• Title/Summary/Keyword: 과학기술위성 3호

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과학기술위성3호 주탑재체 MIRIS의 과학연구 활용

  • Lee, Seong-Ho;Park, Jang-Hyeon;Han, Won-Yong;Nam, Uk-Won;Yuk, In-Su;Jin, Ho;Park, Yeong-Sik;Lee, Dae-Hui;Jeong, Ung-Seop;Lee, Chang-Hui;Park, Seong-Jun;Lee, Hyeong-Mok;Gu, Bon-Cheol;Im, Myeong-Sin;Park, Su-Jong;Song, In-Ok;Seon, Gwang-Il;Jo, Jeong-Yeon;An, Gyeong-Jin;Matsumoto, T.
    • Bulletin of the Korean Space Science Society
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    • 2008.04a
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    • pp.27.2-27.2
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    • 2008
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An Algorithm of Dynamic Resource Management for QoS Guarantee Across Ka-band Satellite ATM Systems (Ka 밴드 위성 ATM망에서 QoS 보장을 위한 동적 자원 관리 알고리즘)

  • Ha, Eun-Ju;Park, Jong-Tae
    • Journal of KIISE:Information Networking
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    • v.27 no.3
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    • pp.381-388
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    • 2000
  • 광대역 종합 정보 통신망이나 인터넷과 같은 대규모의 망에서 고 품질의 서비스 보장은 점점 더 중요해지고 있다. 비동기식 전송 모드(ATM)는 고 품질의 서비스 보장을 위해 채택된 가장 강력한 기술이다. 위상은 한정된 자원(대역폭)을 가지고 있다. 따라서, 하부의 ATM 망과 Ka 밴드 위성을 연결하여 광범위한 대역폭을 요구하는 다양한 멀티미디어 서비스들을 효과적으로 제공하기 위해서고 품질의 서비스를 보장해 주는 효율적인 동적 자원관리 방법이 절실히 요구된다. 본 논문에서 Ka 밴드 위성 ATM 망에서 고 품질의 서비스를 보장해 주는 효율적인 동적 자원 관리 알고리즘을 새롭게 제안하였다. 제안된 동적 대역폭 제어 알고리즘은 다양한 성능분석을 통해 호 손실률 측면에서 기존의 방법에 비해 훨씬 향상된 성능을 보여준다.

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Design of S-band Turnstile Antenna Using the Parasitic Monopole (기생 모노폴을 이용한 S-band Turnstile 안테나 설계)

  • Lee, Jung-Su;Oh, Chi-Wook;Seo, Gyu-Jae;Oh, Seung-Han
    • The Journal of Korean Institute of Electromagnetic Engineering and Science
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    • v.17 no.11 s.114
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    • pp.1082-1088
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    • 2006
  • A turnstile antenna using the parasitic monopole has been developed for STSAT-2 TT&C application. The antenna consists of two radiating elements; a bow-tie dipole and a parasitic monopole. The bow-tie dipole is main radiating element, used a bow-tie structure for bandwidth improvement and size reduction. The parasitic monopole improved beamwidth and axial ratio. The input impedance of the antenna is about 50 ohm without a matching circuit. The proposed antenna has beamwidth of $>140^{\circ}$, axial ratio of < 3 dB and VSWR of < 1.5 in the band of $2.075{\sim}2.282GHz$.

Geometric Modelling and Coordinate Transformation of Satellite-Based Linear Pushbroom-Type CCD Camera Images (선형 CCD카메라 영상의 기하학적 모델 수립 및 좌표 변환)

  • 신동석;이영란
    • Korean Journal of Remote Sensing
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    • v.13 no.2
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    • pp.85-98
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    • 1997
  • A geometric model of pushbroom-type linear CCD camera images is proposed in this paper. At present, this type of cameras are used for obtaining almost all kinds of high-resolution optical images from satellites. The proposed geometric model includes not only a forward transformation which is much more efficient. An inverse transformation function cannot be derived analytically in a closed form because the focal point of an image varies with time. In this paper, therefore, an iterative algorithm in which a focal point os converged to a given pixel position is proposed. Although the proposed model can be applied to any pushbroom-type linear CCD camera images, the geometric model of the high-resolution multi-spectral camera on-board KITSAT-3 is used in this paper as an example. The flight model of KITSAT-3 is in development currently and it is due to be launched late 1998.

