• 제목/요약/키워드: Thermal-optical analysis

검색결과 459건 처리시간 0.026초

저궤도 지구관측위성의 광학탑재체 지지구조물 설계 연구 (A Study on the Optical Bench for LEO Earth Observation Satellite)

  • 김경원;김진희;이주훈;진익민;김종우
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2005년도 춘계학술대회논문집
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    • pp.805-808
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    • 2005
  • This paper is a study on an optical bench satisfying stiffness and thermal pointing error requirements for LEO earth observation satellite. According to shape and stiffness requirements, optical bench type 1 is designed. Because type 1 does not satisfy the thermal pointing error requirement, an optical bench type 2 is suggested. Although the type 2 has better results than type 1, it still does not meet the thermal pointing error requirement. Using the results of optical bench type 1&2, the optical bench type 3 is finally designed, which satisfies both the stiffness and thermal pointing error requirements.

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MCPCB의 온도에 따른 고출력 LED의 광학적, 열적 영향력 분석 (Optical and Thermal Influence Analysis of High-power LED by MCPCB temperature)

  • 이승민;양종경;조주웅;이종찬;박대희
    • 전기학회논문지
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    • 제57권12호
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    • pp.2276-2280
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    • 2008
  • In this paper, we present thermal dependancy of LED package element by changing temperature of MCPCB for design high efficiency LED lamp, and confirmed influence of LED chip against temperature with analysis of thermal resistance and thermal capacitance. As increasing temperature, WPOs were decreased from 25 to 22.5 [%] and optical power were also decreased. that is decreased reason of optical power that forward voltage was declined by decrease of energy bandgap. Therefore optical power by temperature of MCPCB should consider to design lamp for street light and security light. Moreover, compensation from declined optical efficiency is demanded when LED package is composed. Also, thermal resistances from chip to metal PCB were decreased from 12.18 to 10.8[$^{\circ}C/W$] by changing temperature. Among the thermal resistances, the thermal resistance form chip to die attachment was decreased from 2.87 to 2.5[$^{\circ}C/W$] and was decreased 0.72[$^{\circ}C/W$] in Heat Slug by chaning temperature. Therefore, because of thermal resistance gap in chip and heat slug, reliability and endurance of high power LED affect by increasing non-radiative recombination in chip from heat.

Research on Thermal Refocusing System of High-resolution Space Camera

  • Li, Weiyan;Lv, Qunbo;Wang, Jianwei;Zhao, Na;Tan, Zheng;Pei, Linlin
    • Current Optics and Photonics
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    • 제6권1호
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    • pp.69-78
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    • 2022
  • A high-resolution camera is a precise optical system. Its vibrations during transportation and launch, together with changes in temperature and gravity field in orbit, lead to different degrees of defocus of the camera. Thermal refocusing is one of the solutions to the problems related to in-orbit defocusing, but there are few relevant thermal refocusing mathematical models for systematic analysis and research. Therefore, to further research thermal refocusing systems by using the development of a high-resolution micro-nano satellite (CX6-02) super-resolution camera as an example, we established a thermal refocusing mathematical model based on the thermal elasticity theory on the basis of the secondary mirror position. The detailed design of the thermal refocusing system was carried out under the guidance of the mathematical model. Through optical-mechanical-thermal integration analysis and Zernike polynomial calculation, we found that the data error obtained was about 1%, and deformation in the secondary mirror surface conformed to the optical index, indicating the accuracy and reliability of the thermal refocusing mathematical model. In the final ground test, the thermal vacuum experimental verification data and in-orbit imaging results showed that the thermal refocusing system is consistent with the experimental data, and the performance is stable, which provides theoretical and technical support for the future development of a thermal refocusing space camera.

복합재료를 사용한 지구관측위성 광학탑재체 지지구조물 개발 (Development of Composite Optical Bench for Earth observation Satellite)

  • 김진희;김경원;이주훈;진익민;윤길원
    • 한국복합재료학회:학술대회논문집
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    • 한국복합재료학회 2005년도 추계학술발표대회 논문집
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    • pp.207-210
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    • 2005
  • In this paper, technical issues for an optical bench of high precision LEO Earth observation satellite are described. The optical bench should be stable for thermal and dynamic environment. In this point of view, an intermediate type of optical bench is developed. Thermal deformation analysis and modal analysis are performed for two types of FE model. Modal test are performed to verify the analysis results. The test results fit well the analysis results.

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정지궤도위성의 해양관측센서 임무 궤도 열해석 (ON-ORBIT THERMAL ANALYSIS FOR THE GEOSTATIONARY OCEAN COLOR IMAGER OF A GEOSTATIONARY SATELLITE)

  • 김정훈;전형열
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2009년 춘계학술대회논문집
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    • pp.135-141
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    • 2009
  • A preliminary thermal analysis is performed for the optical payload system of a geostationary satellite. The optical payload considered in this paper is GOCI(Geostationary Ocean Color Imager) of COMS of Korea. The radiative and conductive thermal models are employed in order to predict thermal responses of the GOCI on the geostationary orbit. According to the results of this analysis are as follows: 1) the GOCI instrument thermal control is satisfactory to provide the temperatures for the GOCI performances, 2) the thermal control is defined and interfaces are validated, and 3) the entrance baffle temperature is found slightly out its specification, therefore further detailed analyses should be continued on this element.

