• Title/Summary/Keyword: Synthetic Aperture Rader

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위성 영상 레이다(Synthetic Aperture Radar) 기술 현황과 발전 추세

  • Gwak, Yeong-Gil
    • The Proceeding of the Korean Institute of Electromagnetic Engineering and Science
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    • v.22 no.1
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    • pp.88-106
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    • 2011
  • 최근 고해상도의 영상 레이다(Syntetic Aperture Radar. SAR) 기술의 급속한 발전으로 기상의 변화에 관계없이 전천후로 지구의 환경 변화를 관측하거냐 고정밀도의 표적 탐지 및 식별이 가능해짐에 따라 레이다 영상을 이용한 활용 분야가 군사 목적의 정밀 감시 정찰뿐만 아니라 과학 및 민수용으로도 활용범위가 넓어지고 있다. SAR의 역사는 1950년대부터 약 50년의 기술 역사를 가지고 있지만 2010년을 기점으로 최근 3~4년 사이에 전 세계적으로 유사 이래 가장 많은 10여개 이상의 저궤도 SAR 위성들을 발사하므로서 비로소 "저궤도 위성 SAR 전성시대"로 진입하게 되었다. 우리나라에서도 최근 다목적 실용위성 5호에 SAR를 탑재하는 최초의 영상 레이다 위성을 2011년 중반에 궤도에 집입시키기 위하여 현재 발사를 준비하고 있다. 본 논문에서는 2011년 9월 26~30일 한국에서 처음으로 개최되는 국제영상 레이다 학술대회(Asia-Pacific Conference on Synthetic Aperture Rader: APSAR 2011)에 즈음하여 위성 SAR 개발 동향을 중심으로 SAR 기술 특정과 활용 기술 및 최근 기술 발전 동향을 소개한다.

A Study on Variable Conductance Radiator using Liquid Metal for Highly Efficient Satellite Thermal Control (인공위성의 고효율 열제어 구현을 위한 액체금속형 가변 전도율 방열판에 관한 연구)

  • Park, Gwi-Jung;Go, Ji-Seong;Oh, Hyun-Ung
    • Journal of Aerospace System Engineering
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    • v.13 no.2
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    • pp.66-72
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    • 2019
  • The observation satellites which uses high heat-dissipating equipment such as synthetic aperture radar (SAR) satellites require a radiator to transmit heat from the equipment into outer space. However, during cold conditions it requires a heater to maintain the temperature of equipment within the allowable minimum limit when it is not in operation. In this study, we proposed a variable conductivity radiator that changes its thermal conductivity value through movement of the liquid metal between two reservoirs based on the temperature condition. This reduces the power consumption of the heater by limiting heat transfer path to the radiator in cold condition, while effectively transferring heat to the radiator during hot condition. The feasibility of the proposed radiator was validated through comparison of the thermal control performance with the conventional fixed conductivity radiator via a thermal analysis.

Classification of Fused SAR/EO Images Using Transformation of Fusion Classification Class Label

  • Ye, Chul-Soo
    • Korean Journal of Remote Sensing
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    • v.28 no.6
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    • pp.671-682
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    • 2012
  • Strong backscattering features from high-resolution Synthetic Aperture Rader (SAR) image provide useful information to analyze earth surface characteristics such as man-made objects in urban areas. The SAR image has, however, some limitations on description of detail information in urban areas compared to optical images. In this paper, we propose a new classification method using a fused SAR and Electro-Optical (EO) image, which provides more informative classification result than that of a single-sensor SAR image classification. The experimental results showed that the proposed method achieved successful results in combination of the SAR image classification and EO image characteristics.

Manufacture and Qualification of Composite Main Reflector of High Stable Deployable Antenna for Satellite (위성용 전개형 고안정 반사판 안테나 주반사판 제작 및 검증)

  • Dong-Geon Kim;Hyun-Guk Kim;Dong-Yeon Kim;Kyung-Rae Koo;Ji-min An;O-young Choi
    • Composites Research
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    • v.37 no.3
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    • pp.219-225
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    • 2024
  • It is essential to develop a light-weight, high-performance structure for the deployable reflector antenna, which is the payload of a reconnaissance satellite, considering launch and orbital operation performance. Among them, the composite main reflector is a key component that constitutes a deployable reflector antenna. In particular, the development of a high-performance main reflector is required to acquire high-quality satellite images after agile attitude control maneuvers during satellite missions. To develop main reflector, the initial design of the main reflector was confirmed considering the structural performance according to the laminate stacking design and material properties of the composite main reflector that constitutes the deployable reflector antenna. Based on the initial design, four types of composite main reflectors were manufactured with the variable for manufacturing process. As variables for manufacturing process, the curing process of the composite structure, the application of adhesive film between the carbon fiber composite sheet and the honeycomb core, and the venting path inside the sandwich composite were selected. After manufacture main reflector, weight measurement, non-destructive testing(NDT), surface error measurement, and modal test were performed on the four types of main reflectors produced. By selecting a manufacturing process that does not apply adhesive film and includes venting path, for a composite main reflector with light weight and structural performance, we developed and verified a main reflector that can be applied to the SAR(Synthetic Aperture Rader) satellite.