• Title/Summary/Keyword: 위성레이더

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Evaluation of 3D-Positioning Method Using X-band SAR Satellite Images - Focused on InSAR, Radargrammetry and RPC (X-band SAR 위성영상의 3차원 위치결정 기법 평가 - 레이더 간섭기법, Radargrammetry, RPC를 중심으로)

  • Song, Yeong Sun;Lee, Jung Han;Jang, In Tae
    • Journal of Korean Society for Geospatial Information Science
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    • v.22 no.4
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    • pp.117-125
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    • 2014
  • Korea's first X-band SAR satellite KOMPSAT-5 has been launched in 2013, so the research related to the X-band SAR satellite image is required to increase the utilization of KOMPSAT-5. In this study, we generated a DEM(Digital Elevation Model) using X-band SAR satellite images based on three methods which are InSAR, radargrammetry and RPC(Rational Polynomial Coefficients), and evaluated the performance of each methods. The four stripmap mode TerraSAR-X images taken in Daejeon were used to generate DEM, and accuracy was evaluated using DEM by IKONOS RPC. As results, DEM produced by the InSAR showed the highest accuracy. Also, we knew that RPC could be effective method if you want to create a large area DEM which contains the various elevation.

Analysis of Flood Inundated Area Using Multitemporal Satellite Synthetic Aperture Radar (SAR) Imagery (시계열 위성레이더 영상을 이용한 침수지 조사)

  • Lee, Gyu-Seong;Kim, Yang-Su;Lee, Seon-Il
    • Journal of Korea Water Resources Association
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    • v.33 no.4
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    • pp.427-435
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    • 2000
  • It is often crucial to obtain a map of flood inundated area with more accurate and rapid manner. This study attempts to evaluate the potential of satellite synthetic aperture radar (SAR) data for mapping of flood inundated area in Imjin river basin. Multitemporal RADARSAT SAR data of three different dates were obtained at the time of flooding on August 4 and before and after the flooding. Once the data sets were geometrically corrected and preprocessed, the temporal characteristics of relative radar backscattering were analyzed. By comparing the radar backscattering of several surface features, it was clear that the flooded rice paddy showed the distinctive temporal pattern of radar response. Flooded rice paddy showed significantly lower radar signal while the normally growing rice paddy show high radar returns, which also could be easily interpreted from the color composite imagery. In addition to delineating the flooded rice fields, the multitemporal radar imagery also allow us to distinguish the afterward condition of once-flooded rice field.

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Development of Hydrometeorological Information and Application Technology for Monitoring Water Resources in North Korea (북한지역 수자원 감시예측을 위한 수문기상정보 활용기술개발)

  • Kim, Ji-in;Lee, Sungjin;Kang, Jaewon;Kim, Gyumum;Suh, Ae-sook
    • Proceedings of the Korea Water Resources Association Conference
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    • 2015.05a
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    • pp.531-535
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    • 2015
  • 본 연구에서는 한반도 관측 공백지역인 북한지역에 대하여 레이더와 위성 원격탐사자료를 활용하여 강수량과 토양수분 등 수문기상정보를 생산 및 검증하고 효율적인 수문 모니터링 및 수문 기상 재해 감시와 평가 방안을 수립하고자 한다. 또한, 북한지역의 수문 기상 정보 수집 및 통합 DB를 마련하고 북한 수문기상 포털시스템을 구축함으로써 부처 간 자료를 공유할 수 있는 매개체를 마련하여 일관된 정책 수립과 효율적인 물관리를 도모하고자 한다. WPMM(Window Probability Matching Method)방법을 기반으로 구성된 RAD-RAR(Rain rate system) 산정 알고리즘(Rosenfeld et al., 1993)을 활용하여 산출된 합성 강우장 데이터의 정확성을 비교 분석하기 위해 접경지역 AWS 강수량과 세계기상통신망(GTS)기반 강수량을 산출하여 각각 레이더 강수량과 검증분석을 실시하였다. 연구기간은 2012년과 2013년 여름철 기간 중 5개의 기간을 선별하였다. 연구 기간 동안의 RAR 합성 강우장 데이터를 이용하여, 기간 중 1시간 동안 누적된 강수량을 산출하고 접경지역 AWS 강수량과 비교하였고 12시간 누적 강수량을 산출하여 GTS 강수량과 비교 분석을 실시하였다. 전반적으로 레이더 강수량에 비해 AWS 강수량이 더 높게 나타났으며 마찬가지로 레이더 강수량과 GTS 강수량의 비를 통해 레이더 자료가 상대적으로 과소추정되고 있음을 확인 할 수 있었다. 미항공우주국(NASA)과 일본항공우주국(JAXA)을 중심으로 진행된 GPM(Global Precipitation Measurement)미션은 한 개의 핵심위성과 마이크로파 복사계를 탑재한 10여개의 보조위성으로 구성되어 있으며, 매 3시간 간격의 전구 강수량 자료 생산에 목적이 있다. 이는 홈페이지를 통해 Level 1, 2, 3의 GPM 데이터를 배포하고 있다. 특히 Level 2 데이터는 언급된 3시간 간격의 전구 강수량 데이터를 제공한다. 이 경우 복사량을 강수량으로 변환하는 번거로움을 덜 수 있으며 NASA가 제공하는 Panoply라는 프로그램을 이용하여 한반도 강수 자료 가시화가 가능하다.

