• 한국위성정보통신학회논문지
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• 제11권3호
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• pp.12-17
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• 2016

정지궤도 위성들을 이용하여 사용자들에게 GNSS (Global Navigation Satellite System) 정정 데이터 및 레인징 신호를 제공하는 SBAS (Satellite Based Augmentation System)는 국제민간항공기구에 의해 2025년까지 도입되도록 권고되고 있다. 본 논문에서는 현재 개발/구축 사업으로 진행중인 한국형 SBAS 시스템인 KASS (Korea Augmentation Satellite System)의 위성통신시스템 RF 링크를 기본 설계하여 그 결과를 제시한다. C 대역 상향링크와 Ku 대역 상향링크를 모두 고려하여 SBAS 시스템에 대한 국제 표준 요구사항을 만족하도록 RF 링크를 설계하였고, 각 주파수 대역에 따른 요구되는 위성통신국의 최소 EIRP 및 G/T 성능 규모를 파악하였다. 이러한 RF 링크 설계 분석 결과를 이용하여 KASS 위성통신시스템의 하위 시스템 규격 선정시 효과적인 설계가 될 수 있도록 활용할 예정이다.

• 한국지리정보학회지
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• 제23권3호
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• pp.252-262
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• 2020

원격탐사 분야에서 토지피복분류에는 머신러닝 기반의 SVM 모델이 대표적으로 활용되고 있는 한편, 신경망 모델을 이용한 연구도 지속적으로 수행되고 있다. 다목적실용위성의 고해상도 영상을 이용한 연구는 미흡한 실정이며, 따라서 본 연구에서는 고해상도 KOMPSAT-3 위성영상을 이용하여 신경망 모델의 토지피복분류 정확도를 평가하고자 하였다. 경주시 인근 해안지역의 위성영상을 취득하여 훈련자료를 제작하고, 물과 식생 및 육지의 세 항목에 대해 SVM, ANN 및 DNN 모델로 토지피복을 분류하였다. 분류 결과의 정확도를 오차 행렬을 통해 정량적으로 평가한 결과 DNN 모델을 활용한 토지피복분류가 92.0%의 정확도로 가장 우수한 결과를 나타냈다. 향후 다중 시기의 위성영상을 통해 훈련자료를 보완하고, 다양한 항목에 대한 분류를 수행 및 검증한다면 연구의 신뢰성을 높일 수 있을 것으로 판단된다.

• 전기학회논문지
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• 제57권3호
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• pp.439-445
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• 2008

In this paper, the preliminary EMC analysis process between the Communication, Ocean and Meteorological Satellite (COMS) and Geostationary Earth Orbit (GEO) launch vehicles in the frequency range [1MHz-47MHz] is described. The considered launch vehicles are arian V, sea Launch, land Launch, atlas III&V, delta IV, proton M/breeze M, soyuz, HII-A and Angara. The launch vehicle Radiated Emission (RE) specifications have been compared to COMS satellite Radiated Susceptibility (RS) limits. The COMS RS limits are the RS qualification levels of COMS units during launch. As a result, The radiated emission levels of arian V, sea launch, atlas III&V, delta IV, proton M/breeze M, HII-A and angara are compliant with COMS RS limits. The negative margins appear between land launch or soyuz launch vehicle RE and COMS RS. Then, if the land launch or soyuz is chosen by the customer, The tests should be performed at satellite level in order to demonstrate the compatibility with respect to launch vehicles specifications.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2003년도 Proceedings of ACRS 2003 ISRS
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• pp.476-478
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• 2003

Capability of material fixation in forest was noticed since COP3, but now it was difficult to understand material fixation in wide area. In this study, we attempted to estimate and test the amount of carbon, nitrogen, and phosphorus fixed by forest from satellite images. First, we classified into tree species and estimated the number of trees in the forest by species, area, and digital numbers. We inspected to apply it in wide area. Next, we compared the amount of carbon, nitrogen, and phosphorus with NDVI and each band of satellite images.

• 대한원격탐사학회지
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• 제22권5호
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• pp.351-356
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• 2006

Based on current practical needs for geo-spatial information on mobile platform, the main theme of this study is a design and implementation of dynamic 3D terrain rendering system using spaceborne imagery, as a kind of texture image for photo-realistic 3D scene generation on mobile environment. Image processing and 3D graphic techniques and algorithms, such as TIN-based vertex generation with regular spacing elevation data for generating 3D terrain surface, image tiling and image-vertex texturing in order to resolve limited resource of mobile devices, were applied and implemented by using graphic pipeline of OpenGL|ES (Embedded System) API. Through this implementation and its tested results with actual data sets of DEM and satellite imagery, we demonstrated the realizable possibility and adaptation of complex typed and large sized 3D geo-spatial information in mobile devices. This prototype system can be used to mobile 3D applications with DEM and satellite imagery in near future.