과학기술위성 3호 주탑재체 MIRIS의 우주관측 카메라 과학임무

  • Lee, Seong-Ho;Han, Won-Yong;Park, Jang-Hyeon;Nam, Uk-Won;Yuk, In-Su;Jin, Ho;Lee, Dae-Hui;Park, Yeong-Sik;Jeong, Ung-Seop;Lee, Chang-Hui;Park, Seong-Jun;Lee, Hyeong-Mok;Gu, Bon-Cheol;Im, Myeong-Sin;Park, Su-Jong;Song, In-Ok;Seon, Gwang-Il;Jo, Jeong-Hyeon;Matsumoto, Matsumoto;An, Gyeong-Jin
    • The Bulletin of The Korean Astronomical Society
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    • v.33 no.1
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    • pp.44.1-44.1
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    • 2008
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TRIO-CINEMA의 환경시험 및 결과 분석

  • Geum, Gang-Hun;U, Ju;Lee, Seong-Hwan;Lee, Yong-Seok;Jeon, Je-Heon;Chae, Gyu-Seong;Jin, Ho;Seon, Jong-Ho;Lee, Dong-Hun;Thomas, Immel;Lin, Robert P.
    • The Bulletin of The Korean Astronomical Society
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    • v.37 no.2
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    • pp.167.2-167.2
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    • 2012
  • 경희대학교와 UC Berkeley, Imperial College London에서 공동으로 진행하는 TRIO-CINEMA Mission(TRiplet Ionosphere Observatory-Cubesat for Ion, Neutral, Electron and MAgnetic fields)은 총 3기의 초소형 위성으로 구성되어 있다. 3기의 위성은 고도 650~800km 상공의 태양동주기 궤도운동을 예상하고 있으며, 지구 근접공간의 입자 검출과 자기장 측정의 과학 임무를 맡게 된다. TRIO-CINEMA 비행 모델(Flight Model)의 환경시험은 진동시험과 열진공시험으로 진행되었다. 진동시험은 X, Y, Z 세 축에 대해 Sine 과 Random 모드로 진행되었다. TRIO-CINEMA가 탑재 될 러시아의 드네프르 로켓의 요구사항은 각 축에서 20Hz 이상의 고유진동수, Sine의 경우 최대 0.8G와 4oct/min Sweep Rate, Random의 경우 5.2Grms 와 35초의 지속시간에서의 안정성을 만족하는 것이다. 시험 결과 TRIO-CINEMA가 요구사항을 모두 만족시키는 것을 확인하였다. 또한, 열 주기 시험(Thermal Cycling Test)을 진행하여 우주공간에서 위성 시스템이 정상 동작하는지에 대한 신뢰성을 검증하였다. 열주기 시험은 미국 MIL표준 값을 참고하여 $10^{-6}Torr$에서 $-20{\sim}30^{\circ}C$의 온도를 주었으며, 시험을 진행하는 동안과 시험 후에 위성이 정상작동 함을 확인하였다. 이에 본 연구의 시험 방법과 그 결과를 기술하였다.

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KSR-III 액체추진기관 연소시험

  • 하성업;류철성;조남경;설우석
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2000.11a
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    • pp.6-6
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    • 2000
  • 국가우주개발 중장기 계획에 의거, 독자 인공위성 발사체 개발에 필요한 필수기술을 확보하기 위하여 액체추진제 로켓엔진의 개발에 대한 필요성이 대두되었으며, 이에 따라 한국항공우주연구소는 과학로켓 3호(KSR-III)에 적용하기 위한 액체추진기관을 개발하고 있다. 이러한 목적으로 kerosine/LOx를 사용하며 13톤급의 추력을 낼 수 있는 시제엔진이 설계, 제작되었으며 이 엔진에 대한 연소시험이 실시되었다. 본 연구에서는 액체추진기관 시험을 위한 일련의 진행사항, 시험방법을 소개하며, 시험을 통하여 획득한 정특성 자료 및 동특성 자료에 대하여 분석하였다.(중략)

