• 대한원격탐사학회지
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• 제15권4호
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• pp.349-356
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• 1999

Korea Multi-Purpose Satellite-l (KOMPSAT-l) has been developed by the Korea Aerospace Research Institute (KARI) with the aid of TRW and will be launched on the December 21, 1999 at the Vandenberg Air Base in CA, U.S. Now, the satellite application group in KARI is preparing for the service with the KOMPSAT-l satellite data. For the purpose of supplying good service to the users, data application planning has to be established before launching satellite. To use satellite data effectively, KARI makes a plan for data policy, data price, mission planning, and commercializing strategy. This study was carried out with the purpose of effective use of satellite data. For this purpose, KARI, first, made 60 user groups to use KOMPSAT-l data for public welfare and research sectors. These user groups include government, public corporations, institutes, and universities. KARI will offer the service to users through online using Internet. Secondly, KARI made a policy for the priority of KOMPSAT-l missions. These are classified by the mission priority, payloads, and operational states etc. Thirdly, KARI will make data policy and data price of KOMPSAT-l based on the basic master plan. Especially, data price will be determined at the KOMPSAT-l committee including Ministry of Science and Technology (MOST). KARI is also trying to commercialize the data with the domestic and foreign companies to expand the use of KOMPSAT-l data in the industries sector. Afterward in this study, KARI will continue the improvement for the effective distribution of KOMPSAT-l data for all users.

• International Journal of Aeronautical and Space Sciences
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• 제6권1호
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• pp.77-88
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• 2005

KOMPSAT-2 is the second Korean earth observation satellite after KOMPSAT-l: the 1 meter GSD cartographic capability and planning to launch at the end of 2005 by ROKOT launch vehicle. The dedicated AOCS operational modes are designed for KOMPSAT-2 based on KOMPSAT-l experience All of AOCS operational modes requires gyro information. To compensate this drawback, Power Safe Mode is designed and implemented. Successfully AOCS on-board software is developed and extensively verified through a nonlinear simulation process. The simulation results of Power Safe Mode and Science Fine Submode are provided to demonstrate its functionality as well as its performance.

• 대한원격탐사학회지
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• 제39권6_1호
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• pp.1185-1193
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• 2023

위성 영상을 활용하여 정확한 토양 수분도를 산정하는 연구는 원격탐사 응용 분야에 포함되는 중요한 기본 연구 주제 중 하나이다. 이 연구의 목적은 KOMPSAT-3/3A 영상과 KOMPSAT-5 SAR 영상을 적용하여 시험 지역에 대하여 토양수분도를 제작하고 산정된 결과를 정확도 검증 차원에서 미국 NASA에서 제공하는 Soil Moisture Active Passive (SMAP)의 토양수분 자료와 정량 비교하는 것이다. 한편 농림 식생 지대를 중심으로 토양수분도를 산정하기 위하여 환경공간정보서비스에서 제공하는 토지피복지도를 연구에 적용하였다. 시험 연구 지역은 이 연구에 적용한 수분 구름 모델(Water Cloud Model)에 기반한 토양수분 산정 알고리즘 적용에 필요한 입력 자료가 모두 가용한 제주 서부 지역을 선정하였다. 토양수분도 제작에 사용한 Synthetic Aperture Radar (SAR) 영상은 KOMPSAT-5 HV와 Sentinel-1 VV 영상이며, 식생지수는 KOMPSAT-3 영상의 지표반사도를 사용하였다. 이 연구에서 산출한 토양수분도 산정 결과와 SMAP (L-3) 자료를 차분 연산으로 비교하면 차이 값이 평균 4.13±3.60p%의 높은 일치도를 보이는 것으로 나타났고, SMAP (L-4) 자료와의 차분 연산 결과는 평균 14.24±2.10p% 수준의 일치도를 보였다. 이 연구를 통하여 향후 우리나라 위성영상과 공공 제공자료를 이용하여 정확도가 높은 정밀 토양수분도를 제작할 수 있는 가능성을 제시하였다.