• Journal of Astronomy and Space Sciences
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• 제30권3호
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• pp.179-185
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• 2013

Photometric observation is one of the most effective techniques for determining the physical characteristics of unknown space objects and space debris. In this research, we examine the change in brightness of the Communication, Ocean, Meteorological Satellite-1 (COMS-1) Geostationary Orbit Satellite (GEO), and compare it to our estimate model. First, we calculate the maximum brightness time using our calculation method and then derive the light curve shape using our rendering model. The maximum brightness is then calculated using the induced equation from Pogson's formula. For a comparison with our estimation, we carried out photometric observation using an optical telescope. The variation in brightness and the shape of the light curve are similar to the calculations achieved using our model, but the maximum brightness shows a slightly different value from our calculation result depending on the input parameters. This paper examines the photometric phenomenon of the variation in brightness of a GEO satellite, and the implementation of our approach to understanding the characteristics of space objects.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2005년도 Proceedings of ISRS 2005
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• pp.645-648
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• 2005

The COMS(Communication, Ocean and Meteorological Satellite), a multi-mission geo-stationary satellite, is being developed by KARl. The first mission of the COMS is the meteorological image and data gathering for weather forecast by using a five channel meteorological imager. The second mission is the oceanographic image and data gathering for marine environment monitoring around Korean Peninsula by using an eight channel Geostationary Ocean Color Imager(GOCI). The third mission is newly developed Ka-Band communication payload certification test in space by providing communication service in Korean Peninsula and Manjurian area. There were many low Earth orbit satellites for ocean monitoring. However, there has never been any geostationary satellite for ocean monitoring. The COMS is going to be the first satellite for ocean monitoring mission on the geo-stationary orbit. The meteorological image and data obtained by the COMS will be distributed to end users in Asia-Pacific area and it will contribute to the improved weather forecast.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2007년도 Proceedings of ISRS 2007
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• pp.207-210
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• 2007

A part of the big differences between LEO(Low Earth Orbit) and GEO(Geostationary Earth Orbit) satellite is that transfer orbit is used or not or what tolerance of the position on the mission orbit is permitted. That is to say, the transfer orbit is not used and the constraint of orbit position is not adapted on LEO satellite. Whereas for GEO satellite case, the transfer orbit shall be used due to the very high altitude and the satellite shall be stayed in the station keeping box which is permitted on the mission orbit. These phases are functions for AOCS mission. The aim of this paper is to introduce the AOCS hardware configuration for COMS (Communication, Ocean and Meteorological Satellite). The AOCS hardware of COMS consist of 3 Linear Analogue Sun Sensors (LIASS), 3 Bi-Axis Sun Sensors (BASS), 2 Infra-Red Earth Sensors (IRES), 3 Fiber Optical Gyroscopes (FOG), 5 momentum wheels and 14 thrusters. In this paper, each component is explained how to be used, how to locate and what relation between the AOCS algorithm and these components.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2008년 영문 학술대회
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• pp.307-310
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• 2008

In the framework of COMS(Communication, Ocean and Meteorological Satellite) programme, the first bipropellant propulsion system for GEO satellite has been developed successfully. So far Korea has its own experience of development of a monopropellant propulsion system for LEO satellites, i.e., KOMPSAT's. Other types of propulsion systems for a satellite, such as cold gas and electric propulsion etc., are being developed somewhere in Korea, however they are not commercialised yet, apart from those two systems aforementioned. This paper mainly focused on the design of the Chemical Propulsion System(CPS) for the COMS, joint scientific and communications satellite. It includes descriptions of the general system design and a summary of the supporting analysis performed to verify suitability for space flight. Essentially it provides an overview and guide to the various engineering rationale generated in support of the COMS CPS design activities. The manufacture and subsequent testing of COMS CPS are briefly discussed. Feasibility of COMS CPS to an interplanetary mission is proposed as well.

• 항공우주시스템공학회지
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• 제10권4호
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• pp.90-97
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• 2016

항공우주연구원은 천리안위성의 임무를 승계하기 위해 2018년과 2019년 발사를 목표로 정지궤도복합위성 2A와 2B를 개발하고 있다. 정지궤도복합위성은 아리안 V 발사체에 의하여 발사되어 전이궤도(Transfer Orbit)에 전입한 후 여러 번의 액체원지점엔진분사를 통하여 표류궤도에 진입한다. 액체원지점엔진의 분사시기, 분사시간, 각 분사간의 간격 등은 위성이 목표하는 표류궤도에 진입할 수 있도록 선정되고 적용된다. 정지궤도복합위성의 경우 표류궤도 진입을 위하여 4회의 액체원지점엔진 분사를 수행할 계획이다. 본 논문에서는 미리 정의된 제한조건을 고려하고 외부 교란력을 고려하여 정지궤도복합위성의 액체원지점엔진 분사계획을 수립하였다. 여기서는 단일계산(Single Shot) 방식과 반복계산에 의한 최적화 기법, 두 가지 접근을 고려하였다. 최적의 해를 얻기 위해 Focusleop이라고 하는 발사초기임무해석 도구를 적용하였다.