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Example of Legislation on the Space Relations of Every Countries in the World and Main Contents of the Space Exploration Promotion Act and Future Task in Korea (세계 각국의 우주관계 입법례와 우리나라 우주 개발진흥법의 주요내용 및 앞으로의 과제)

  • Kim, Doo-Hwan
    • The Korean Journal of Air & Space Law and Policy
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    • v.20 no.1
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    • pp.9-43
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    • 2005
  • The Korean government established her first "National Space Program" in 1996, and revised it in 2000 and 2005. As embedded in the National Space Program, Korea aims to become one of the world's top countries in space technology by 2010. All of 13 satellites are planned to be put into orbit as schematized, which include 7 multi-purpose satellites, 4 science satellites and 2 geostationary orbit satellites. The Space Center in Korea is to be built at Woinara-Do, Bongrae-Myon, Koheung-Goon, Junlanam Province on the southern coast of the Korean peninsular. The first phase of the construction of the space center will be finished by 2007 for launch of KSLV-l. This will make Korea be the 13th advanced country in space development having a launching site in the world. The "Space Center" will serve as the infrastructure for the development of space technology and related technology, and plan to launch a low earth orbit satellite in 2007. A second science satellite made in Korea will be launched from the space center by 2007. From 2010, the center will be operated on a commercial basis operating launch facilities for low-to mid-altitude orbit satellites. Since the 'Aircraft Industry Promotion Act' was replaced by the 'Aerospace Industry Development Promotion Acf of 1987, this Act had been amended seven times from 1991 year to 2004. Most of developed countries has been enacted the space law including the public or private items such as an (1)DSA, (2)Russia, (3)the United Kingdom, (4)Germany, (5)France, (6)Canada, (7)Japan, (8)Sweden, (9)Australia, (10)Brazil, (11)Norway, (12)South Africa, (13)Argentina, (14)Chile, (15)Ukrainian etc. As the new Space Exploration Promotion Act was passed by the resolution of the Korean Congress on May 3, 2005, so the Korean government has made the public proclamation the abovementioned Act on May 31, this year. This Act takes effect on December 1, 2005 after elapsing six months from the date of promulgation. The main contents of Space Exploration Promotion Act of 2005 is as the following (1)establishing a basic plan for promoting space exploration, (2)establishment and function of national space committee, (3)procedure and management of domestic and international registration of space objects, (4)licensing of launch by space launch vehicles, (5)lability for damages caused by space accidents and liability insurance, (6) organizing and composition of the space accident investigation committee, (7)Support of non-governmental space exploration project, (8)Requesting Support and Cooperation of Space Exploration, (9)Rescue of Astronauts and Restitution of Space Objects, etc.. In oder to carry out successfully the medium and long basic plan for promoting space exploration and to develope space industry in Korea, I think that it is necessary for us to enlarge and to reorganize the function and manpower of the Space Technology Development Division of the Ministry of Science & Technology and the Korea Aerospace Research Institute. Korea has been carrying out its space program step by step according to the National Space Program. Korea also will continually strengthen the exchange and cooperation with all the countries in the world under the principle of equality, friendship relations and mutual benefits. Together with all other peoples around the globe, Korea will make due contribution towards the peaceful utilization of space resources and promotion of human progress and prosperity.

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Comparison of rainfall-runoff performance based on various gridded precipitation datasets in the Mekong River basin (메콩강 유역의 격자형 강수 자료에 의한 강우-유출 모의 성능 비교·분석)

