• 제목/요약/키워드: Orbit Element

검색결과 74건 처리시간 0.017초

MIRIS 우주관측카메라의 기계부 개발 (DEVELOPMENT OF THE MECHANICAL STRUCTURE OF THE MIRIS SOC)

  • 문봉곤;정웅섭;차상목;이창희;박성준;이대희;육인수;박영식;박장현;남욱원;;;양순철;이선희;이승우;한원용
    • 천문학논총
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    • 제24권1호
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    • pp.53-64
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    • 2009
  • MIRIS is the main payload of the STSAT-3 (Science and Technology Satellite 3) and the first infrared space telescope for astronomical observation in Korea. MIRIS space observation camera (SOC) covers the observation wavelength from $0.9{\mu}m$ to $2.0{\mu}m$ with a wide field of view $3.67^{\circ}\times3.67^{\circ}$. The PICNIC HgCdTe detector in a cold box is cooled down below 100K by a micro Stirling cooler of which cooling capacity is 220mW at 77K. MIRIS SOC adopts passive cooling technique to chill the telescope below 200 K by pointing to the deep space (3K). The cooling mechanism employs a radiator, a Winston cone baffle, a thermal shield, MLI (Multi Layer Insulation) of 30 layers, and GFRP (Glass Fiber Reinforced Plastic) pipe support in the system. Optomechanical analysis was made in order to estimate and compensate possible stresses from the thermal contraction of mounting parts at cryogenic temperatures. Finite Element Analysis (FEA) of mechanical structure was also conducted to ensure safety and stability in launching environments and in orbit. MIRIS SOC will mainly perform Galactic plane survey with narrow band filters (Pa $\alpha$ and Pa $\alpha$ continuum) and CIB (Cosmic Infrared Background) observation with wide band filters (I and H) driven by a cryogenic stepping motor.

우주개발동향과 주요 이슈 (Trend of Space Development and Issue)

  • 조홍제;신용도
    • 항공우주정책ㆍ법학회지
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    • 제29권1호
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    • pp.97-126
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    • 2014
  • October 4, 1957 the Soviet Sputnik 1 was launched into space the first time in the history of mankind. After launching, the realm of humankind was expanded to space. Today all countries of the world wage a fierce competition in order to utilize space for various purposes. World powers of space such as United States, Russia, China, and Japan, put reconnaissance satellites and ocean surveillance satellites into orbit, being able to easily see equipment and troops movement on earth. Each country makes efforts to occupy space assets through the militarization of space and expand national interests. Recently private companies or individuals involved in commercial space activities are becoming more prevalent. Thus, in addition to space activities for military purposes, commercial space activities become widespread. Individuals and private companies as well as nations are also involved in space activities. Outer space is not the monopoly of space powers such as the United States and Russia. The whole human race can benefit from free access to space, being the common heritage of mankind. In particular, outer space becomes an indispensable element of military activities and human life. Many countries are now entering space development, putting a lot of budget into new development programs. Republic of Korea also built the Narodo Space Center, starting its space development with budget and manpower. We have to find out ways to use space not only for military purposes but also for commercial space activities that can contribute to the national economy. In addition, through the joint efforts of the international community, we have to make efforts for preservation and peaceful use of space. Various issues relating to space activities and research should be studies in order to contribute to the progress of humanity. Those issues include the definition of outer space, space debris reduction and environmental conservation issues, non-bind measure cooperation - European International Code of Conduct, space law and national legislation related empowerment issues, arms control measures in space, and restrictions on the use of nuclear fuel. We also need to be involved in the discussion of those issues as one of responsible space countries. In addition, we try to find out regional cooperation schemes such as the ESA in the Europe actively. Currently in the Northeast Asia, cooperation bodies led by Japan and China respectively, are operated in the confrontational way. To avoid such confrontation, a new cooperative body needs to be established for cooperation on space exploration and information. The system to allow the exchange of satellite information for early warning of natural disasters needs to be built as well. In addition, efforts to enhance the effectiveness of the relevant international treaties on space, and fill in the blanks in international space laws should be made at the same time. To this end, we have to do a leading role in the establishment of standards such as non-binding measures (resolution) - Code of Conduct, being discussed in the UN and other organizations, and compliance with those standards. Courses in aerospace should be requires in law schools and educational institutes, and professional manpower need to be nurtured. In addition, the space-related technology and policy needs to be jointly studied among the private, public, and military groups, and the cross exchange among them should be encouraged.

PAT 기반 온도장 보간을 이용한 관측위성의 열지향오차해석 (Thermal pointing error analysis of the observation satellites with interpolated temperature based on PAT method)

  • 임재혁;김선원;김정훈;김창호;전형열;오현철;신창민;이병채
    • 한국항공우주학회지
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    • 제44권1호
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    • pp.80-87
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    • 2016
  • 본 논문에서는 계절 및 주야의 온도변화를 고려한 관측위성의 열지향오차해석을 실시한다. 관측위성은 임무수행기간 동안 다채널의 관측센서를 이용해서 지구표면의 영상을 촬영한다. 그러나 주야 및 계절별로 최대 200도의 온도환경 차이가 발생하며 이로 인해 관측센서 및 별추적기의 시선벡터가 변화되고 정해진 목표지점의 영상촬영이 어렵다. 이런 문제를 사전예측하고 대응하기 위해서 열지향오차해석을 실시한다. 우선 궤도열환경해석으로부터 도출된 성긴 온도장 정보를 상세한 구조유한요소모델에 PAT기법을 이용해 보간하여 온도변화에 따른 열변형해석을 수행하였다. PAT로 보간된 온도분포의 정확도를 검증하였으며, 열변형해석결과로부터 열지향오차를 도출하였다.

분석툴을 이용한 천리안2A 기상탑재체 복사 보정 파라미터 검증 (Verification of GEO-KOMPSAT-2A AMI Radiometric Calibration Parameters Using an Evaluation Tool)

  • 진경욱;박진형
    • 대한원격탐사학회지
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    • 제36권6_1호
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    • pp.1323-1337
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    • 2020
  • 천리안2A호 AMI(Advanced Meteorological Imager) 복사 보정에 대한 검증은 탑재체의 기능 및 성능 점검뿐만 아니라, 탑재체 자료의 품질을 결정 짓는 중요한 요소이다. AMI 탑재체는 여섯 개의 가시 및 근적외 채널과 10개의 열적외 채널로 구성되어 있다. 가시/근적외 채널의 복사 성능을 대표하는 핵심적인 파라미터로는 SNR(Signal-to-Noise Ratio), 열적외채널의 경우는 NEdT(Noise Equivalent delta Temperature)를 들 수 있다. 다이나믹 레인지와 검출기의 반응도와 관련된 Gain 값 또한 복사 보정 성능과 관련된 중요한 파라미터이다. AMI 탑재체의 주요 복사 보정 성능 검증을 위해, 실시간 AMI자료 처리 시스템과는 별도의 오프라인 복사 성능 분석 툴을 개발하였다. 개발된 분석 툴을 이용하여 천리안2A호 발사 후 궤도상 시험 기간 동안 검증 작업을 수행하였다. 분석 툴을 통한 계산 결과는 탑재체 개발업체인 HARRIS사의 분석 값과 비교 검증하였다. AMI 복사 성능 검증 작업은 총 세차례로 나누어 AMI탑재체 양쪽 면인 Side1과 Side2에 대해 이루어졌다. 복사 성능 검증 결과 주요 복사 보정 파라미터들의 성능은 요구조건 값들을 크게 상회하는 우수한 성능을 보여 주었으며, AMI 복사 성능 분석 툴의 유효성이 입증되었다.