• The Science & Technology
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• v.28 no.1 s.308
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• pp.35-38
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• 1995

• Journal of Space Technology and Applications
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• v.1 no.1
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• pp.49-63
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• 2021

The exploration of the solar system is carried out through various payloads, and accordingly, many research results are emerging. We tried to apply deep-learning as a method of studying the bodies of solar system. Unlike Earth observation satellite data, the data of solar system differ greatly from celestial bodies to probes and to payloads of each probe. Therefore, it may be difficult to apply it to various data with the deep-learning model, but we expect that it will be able to reduce human errors or compensate for missing parts. We have implemented a model that detects craters on the lunar surface. A model was created using the Lunar Reconnaissance Orbiter Camera (LROC) image and the provided shapefile as input values, and applied to the lunar surface image. Although the result was not satisfactory, it will be applied to the image of the permanently shadow regions of the Moon, which is finally acquired by ShadowCam through image pre-processing and model modification. In addition, by attempting to apply it to Ceres and Mercury, which have similar the lunar surface, it is intended to suggest that deep-learning is another method for the study of the solar system.

• Geophysics and Geophysical Exploration
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• v.11 no.3
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• pp.230-241
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• 2008

Characteristics of transfer responses for arrays like triangle, hexagon and semicircle were investigated. To characterize the site near Izmit city with ambient noise measurement, dispersion curves of surface waves were derived with using array technique like F-K, High resolution F-K, MSPAC and H/V ratio was calculated. Also, MASW was surveyed to get the high frequency part of dispersion curves. The transition from fundamental mode to first high mode of surface waves for dispersion curve was observed. Dispersion curve of fundamental mode of ambient noise and first higher mode of MASW was used in inversion to get S-wave velocity structure of subsurface. None-unique problem of results of surface wave inversion was solved with comparison of result of refraction tomography performed with first arrivals of MASW data.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.44 no.8
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• pp.741-757
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• 2016

Over 60 years has passed since mankinds started space exploration beyond the Earth with lunar explorer Luna 1 launched by Soviet Union. Unprecedently remarkable outcomes have been obtained by sending unmanned spacecrafts to most planets in the solar system and having the lander landed on the approaching comet toward the Earth even though any evidence of life presence has not been discovered yet. Only moon is an natural object beyond the earth on which human beings landed. Many countries are planning to send humans to the moon or mars to build colonies and to survive with substantiality. Korean lunar exploration program has officially started as of 2016 after its plan including lunar exploration has been specified in the series of National Space Promotion Plan since Korea initiated space development in early 1990s. In this paper, the plan for Korean space exploration is summarized with reviewing overseas space exploration program status and trends.

• Journal of the Korean earth science society
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• v.25 no.4
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• pp.270-276
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• 2004

Multi-channel Analysis of Surface Waves (MASW) and Seismic Cone Penetration Test (SCPT) have been recently developed to obtain S-wave velocity profiles which were conventionally investigated by a down-hole seismic survey. For unconsolidated sedimentary sites, we studied these three methods, and compared the results with a drilling log. All the methods showed that the changes in the S-wave velocities were consistent with the changes in the sedimentary facies. In addition, the SCPT was most sensitive to changes in sedimentary facies among the three profiles. The results of the SCPT showed that there exists a low velocity zone, which is mainly composed of clayey sand, at the depth of 8${\sim}$12m in the sediments.

• Korean Journal of Remote Sensing
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• v.16 no.1
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• pp.65-72
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• 2000

Scattering coefficients of randomly rough lossy dielectric surfaces were computed by using the FDTD(Finite-Difference Time-Domain) method and the Monte Carlo method in this paper. The FDTD method was applied to compute electromagnetic wave scattering characteristics at any incident angles, any linear polarizations by dividing the computation region into the total-field region and the scattered-field region. The radar cross sections(RCS) of conducting cylinders have been computed and compared with theoretical results, measurement data and the results from the method of moment(MoM) to verify the FDTD algorithm. Then, to apply the algorithm to compute scattering coefficients of distributed targets, a two-dimensionally rough surface was generated numerically for given roughness characteristics. The far-zone scattered fields of 50 statistically independent dielectric rough surfaces were computed and the scattering coefficient of the surface was calculated from the scattered fields by using the Monte Carlo method. It was found that these scattering coefficients agree well with the SPM(Small Pertubation Method) model in its validity region.

• Korean Journal of Remote Sensing
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• v.26 no.1
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• pp.21-27
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• 2010

This paper presents a numerical simulation of the radar backscattering from oil spills on ocean surface. At first, a one-dimensionally rough sea surface is numerically generated for a given wind speed at HEBEI SPIRIT accident. Then, an oil-spilled sea surface is represented with a two-layered medium, which is generated by adding a thin low-dielectric oil layer on the randomly-rough highdielectric sea surface. The backscattering coefficients of various oil-spilled sea surfaces are obtained using the Method of Moments and Monte Carlo technique for various surface roughness, oil-layer thicknesses, frequencies, polarizations and incidence angles. The numerical method is verified with theoretical models for simple structures. The reduction of the backscattering coefficients due to the lowdielectric oil-layers on sea surfaces has been analyzed. These numerical results will help to detect any oil spills on sea surfaces, and consequently, to classify SAR images.

