• The Bulletin of The Korean Astronomical Society
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• v.37 no.2
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• pp.133.1-133.1
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• 2012

전자파설계는 위성의 전력시스템, 통신시스템 뿐만 아니라 구조체 등 위성시스템 전반에 걸쳐서 종합적으로 고려가 되어야 하며, 이를 위해서는 개발 초기단계에서부터 시스템 설계에 반영되어야 한다. 위성시스템의 상세 설계가 끝난 후에는 시스템에 구현된 전자파 설계의 적합성을 검증하여야 하며 이는 해석 및 시험을 통해 이루어진다. 본 논문에서는 저궤도 중형급 위성이 우주환경에서 전자파적합성을 이루기 위한 설계 기법 및 전자파환경에 대한 적합성 검증과정에 대해서 다루고 있다. 저궤도 중형급 위성시스템에 대하여 구조물의 전자기적 특성을 정의하는 것부터 우주환경에서 위성의 RF호환성에 이르기까지 부품단위에서부터 시스템 수준까지의 전자파 설계 기준과 각 단계별로 전자파적합성을 검증하기 위한 방법 및 절차에 대해서 기술한다.

• Proceedings of the Korean Magnestics Society Conference
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• 2017.05a
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• pp.171-172
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• 2017

• Proceedings of the Korean Magnestics Society Conference
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• 2017.05a
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• pp.170-170
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• 2017

• Journal of Satellite, Information and Communications
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• v.9 no.2
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• pp.1-6
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• 2014

The increasing demands and utilization of the multi-purpose satellites have led to diverse research activities with regards to satellite image processing and applications. In this paper, the research activities of satellite images is investigated relevant to domestic agricultural activities in past 5 years and the system characteristics of the related spaceborne payload is analyzed. For this purpose, a broad range of research materials has been collected published in past years and a statistical analysis is performed to classify the use of satellite images. Overall the current work is aimed to carry out a comprehensive analysis on the current status of satellite imaging in agricultural sectors. Furthermore, this paper can be utilized to identify and support the incoming satellite development plan utilizing medium imaging capabilities specially in the field of agricultural uses.

• The Journal of The Korea Institute of Intelligent Transport Systems
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• v.14 no.2
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• pp.24-29
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• 2015

In this paper, a microstrip antenna with isoflux radiation patterns is presented for Low Earth Orbit(LEO) medium-sized satellites. Because of making isoflux patterns, the ground of proposed antenna under the patch was transform into a trapezoid for adjusting fringing field between the patch and ground. Next, the cavity walls were located at end of the ground for reducing back radiation. The proposed antenna was designed to receive S-band uplink(2.025 ~ 2.110 GHz) and the dimensions of the designed antenna with the ground are $160mm{\times}160mm{\times}40mm$ ($1.1{\lambda}{\times}1.1{\lambda}{\times}0.3{\lambda}$, ${\lambda}$ is the free-space wavelength at 2.068 GHz). Measured -10 dB bandwidth was 90 MHz(4.4 %) and it covers the required system bandwidth. Also, measured 3 dB axial ratio was 18 MHz(0.9 %). On the other hand, measured radiation patterns were isoflux patterns and its measured gain was 5.31 dBi at E-plane $46^{\circ}$ in the y-axis pol.

• Journal of Satellite, Information and Communications
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• v.11 no.3
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• pp.104-109
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• 2016

A technology of GEO satellite communications starts from Koreasat program in Korea. Payload equipment of EQM Ku and Ka band transponders had been developed and space-qualified Ka band payload in COMS was successfully launched in June, 2010. For the purpose of military communications, Dehop-Rehop transponder was developed in Koreasat5 as ANASIS system and DAT(Digital Active Transponder) and DCAMP(Digital Channel AMPlifier) transponders are now under development. In this paper, from the study of military satellite communications trend, a direction of military communication satellite is suggested based on the current GEO SATCOM technologies in Korea. Considering the limit of frequency resources, a technology of battlefield adaptive transponder with medium capacity against high moveable jamming tactics would be efficient for the future military SATCOM system. Mid-sized military satellites with frequency hopping and mid-capacity transponders can be a solution of vitalizing the GEO satellite programs.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.44 no.8
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• pp.702-709
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• 2016

By means of the our satellite development for the past 20 years, it ensure us to obtain domestic independent development capabilities. In the case of practical-class Low-Earth Orbit(LEO) remote sensing satellites, we become a world-class developer. Furthermore, we acquire the technology to develop domestic-leading geostationary satellites, depending on the mission. Currently, we proceed with the next-generation mid-size satellite development program featuring standard bus for the expansion of the world market and has embarked on the development of lunar orbiter from this year.

