices)

  • 양인철;김진영
    • 한국진공학회:학술대회논문집
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    • 한국진공학회 1995년도 제8회 학술발표회 논문개요집
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    • pp.057-58
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    • 1995
  • 극소전자 디바이스의 고집적화에 의해 박막배선의 선폭은 0.5$mu extrm{m}$ 이하로 축소되고 있고 상대적으로 높은 전류밀도가 흐르게 된다. 높은 전류밀도하에서는 현재 일반적으로 사용되고 있는 Al을 기본으로 하는 박막배선에서의 electromigration에 의한 결함 발생 그리고 비교적 낮은 전기전도도가 심각한 문제점으로 제기된다. 본 연구에서는 Al과 고전기전도도 물질인 Ag, Cu, 그리고 Au 박막배선에 대해 electromigration에 대한 저항성, 즉 activation energy를 측정 비교함으로써 차세대 극소전자 디바이스를 위한 박막배선재료로서의 가능성을 알아보고자 한다. Electromigration test 및 activation energy를 구하기 위해 순수 Ag, Cu, Al, Au 박막배선을 0.05$\mu\textrm{m}$ 두께, 100$\mu\textrm{m}$ 선폭, 그리고 5000$\mu\textrm{m}$ 길이로 SiO2 열산화막 처리된 pp-Si(100) 기판 위에 진공 증착시켰다. 가속화 실험을 위해 인가된 d.c. 전류밀도는 2$\times$106A/$ extrm{cm}^2$ 이었고, Al과 Au에서는 6$\times$106A/$\textrm{cm}^2$이었다. 실온에서 24$0^{\circ}C$까지의 온도범위에서 d.c.인가후의 저항변화를 측정하여 Median-Time-to-Failure(MTF)를 구한 후 Black 방정식을 이용하여 activation energy를 측정하였다. Activation energy는 Cu가 1.34eV로서 가장 높게 나타났고 Au가 1.01eV, Al이 0.66eV, Ag가 0.29eV의 순으로 측정되었다. 따라서 Cu와 Au 박막배선의 경우 Al보다 electromigration에 대한 저항력이 강한 고활성화에너지 특성을 갖는 고전기전도도 재료로서 차세대 극소전자 디바이스를 위한 대체 박막배선재료로서의 가능성을 보인다.

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별을 이용한 저궤도 광학 위성의 탑재체 영상 품질 측정 지표 및 자세 기동 연구

  • 유지웅;임동욱;박상영;손영종;이동한
    • 한국우주과학회:학술대회논문집(한국우주과학회보)
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    • 한국우주과학회 2009년도 한국우주과학회보 제18권2호
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    • pp.29.1-29.1
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    • 2009
  • 이 연구는 별 관측을 통해 점 퍼짐 함수(PSF)를 측정하고 나이퀴스트 주파수에서 변조 전달 함수(MTF)을 계산하여 주파수 영역에서 저궤도 광학 위성의 영상품질 평가방법을 도출하였다. 가상 별 영상을 생성하고 IRAF로 2차원의 점 퍼짐 함수를 얻었고 MATLAB으로 점 퍼짐 함수를 2차원 푸리에 변환하여 변조 전달함수를 계산하였다. 공간 영역에서는 점 퍼짐 함수의 모양을 통해서도 영상품질을 검증할 수 있다. Along/Across-Track의 모양이 일치하고 중심에서 좌우대칭이며 델타함수에 가까울수록 좋은 품질의 영상을 의미한다. Along/Across-Track의 점 퍼짐 함수 모양차이는 Line Rate나 Time Delay and Integration(TDI)의 오차에서 기인한다. 별을 점광원으로 본다면 점 퍼짐 함수를 정의하기 쉽고 Along/Across 방향을 동시에 측정 가능하다는 장점이 있다. 궤도상에서 별을 관측하는 것은 지상을 관측하는 것보다 대기 환경의 효과가 크지 않기 때문에 영상 품질 평가에 유리하다. Yaw Steering이나 Nadir Pointing과 같은 자세제어의 효과를 배제할 수 있으므로 자세제어의 효과가 상당 부분 제거된 영상품질을 분석할 수 있다. 지상관측시간이나 배터리 충전시간이 아닌 지구 본영에서 별을 관측하므로 임무에 방해받지 않는다. 지상관측과 같은 효과를 내고 TDI를 사용하는 환경을 구현하기위해 Line Rate를 고려한 자세 기동 방법에 대해 연구하였다. 큰 각도의 자세 기동이 예상되어 쿼터니안을 이용하여 Inertial Pointing하도록 자세 제어하였고, 자세 Slew Rate 구속조건 하에서 제어가 필요하다.