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통신해양기상위성 해양탑재체 정지궤도 예비 열해석 (PRELIMINARY ON-ORBIT THERMAL ANALYSIS FOR THE GEOSTATIONARY OCEAN COLOR IMAGER OF COMS)

  • 김정훈;전형열;한조영
    • 한국전산유체공학회지
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    • 제15권1호
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    • pp.24-30
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    • 2010
  • A preliminary thermal analysis is performed for the optical payload system of a geostationary satellite. The optical payload considered in this paper is GOCI(Geostationary Ocean Color Imager) of COMS of Korea. The radiative and conductive thermal models are employed in order to predict thermal responses of the GOCI on the geostationary orbit. The results of this analysis are as follows: 1) the GOCI instrument thermal control is satisfactory to provide the temperatures for the GOCI performances, 2) the thermal control is defined and interfaces are validated, and 3) the entrance baffle temperature and shutter wheel motor gradient are found slightly out their specification, therefore further detailed analyses should be continued on these elements.

광 픽업의 열변형이 광학적 성능에 미치는 영향 (Effect of Thermal Deformation of Optical Pick-up Base on the Optical Performance)

  • 김홍민;조성훈;이자용;강신일
    • 한국소성가공학회:학술대회논문집
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    • 한국소성가공학회 2004년도 춘계학술대회 논문집
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    • pp.105-108
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    • 2004
  • The effect of thermal deformation of optical pick-up due to laser diode(LD) and LD driving integrated circuit on the optical performance of digital versatile disk(DVD) optical system was analyzed using the finite element analysis with initial surface residual stress conditions, and results were compared with the measured results with holographic interferometry. Ray tracing was performed using the deformed configuration of optical system.

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정지궤도위성 광학탑재체 복사 열제어 시스템 개념 설계 (A CONCEPTUAL DESIGN OF RADIATIVE THERMAL CONTROL SYSTEM IN A GEOSTATIONARY SATELLITE OPTICAL PAYLOAD)

  • 김정훈;전형열
    • 한국전산유체공학회지
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    • 제12권3호
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    • pp.62-68
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    • 2007
  • A conceptual thermal design is performed for the optical payload system of a geostationary satellite. The optical payload considered in this paper is GOCI(Geostationary Ocean Color Imager) of COMS of Korea. The radiative thermal control system is employed in order to expect a small thermal gradient in the telescope structure of GOCl. Two design margins are applied to the dedicated radiator dimensioning, and three kinds of configuration to the heater power sizing. A Monte-Carlo ray tracing method and a network analysis method are utilized to calculate radiative couplings and thermal responses respectively. At the level of conceptual design, sizing thresholds are presented for the radiator and heater on the purpose of determining the mass and power budget of the spacecraft.

Analysis of residual thermal stress in an aluminosilicate core and silica cladding optical fiber preform

  • Shin, Woo-Jin;K. Oh
    • 한국광학회:학술대회논문집
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    • 한국광학회 2000년도 제11회 정기총회 및 00년 동계학술발표회 논문집
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    • pp.214-215
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    • 2000
  • As silica based optical fibers and preforms are processed at a high temperature, residual stresses are bulit in the strucure when cooled down to the room temperature. The magnitude of the residual stress depends on the difference in the thermal expansion coefficients between core and cladding glass as well as on the temperature difference. Residual stress distribution determines the intrinsic strength and could affect the long term reliability of optical fibers. And furthermore, stress can introduces anisotropy into optical fibers by photoelastic effects. The analysis of thermal stress has been intensively studied for multimode fibers$^{(1)}$ and the authors and co-wokers recently reported the stress distribution in a depressed inner cladding structure$^{(2)}$ . The compositions of the glass in the previous studies, however, have been restricted to conventional glass formers, such as GeO2, B2O3, P2O5, Fluorine. (omitted)

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광학탑재체 지지구조물 열지향오차 해석기법 연구

  • 김경원;김진희;이주훈;진익민
    • 항공우주기술
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    • 제4권1호
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    • pp.45-48
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    • 2005
  • 본 논문은 광학탑재체 지지구조물의 열지향오차 해석기법에 대한 연구이다. 광학탑재체 지지구조물의 열지향오차 해석을 수행하기 위해서는 위성본체 전체의 유한요소모델을 필요로 한다. 그러나 광학탑재체 지지구조물의 초기 설계시 위성본체의 유한요소모델이 정해지지 않기 때문에, 열지향오차 해석시 유한요소모델이 존재하지 않더라도 위성본체에 의한 열지향오차를 유도하는 해석기법이 필요하게 된다. 본 논문에서는 이러한 해석기법과 실제 해석시 이를 반영하는 구체적인 방법에 대해서 서술한다.

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