• 제목/요약/키워드: Optical Observation

검색결과 752건 처리시간 0.039초

NEW RETRIEVAL METHOD FOR AEROSOL OPTICAL PARAMETERS USING DIRECTIONAL REFLECTANCE AND POLARIZATION DATA BY POLDER ON BOARD ADEOS

  • Kawata, Yoshiyuki;Izumiya, Toshiaki
    • 대한원격탐사학회:학술대회논문집
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    • 대한원격탐사학회 1999년도 Proceedings of International Symposium on Remote Sensing
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    • pp.95-99
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    • 1999
  • We proposed a new retrieval method for aerosol's real part of refractive index, optical thickness, and Angstrom exponent using POLDER's directional reflectance and polarization data. We showed that aerosol's real part of refractive index can be retrieved systematically using multi-directional PR(polarization and reflectance) diagrams in a single infrared band by our algorithm for the first time. We examined the retrieved results, by comparing with the simultaneously measured sky observation data at the study site and we obtained a reasonable agreement between them.

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Ficin처리시 우육의 단백질 분해에 관한 연구 IV. 광학 현미경에 의한 관찰 (Studies on the Digestion of Beef by Ficin Treatment : IV. An Optical Microscopic Observation)

  • 김정숙;주순재
    • 한국식품영양학회지
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    • 제1권2호
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    • pp.9-17
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    • 1988
  • The morphological changes of fresh beef treated with ficin(0.1% : 2hrs, 6hrs) were examined with optical microscope (OM, LM), the results obtained were as follows : Connective tissue protein in fresh beef treated with ficin was occurred swelling and separation of endomysial reticulum with time, followed showing granulation and solubilization slightly. Myofibrillar protein was loosed wavy contractile muscle fiber, and showed erosin, cracks and breaks in fibers with time.

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소형 위성용 지구관측 광학카메라의 시험모델 평가 (Performance Evaluation of An Earth Observation Camera for Small Satellites)

  • 양호순;강명석;정성근;최영완;김이을;양승욱;김종운;윤지호;김도형
    • 한국광학회:학술대회논문집
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    • 한국광학회 2003년도 하계학술발표회
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    • pp.134-135
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    • 2003
  • Medium-sized Aperture Camera (MAC)는 근적도궤도(Near Equatorial Orbit) 지구관측위성 MACSAT의 주탑재체로, 우리나라의 (주)쎄트렉아이와 말레이시아의 ATSB社와 오는 2004년 발사를 목표로 공동 개발되고 있다. MAC은 push-broom 방식의 전자광학 탑재체로, 지상해상도 2.5 m를 가지는 PAN band 1개, 지상해상도 5 m를 가지는 Multi-Spectral band 4 개를 가지고, 지상의 swath width는 20 km를 가진다. (중략)

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초정밀 단일점 다이아몬드 터닝을 이용한 비구면 금속 부반사경 가공 (Ultra-precision single point diamond turning (SPDT) on an aspheric metal secondary mirror)

  • Kim, E. D.;H. S. Yang;Kim, G-H.
    • 한국광학회:학술대회논문집
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    • 한국광학회 2001년도 제12회 정기총회 및 01년도 동계학술발표회
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    • pp.96-97
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    • 2001
  • A 110 mm diameter aspheric metal secondary mirror for a test model of an earth observation satellite camera was fabricated by ultra-precision single point diamond turning (SPDT) . Without a conventional polishing process, the surface texture of R$\sub$a/=2.8 nm, and the form error of R$\sub$a/=0.05 λ has been stably achieved In a laboratory condition. (omitted)

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Minimum Number of Observation Points for LEO Satellite Orbit Estimation by OWL Network

  • Park, Maru;Jo, Jung Hyun;Cho, Sungki;Choi, Jin;Kim, Chun-Hwey;Park, Jang-Hyun;Yim, Hong-Suh;Choi, Young-Jun;Moon, Hong-Kyu;Bae, Young-Ho;Park, Sun-Youp;Kim, Ji-Hye;Roh, Dong-Goo;Jang, Hyun-Jung;Park, Young-Sik;Jeong, Min-Ji
    • Journal of Astronomy and Space Sciences
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    • 제32권4호
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    • pp.357-366
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    • 2015
  • By using the Optical Wide-field Patrol (OWL) network developed by the Korea Astronomy and Space Science Institute (KASI) we generated the right ascension and declination angle data from optical observation of Low Earth Orbit (LEO) satellites. We performed an analysis to verify the optimum number of observations needed per arc for successful estimation of orbit. The currently functioning OWL observatories are located in Daejeon (South Korea), Songino (Mongolia), and Oukaïmeden (Morocco). The Daejeon Observatory is functioning as a test bed. In this study, the observed targets were Gravity Probe B, COSMOS 1455, COSMOS 1726, COSMOS 2428, SEASAT 1, ATV-5, and CryoSat-2 (all in LEO). These satellites were observed from the test bed and the Songino Observatory of the OWL network during 21 nights in 2014 and 2015. After we estimated the orbit from systematically selected sets of observation points (20, 50, 100, and 150) for each pass, we compared the difference between the orbit estimates for each case, and the Two Line Element set (TLE) from the Joint Space Operation Center (JSpOC). Then, we determined the average of the difference and selected the optimal observation points by comparing the average values.