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Development of Integrated Simulation Tool for Jitter Analysis

  • Lee, Dae-Oen;Yoon, Jae-San;Han, Jae-Hung
    • International Journal of Aeronautical and Space Sciences
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    • 제13권1호
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    • pp.64-73
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    • 2012
  • Pointing stability of high precision observation satellites must satisfy the stringent requirements to perform at a designed level. As even a small vibrational disturbance can result in severe degradation of the optical performance, the effects of inorbit vibrational environment on the performance of optical payload must be predicted and analyzed in the design phase in order to ensure that the requirements imposed on the payload are fully met. In this paper, an integrated framework for the evaluation of the performance of optical payloads is developed. The developed simulation tool comprises of the reaction wheel induced disturbance model, state space model of a structure in modal form and Cassegrain reflector model. The performance degradation of the optical system due to jitter is expressed by using modulation transfer function (MTF) and image simulation. Moreover, vibration isolator model is also added to show the effectiveness of using a vibration isolator for the elimination of the effects of jitter in the acquisition of an image.

초박형 라이트필드 카메라의 실시간 분해능 향상 알고리즘 개발 (Improving Spatial Resolution in Real-time for Ultra-thin Light Field Cameras)

  • 김동건;유재관;조용진;김민혁
    • 한국컴퓨터그래픽스학회논문지
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    • 제27권3호
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    • pp.25-29
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    • 2021
  • 초박형 라이트필드 카메라 시스템은 이미지 센서 위에 렌즈 어레이를 부착하는 방식으로 만들어진다. 이러한 초박형 라이트필드 카메라는 하나의 이미지 센서를 여러 개의 sub-aperture가 나눠쓰는 방식으로 되어있어 개별 이미지의 분해능이 낮으며, sub-aperture 이미지들을 융합해 추가적인 분해능 향상이 수행되어야 한다. 본 연구에서는 초박형 라이트필드 카메라 시스템을 개발했으며, 개발된 카메라 시스템을 위한 실시간 분해능 향상 알고리즘을 개발, 실험을 통해 검증했다. 개발된 초박형 라이트필드 카메라는 두께 2mm, 24개(6×4)의 551×551 해상도의 sub-aperture로 구성되어 있으며, 임베디드 컴퓨팅 보드를 사용해 휴대가 가능하도록 제작되었다. 실시간 분해능 향상 알고리즘은 임베디드 컴퓨팅 보드의 GPU에서 병렬처리를 통해 라플라시안 피라미드 기반의 이미지 융합 알고리즘을 수행한다. 실험을 통해 검증한 결과로, 개발 시스템은 MTF50값이 평균 35% 정도 개선되었으며, 10.65fps의 처리속도로 실시간 처리가 가능함을 확인했다.

Design of Projection Optical System for Target Imaging Simulator with Long Exit Pupil Distance

  • Xueyuan Cao;Lingyun Wang;Guangxi Li;Ru Zheng
    • Current Optics and Photonics
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    • 제7권6호
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    • pp.745-754
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    • 2023
  • In order to test the recognition ability and accuracy of a target imaging simulator under the irradiation of solar stray light in a laboratory environment, it needs to be fixed on a five-axis turntable during a hardware-in-the-loop simulation test, so the optical system of the simulator should have a long exit pupil distance. This article adopts a secondary imaging method to design a projection optical system suitable for thin-film-transistor liquid crystal displays. The exit pupil distance of the entire optical system is 1,000 mm, and the final optimization results in the 400 nm-850 nm band show that the modulation transfer function (MTF) of the optical system is greater than 0.8 at the cutoff frequency of 72 lp/mm, and the distortion of each field of view of the system is less than 0.04%. Combined with the design results of the optical system, TracePro software was used to model the optical system, and the simulation of the target imaging simulator at the magnitude of -1 to +6 Mv was analyzed and verified. The magnitude error is less than 0.2 Mv, and the irradiance uniformity of the exit pupil surface is greater than 90%, which meets the requirements of the target imaging simulator.