• The Bulletin of The Korean Astronomical Society
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• v.43 no.1
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• pp.48.4-48.4
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• 2018

대한민국 달탐사 시험용 궤도선은 2020년 말에 발사를 예정으로 위성개발이 진행되고 있다. KPLO(Korea Pathfinder Lunar Orbiter) 라고 명명된 달 궤도선에는 6개의 탑재체가 있으며, 경희대학교 우주탐사학과에서는 달 주위 공간 및 달 표면의 이상 자기장 영역을 관측하는 탑재체 (KMAG: Kplo MAGnetometer)를 개발하고 있다. 자기장센서는 3축 플럭스게이트 센서를 사용하며 약 0.2nT 이하의 분해능을 가지고 있다. 측정주기는 10Hz이며 총 무게는 3.5kg 이다. 1.2m 길이의 붐(Boom) 구조물 내부에 3개의 자기장 센서들을 설치하였으며 가능한 위성체로부터 거리를 두고 자기장을 측정하는 구조로 구성하였다. 시험모델 개발을 완료하고, 개발된 탑제체의 환경시험결과와 성능시험결과 요구조건에 부합되는 결과를 얻었다. KAMG는 국내최초의 심우주 탐사용 자기장 측정기로서 향 후, 행성 및 소행성 탐사 등에 활용하기 위한 기반 기술로 활용할 수 있을 것으로 기대한다.

• The Bulletin of The Korean Astronomical Society
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• v.37 no.2
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• pp.225.2-225.2
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• 2012

저궤도 관측용 다중 카메라를 통해 고해상도 위성을 제공할 수 있으며, 지도 제작이나 환경, 농업, 해양 지역 모니터링 등의 목적으로 사용될 수 있다. 특히 항공촬영 및 지구 관측을 통해 수치표고모델(DEM) 추출을 함으로써 촬영지역의 고도정보를 포함하는 입체영상을 얻는데 유용하다. 또한, 달 관측을 위한 관측위성에 장착할 경우 달 표면의 지형을 정밀하게 얻어내어 달표면 고도 지형 지도제작 및 향후 달 탐사선을 통한 달 탐사 시 탐사지역 선정에 필요한 정보를 제공할 수 있다. 다중 카메라를 포함한 탑재체 시스템은 크게 광학부와 카메라 전자부로 구성된다. 광학부에서는 입체촬영 및 줌인이 가능한 광학계를 제공하며, 카메라 전자부에서는 광학계를 통해 검출기로 입사되는 빛에너지를 전자신호로 변환하고, 이를 카메라 전자부 영상출력 형식으로 변환하게 된다. 특히, 다중카메라를 각각 제어하기 위한 정밀제어로직, 다양한 촬영 지원 모드, 다중카메라 영상자료 및 영상처리를 위한 추가적인 영상정보를 제공한다. 본 논문에서는 저궤도 관측용 다중 카메라를 이용한 다양한 활용에 따른 각 모드별 성능분석방법을 제안한다. 이를 위해 각 촬영조건에 따라 필요한 파라미터를 분석하고 실제 활용시 예상되는 성능을 분석해 본다. 또한 다중카메라를 통해 얻어진 영상을 처리하는데 필요한 처리 과정 및 처리된 영상을 활용하는 방법을 제시한다. 특히 다중 카메라 촬영을 통해 얻어진 영상데이터의 특성을 알아보고, 이를 보정 및 처리하기 위해 필요한 추가 적인 정보, 영상파라미터, 처리 단계 및 최종결과물을 검증하는 방법을 제시한다.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.19 no.7
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• pp.144-152
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• 2018

Lunar exploration, which was led by the United States and the former Soviet Union, ceased in the 1970s. On the other hand, since massive lunar ice deposits and rare resources were found in 1990s, European Union, China, Japan, and India began to participate in lunar exploration to secure future lunar resource as well as to construct a lunar base. In the near future, it is expected that national space agencies and private industries will participate in the lunar exploration together. Their missions will include the exploration and sample return of lunar resources. Lunar resources have a close relationship with the lunar in-situ resource utilization (ISRU). To construct a lunar base, it is inevitable to bring huge amounts of resources from Earth. Water and oxygen, however, will need to be produced from local lunar resources and lunar terrain feature will need to be used to construct the lunar base. Therefore, in this paper, the global trends on lunar exploration and lunar construction technology are investigated and compared along with the ISRU technology to support human exploration and construct a lunar base on the Moon's surface.