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A Study on Active SAR Satellite Maneuver Time Reduction through Sequential Rotation (연속회전을 통한 능동 합성개구레이더위성 기동시간 단축 연구)

  • Son, Jun-Won;Park, Young-Woong
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.43 no.7
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    • pp.648-656
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    • 2015
  • Active SAR satellite's main maneuver is roll axis maneuver to change SAR antenna direction. In addition, yaw steering is required to minimize the doppler centroid variation. Thus, it is resonable to assign the torque/momentum capacity mostly to roll axis and then yaw axis. In this case, the pitch axis shows low agility performance. However, due to orbit maintenance, large angle maneuver about pitch axis is sometimes required. In this paper, we study the pitch axis maneuver time reduction through sequential rotation about roll and yaw axis. Since these two axes have high agility performance than pitch axis, maneuver time reduction is possible when large angle rotation about pitch axis is required.

Current Status and Future Prospects of Satellite Payloads Technology (인공위성 탑재체 기술 현황 및 전망)

  • Yong, Sang-Soon;Kang, Gm-Sil;Heo, Haeng-Pal
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.44 no.8
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    • pp.710-717
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    • 2016
  • Satellite payload can be classified as electro-optical payload, SAR, microwave radiometer, communication payload, navigation payload and so on in accordance with the mission objective. The technology of satellite payload was tried to be obtained through development of KOMPSAT series, COMS and STSAT in Korea. In this paper, the required technology for the development and world market trend of satellite payload were studied and described. Since KOMPSAT program has been started in 1994, technology status and future prospects of satellite payload in Korea are studied and analyzed.

A Study on Automatic Correction Method of Electronic Compass Deviation Using the Geostationary Satellite Azimuth Information (정지위성 방위각 정보를 활용한 전자 컴퍼스 편차 자동보정기법 연구)

  • Lee, Jae-Won;Lee, Geon-Ho
    • Journal of Navigation and Port Research
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    • v.41 no.4
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    • pp.189-194
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    • 2017
  • The Moving Search Radar System (MSRS) monitors sea areas by moving along the coast. Since the radar is initially aligned to the front of the vehicle, it is important to know the changes in the heading azimuth of the vehicle to quickly acquire the target azimuth from the radar after the MSRS has moved. The heading azimuth can be obtained using the gyro compass, the GPS compass or the electronic compass. The electronic compass is suitable for MSRS requiring fast maneuverability due to its small volume, short stabilization time and low price. However, using a geomagnetic sensor may result in an error due to the surrounding magnetic field. Errors can make early automatic tracking of the satellites difficult and can reduce the radar detection accuracy. Therefore, this paper proposes a method to automatically compensate for the error reflecting the correction value on the radar obtained by comparing the reference azimuth calculated by solving the geodesic inverse problem using two coordinates between the radar and the geostationary satellite with the actually-directed azimuth angle of the satellite antenna. The feasibility and convenience of the proposed method were verified by applying it to the MSRS in the field.

The Interference Impact between Automotive Radar and Radio Astronomy Service (차량용 레이더와 전파 천문 업무 사이의 간섭영향 연구)

  • Yun, Hyeju;Lee, Ilkyoo;Chung, Yongjun
    • Journal of Satellite, Information and Communications
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    • v.9 no.3
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    • pp.53-58
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    • 2014
  • The global automotive radar is regulated to use the 22GHz~26GHz band. However, it plans to move to the 77~81GHz band of a broadband radar in the millimeter wave for the high resolution of pedestrian sensing and blind spot. On the other hand, the 71~275GHz band is regulated to use a radio astronomy service. The interference is predicted between an automotive radar and a radio astronomy service. Therefore, this paper analyzed the interference impact of the automotive radar on the radio astronomy service and then obtained separation distance for the protection of the radio astronomy service.

Analysis of the KARISMA Orbit Determination Performance for the Radar Tracking Data (우주파편 충돌위험 종합관리 시스템의 레이더 관측 데이터 처리 결과 비교 분석)

  • Cho, Dong-Hyun;Kim, Hae-Dong;Lee, Sang-Cherl
    • Aerospace Engineering and Technology
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    • v.12 no.2
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    • pp.123-130
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    • 2013
  • Many countries tried to design the collision risk management system to protect their own satellites from collision probability due to the space debris. In this situation, KARI(Korea Aerospace Research Institute) is developing the KARISMA(KARI Conjunction Risk Management System) to protect our operating satellites from these space debris. The quality of this system is depending on the accuracy of orbit determination for the space debris which has collision risk. Therefore, this system must treat many kinds of measurement data types to estimate the orbit of space debris. In this paper, to handle the radar observation data widely used for these space debris, the orbit determination system was applied with simulated radar tracking data for the KOMSAT-2 which has precise orbit determination data.

Ship Detection by Satellite Data: Radiometric and Geometric Calibrations of RADARS AT Data (위성 데이터에 의한 선박 탐지: RADARSAT의 대기보정과 기하보정)

  • Yang, Chan-Su
    • Journal of the Korean Society of Marine Environment & Safety
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    • v.10 no.1 s.20
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    • pp.1-7
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    • 2004
  • RADARSAT is one of many possible data sources that can play an important role in marine surveillance including ship detection because radar sensors have the two primary advantages: all-weather and day or night imaging. However, atmospheric effects on SAR imaging can not be bypassed and any remote sensing image has various geometric distortions, In this study, radiometric and geometric calibrations for RADARSAT/SAT data are tried using SGX products georeferenced as level 1. Even comparison of the near vs. far range sections of the same images requires such calibration Radiometric calibration is performed by compensating for effects of local illuminated area and incidence angle on the local backscatter, Conversion method of the pixel DNs to beta nought and sigma nought is also investigated. Finally, automatic geometric calibration based on the 4 pixels from the header file is compared to a marine chart. The errors for latitude and longitude directions are 300m and 260m, respectively. It can be concluded that the error extent is acceptable for an application to open sea and can be calibrated using a ground control point.

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