• 대한전기학회논문지:시스템및제어부문D
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• 제53권8호
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• pp.571-577
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• 2004

In this paper, we describe the structure, function and the design factor of common module for KOMPSAT-2 OBC, which will be launched in 2005. By analysing OBC's performance, we can know the throughput and how much improve performance than KOMPSAT-l. it is used in the satellite mission design by system engineer. We verify the usefulness of common module for KOMPSAT-2 OBC through environment test.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2004년도 Proceedings of ISRS 2004
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• pp.464-466
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• 2004

Ranging and 2-way Doppler measurements are very essential source for orbit determination in LEOP (Launch and Early Operation). This paper shows ranging system features of 13M TT &C antenna and test results recently acquired with KOMPSAT-l. Ranging and 2-way Doppler measurements were compared with KOMPSAT-I GPS telemetry data. Through comparison, it was found that constant and accurate ranging measurements are available with 13M antenna system. Ranging and Doppler measurement function is expected to be used for KOMPSAT-1 and KOMPSAT-2.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2004년도 Proceedings of ISRS 2004
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• pp.501-504
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• 2004

There is a world-wide trend to implement autonomous TM/TC system in satellite operations. KARI developed CALS(Command AutoLoader System) for KOMPSAT-1 operation automation in 2004. This paper provides system requirement, system design, system test and operational procedure. Through test with simulator and KOMPSAT-1, CALS was verified to meet all functional and operational requirement like scheduling, real-time telemetry check, CRC generation, command grouping. CALS is expected to be used in KOMPSAT-1 normal mission operation in end of 2004

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 2003년도 ICCAS
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• pp.2325-2330
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• 2003

GPS based orbit determination system for the KOMPSAT-2 has been developed. Two types of orbit determination software such as operational orbit determination and precise orbit determination are designed and implemented. GPS navigation solutions from on-board the satellite are used for the operational orbit determination and raw measurements data such as C/A code pseudo-range and L1 carrier phase for the precise orbit determination. Operational concept, architectural design, software implementation, and performance test are described.

• Korean Journal of Geomatics
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• 제3권1호
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• pp.53-57
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• 2003

As the Korea Multi-Purpose Satellite-I (KOMPSAT-1) satellite can roll tilt up to $\pm$45$^{\circ}$, we have analyzed some KOMPSAT-1 EOC images taken at different tilt angles for this study. The required ground coordinates for bundle adjustment and geometric accuracy are obtained from the digital map produced by the National Geography Institution, at a scale of 1:5,000. Followings are the steps taken for the tilting angle of KOMPSAT-1 to be present in the evaluation of geometric accuracy of each different stereo image data: Firstly, as the tilting angle is different in each image, the characteristic of satellite dynamic must be determined by the sensor modeling. Then the best sensor modeling equation should be determined. The result of this research, the difference between the RMSE values of individual stereo images is mainly due to quality of image and ground coordinates instead of tilt angle. The bundle adjustment using three KOMPSAT-1 stereo pairs, first degree of polynomials for modeling the satellite position, were sufficient.

• 천문학논총
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• 제15권spc2호
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• pp.37-44
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• 2000

Two different types of plasma probes have been developed and are currently in operation on board the KOMPSAT-l. One is the cylindrical Langmuir Probe (LP) that measures the electron density and temperature from its current-voltage characteristics in thermal plasmas, and the other is the Electron Temperature Sensor (ETS) which directly gives the information of the ambient electron temperatures. These plasma probes provide the electron properties of the local nighttime ionosphere at the KOMPSAT-l altitudes. In this paper we briefly describe the probes and the initial results obtained from these probes since the beginning of their normal operation in April, 2000.

• 한국측량학회지
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• 제19권4호
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• pp.373-383
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• 2001

본 연구에서는 중해상도 위성영상으로 대표적인 SPOT, 아리랑, IRS-1C위성영상에 대하여 각기 하나의 입체모델을 이용한 지도제작 실험을 수행하였으며, 각각에 대한 위치정확도, 판독 및 묘사가능한 지형지물의 분석, 기존 수치지도와의 비교 등을 통하여, 제작가능한 지도축척의 범위에 대한 기술적인 검토 및 경제성 검토를 하였다. 도화작업에 있어서, SPOT 영상은 수치입체도화기를 사용한 3차원 도화를 하였으며, 아리랑 및 IRS-lC 위성영상은 데이터에 대한 시스템 지원상의 문제가 있어서 영상정합 방법으로 수치표고모형을 생성한 후 정사보정영상을 제작하여 head-up digitizing에 의한 2차원 도화를 실시하였다. 실험 결과 중해상도 영상으로 큰 도로, 하천, 수애선 등 일부 항목에 대하여 판독과 묘사가 가능하였지만, 불가능한 항목이 많았다. 지도제작 측면에서 SPOT은 1/50,000지형도 수정용, 아리랑 및 IRS-lC는 1/25,000지형도의 수정용으로 활용이 가능하다고 판단되었다.