• Aerospace Engineering and Technology
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• v.1 no.1
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• pp.55-64
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• 2002

A conceptual design of propulsion system for a geosynchronous communication satellite with 12 years design life is presented in this paper. Propellant mass budget for the design life is calculated using total velocity increment (ΔV) flowed-down from mission requirement analysis. Sizes of the fuel and oxidizer tank are derived based on the calculated propellant mass budget, and mass of the pressurant as well as the size and pressure of pressurant tank are calculated too. Thruster positioning, number of rocket engines, and position of tank are determined through Trade-Off Study with Structure & Mechanical Subsystem. Propulsion system configuration and its schematics are presented finally.

• Journal of the Korean Association of Geographic Information Studies
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• v.21 no.4
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• pp.218-237
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• 2018

The purpose of this study is to propose a mid - range low - orbit water disaster monitoring satellite development plan to revolutionize water disaster management infrastructure through securing an independent and leading observation infrastructure and to secure safety against disaster prepared for climate change. Water and water disaster satellites should be able to detect changes in the surface of the ground and observe hydrological factors during daytime, nighttime, and bad weather. In addition, independent technology development should be possible. To do this, we selected C-band image radar payload considering domestic technology and water resources management, and suggested detailed development plan. In this way, it is reflected in the national next-generation mid-satellite 2-phase project plan to secure the basis for building a disaster monitoring system related to wide-area water.

• Proceedings of the Korea Water Resources Association Conference
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• 2023.05a
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• pp.3-3
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• 2023

수자원위성은 C-band 영상레이더(synthetic aperture radar, SAR)를 탑재한 중형급의 수자원 관리 및 수재해 감시 전용 위성이다. 수자원위성은 물 환경과 관련된 다양한 분야에 활용되어 고부가가치의 정보를 제공할 것으로 예상되는데, 특히 시계열 레이더 간섭기법(SAR interferometry, InSAR)의 적용을 통해 댐·보와 같은 수자원시설물의 미세변위 탐지 및 안정성 평가에 효과적으로 사용될 것으로 기대된다. 시계열 영상레이더 간섭기법은 고정산란체를 이용하는 Persistent Scatterer InSAR(PSInSAR) 기법과 분산산란체 기반의 Small BAseline Subset(SBAS) InSAR 기법으로 대표된다. 이 연구에서는 수자원위성에 적합한 수리시설물 시계열 변위 모니터링 알고리즘 개발을 목적으로, Sentinel-1 위성의 C-band SAR 기반 시계열 레이더 간섭기법의 적용성을 평가하고 알고리즘 개발에 고려해야 할 사항들을 분석하였다. 2020년 여름 수재해가 발생한 섬진강댐과 담양댐 및 수변부를 테스트 사이트로 선정하고, 2019년부터 2021년까지의 Sentinel-1 시계열 SAR 영상에 PSInSAR와 SBAS InSAR를 적용하여 시계열 변위를 관측하였다. 댐체에서는 PSInSAR가 SBAS InSAR에 비해 신뢰할 수 있는 시계열 변위를 산출하였다. 그러나 시계열 분석 기간이 길어짐에 따라 PSInSAR 시계열 변위의 정밀도가 낮아지는 경향이 관측되었다. 수변부에서 PSInSAR는 변위 정보를 거의 제공하지 못했다. SBAS InSAR는 수변부의 시계열 변위 모니터링에 효과적이었으나, 여름철 장마 등으로 인해 레이더 간섭도의 긴밀도(coherence)가 낮아질 경우 부정확한 변위를 산출하였다. 앞으로 국내의 다양한 수자원시설물을 대상으로 Sentinel-1 위성을 이용한 시계열 변위 모니터링 알고리즘의 적용성 평가 연구가 진행될 예정이며, 연구 결과를 수자원위성의 관측 특성에 적합한 변위 탐지 알고리즘의 개발에 활용하고자 한다.