  • Kim, Younghun;Le, Xuan-Hien;Jung, Sungho;Yeon, Minho;Lee, Gihae
    • Journal of Korea Water Resources Association
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    • v.56 no.2
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    • pp.75-89
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    • 2023
  • As the Mekong River basin is a nationally shared river, it is difficult to collect precipitation data, and the quantitative and qualitative quality of the data sets differs from country to country, which may increase the uncertainty of hydrological analysis results. Recently, with the development of remote sensing technology, it has become easier to obtain grid-based precipitation products(GPPs), and various hydrological analysis studies have been conducted in unmeasured or large watersheds using GPPs. In this study, rainfall-runoff simulation in the Mekong River basin was conducted using the SWAT model, which is a quasi-distribution model with three satellite GPPs (TRMM, GSMaP, PERSIANN-CDR) and two GPPs (APHRODITE, GPCC). Four water level stations, Luang Prabang, Pakse, Stung Treng, and Kratie, which are major outlets of the main Mekong River, were selected, and the parameters of the SWAT model were calibrated using APHRODITE as an observation value for the period from 2001 to 2011 and runoff simulations were verified for the period form 2012 to 2013. In addition, using the ConvAE, a convolutional neural network model, spatio-temporal correction of original satellite precipitation products was performed, and rainfall-runoff performances were compared before and after correction of satellite precipitation products. The original satellite precipitation products and GPCC showed a quantitatively under- or over-estimated or spatially very different pattern compared to APHPRODITE, whereas, in the case of satellite precipitation prodcuts corrected using ConvAE, spatial correlation was dramatically improved. In the case of runoff simulation, the runoff simulation results using the satellite precipitation products corrected by ConvAE for all the outlets have significantly improved accuracy than the runoff results using original satellite precipitation products. Therefore, the bias correction technique using the ConvAE technique presented in this study can be applied in various hydrological analysis for large watersheds where rain guage network is not dense.

Sensitivity Analysis for CAS500-4 Atmospheric Correction Using Simulated Images and Suggestion of the Use of Geostationary Satellite-based Atmospheric Parameters (모의영상을 이용한 농림위성 대기보정의 주요 파라미터 민감도 분석 및 타위성 산출물 활용 가능성 제시)

  • Kang, Yoojin;Cho, Dongjin;Han, Daehyeon;Im, Jungho;Lim, Joongbin;Oh, Kum-hui;Kwon, Eonhye
    • Korean Journal of Remote Sensing
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    • v.37 no.5_1
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    • pp.1029-1042
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    • 2021
  • As part of the next-generation Compact Advanced Satellite 500 (CAS500) project, CAS500-4 is scheduled to be launched in 2025 focusing on the remote sensing of agriculture and forestry. To obtain quantitative information on vegetation from satellite images, it is necessary to acquire surface reflectance through atmospheric correction. Thus, it is essential to develop an atmospheric correction method suitable for CAS500-4. Since the absorption and scattering characteristics in the atmosphere vary depending on the wavelength, it is needed to analyze the sensitivity of atmospheric correction parameters such as aerosol optical depth (AOD) and water vapor (WV) considering the wavelengths of CAS500-4. In addition, as CAS500-4 has only five channels (blue, green, red, red edge, and near-infrared), making it difficult to directly calculate key parameters for atmospheric correction, external parameter data should be used. Therefore, thisstudy performed a sensitivity analysis of the key parameters (AOD, WV, and O3) using the simulated images based on Sentinel-2 satellite data, which has similar wavelength specifications to CAS500-4, and examined the possibility of using the products of GEO-KOMPSAT-2A (GK2A) as atmospheric parameters. The sensitivity analysisshowed that AOD wasthe most important parameter with greater sensitivity in visible channels than in the near-infrared region. In particular, since AOD change of 20% causes about a 100% error rate in the blue channel surface reflectance in forests, a highly reliable AOD is needed to obtain accurate surface reflectance. The atmospherically corrected surface reflectance based on the GK2A AOD and WV was compared with the Sentinel-2 L2A reflectance data through the separability index of the known land cover pixels. The result showed that two corrected surface reflectance had similar Seperability index (SI) values, the atmospheric corrected surface reflectance based on the GK2A AOD showed higher SI than the Sentinel-2 L2A reflectance data in short-wavelength channels. Thus, it is judged that the parameters provided by GK2A can be fully utilized for atmospheric correction of the CAS500-4. The research findings will provide a basis for atmospheric correction of the CAS500-4 in the future.