Optomechanical Design of a Compact Imaging Spectrometer for a Microsatellite STSAT3

  • Lee, Jun-Ho;Lee, Chi-Weon;Kim, Yong-Min;Kim, Jae-Wook
    • Journal of the Optical Society of Korea
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    • 제13권2호
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    • pp.193-200
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    • 2009
  • A compact imaging spectrometer (COMIS) is currently under development for use in the STSAT3 microsatellite. COMIS images the Earth's surface and atmosphere with ground sampling distances of ${\sim}30m$ in the $18{\sim}62$ spectral bands ($4.0{\sim}1.05{\mu}m$) for the nadir looking at an altitude of 700 km. COMIS has an imaging telescope and an imaging spectrometer box into which three electronics PCBs are embedded. These are designed into a single assembly with dimensions of 35(L) $\times$ 20(W) $\times$ 12(H) $cm^3$ and a mass of 4.3 kg. Optomechanical design efforts are focused on manufacturing ease, alignment, assembly, testing and improved robustness in space environments. Finite element analysis demonstrates that COMIS will survive in launch and space environments and perform the system modulation transfer function (MTF) in excess of 0.29 at the Nyquist frequency of the CCD detector (38.5 lines-per-mm).

Design and Analysis of a 10× Optical Zoom System for an LWIR Camera

  • Ok, Chang-Min;Park, Sung-Chan
    • Journal of the Optical Society of Korea
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    • 제18권5호
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    • pp.574-581
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    • 2014
  • This paper presents the design and evaluation of the optical zoom system for an LWIR camera. The 12.8operating wavelength range of this system is from $7.7{\mu}m$ to $12.8{\mu}m$. Through a paraxial design and optimization process, we have obtained the extended four-group inner-focus zoom system with focal lengths of 10 to 100 mm, which consists of the six lenses including four aspheric surfaces and two diffractive surfaces. The diffractive lenses were used to balance the higher-order aberrations, and its diffraction properties were evaluated by scalar diffraction theory. We have calculated the polychromatic integrated diffraction efficiency and the MTF drop generated by background noise. The f-number of the zoom system is F/1.4 at all positions. Fields of view are given by $51.28^{\circ}{\times}38.46^{\circ}$ at wide field and $5.50^{\circ}{\times}4.12^{\circ}$ at narrow field positions. In conclusion, this design procedure results in a $10{\times}$ compact zoom lens system useful for an LWIR camera.

Optical System Design for Thermal Target Recognition by Spiral Scanning [TRSS]

  • Kim, Jai-Soon;Yoon, Jin-Kyung;Lee, Ho-Chan;Lee, Jai-Hyung;Kim, Hye-Kyung;Lee, Seung-Churl;Ahn, Keun-Ok
    • Journal of the Optical Society of Korea
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    • 제8권4호
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    • pp.174-181
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    • 2004
  • Various kinds of systems, that can do target recognition and position detection simultaneously by using infrared sensing detectors, have been developed. In this paper, the detection system TRSS (Thermal target Recognition by Spiral Scanning) adopts linear array shaped uncooled IR detector and uses spiral type fast scanning method for relative position detection of target objects, which radiate an IR region wavelength spectrum. It can detect thermal energy radiating from a 9 m-size target object as far as 200 m distance. And the maximum field of a detector is fully filled with the same size of target object at the minimum approaching distance 50 m. We investigate two types of lens systems. One is a singlet lens and the other is a doublet lens system. Every system includes one aspheric surface and free positioned aperture stop. Many designs of F/1.5 system with ${\pm}5.2^{\circ}$ field at the Efl=20, 30 mm conditions for single element and double elements lens system respectively are compared in their resolution performance [MTF] according to the aspheric surface and stop position changing on their optimization process. Optimum design is established including mechanical boundary conditions and manufacturing considerations.

A Miniaturized Catadioptric Laser-Irradiation-Precision Test System

  • Liu, Huan;Sun, Hao;Wang, Chunyan
    • Current Optics and Photonics
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    • 제5권2호
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    • pp.164-172
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    • 2021
  • In this paper a catadioptric laser-irradiation-precision test system is designed, to achieve a high-precision laser-irradiation-accuracy test. In this system, we adopt the method of imaging the entire target surface at a certain distance to realize the measurement of laser-irradiation precision. The method possesses the advantages of convenient operation, high sensitivity, and good stability. To meet the test accuracy requirement of 100 mm/km (0.01%), the coma, field curvature, and distortion over the entire field of view should be eliminated from the optical system's design. Taking into account the whole length of the tube and the influence of stray light on the structure type, a catadioptric system with a hood added near the primary imaging surface is designed. After optimization using the ZEMAX software, the modulation transfer function (MTF) of the designed optical system is 0.6 at 30 lp/mm, the full-field-of-view distortion is better than 0.18%, and the energy concentration in the 10-㎛-radius surrounding circle reaches about 90%. The illumination-accuracy test results show that the measurement accuracy of the radiation hit rate is better than 50 mm when the test distance is 1 km, which is better than the requirement of 100 mm/km for the laser-irradiation-accuracy test.