• Title/Summary/Keyword: 전방관측적외선장비

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Development of a Geo-Pointing System of Helicopter-Mounted FLIR (헬기 장착 전방관측적외선장비 좌표지향시스템 개발)

  • Kim, Sung-Su;Shin, Yong-San;Kim, Sung-Soo;Kwon, Kang-Hun
    • Journal of the Korea Institute of Military Science and Technology
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    • v.12 no.6
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    • pp.750-759
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    • 2009
  • FLIR(Forward Looking Infrared) geo-pointing is a function that helps pilots to see a target within the field of view under all coordinates and attitudes of helicopter. Geo-pointing controls FLIR LOS(line of sight) toward known target coordinates by using azimuth and elevation angles calculated from several information such as helicopter coordinates and attitudes, a FLIR position from a GPS antenna, and target coordinates. Geo-pointing performance has been tested and evaluated on the ground to save flight test costs and ensure flight safety. In this paper, design and implementation of a geo-pointing system is described with the results of performance test conducted on the ground test system.

Optical system performance depending on the input wavefront distortion (입력 광파면 왜곡에 따른 광학계 성능)

  • 김연수;김현숙;김병윤;이윤우;송재봉
    • Proceedings of the Optical Society of Korea Conference
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    • 2001.02a
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    • pp.84-85
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    • 2001
  • 광학장비의 결상성능은 회절변조전달 성능(diffraction MTF) 이나 Strehl ratio 로 표시할 수 있다. 광학 렌즈 또는 거울의 표면 형상오차 등에 기인한 광학성능 저하는 이론적으로 잘 알려져 있으며, 입사동에서의 위상변조를 통하여 초분해능 광학계를 개발할려는 연구도 활발히 진행되고 있다. 헬기에 장착되어 야간 표적 획득 시스템으로 사용되고 있는 전방관측 적외선 열상장치는 볼 내부에 장착되며, 적외선 통과창으로서 이용되는 Ge 윈도우를 통하여 외부 영상을 획득한다. (중략)

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Analysis of IR lens mounting with elastomer (밀봉재를 이용한 적외선 렌즈 마운팅 분석)

  • 김연수;김현숙;최세철;김창우
    • Korean Journal of Optics and Photonics
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    • v.12 no.6
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    • pp.460-462
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    • 2001
  • We have analyzed the characteristics of IR lens mounting with elastomer and applied the results to the mounting of a silicon lens with diameter 117 mm which is the objective of a thermal imaging system. The elastomer, the 577 primerless silicone adhesive (Dow Corning Co.) which is heat cure type, and the mount material, A16061 are used for our analysis. Theoretical analysis gives the result that the space between lens and mount is required to be more than 250 ${\mu}{\textrm}{m}$ under the operational temperature conditions of -40~+6$0^{\circ}C$.

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