• 제목/요약/키워드: S.Korea's satellite

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Development of TPF Generation SIW for KOMPSAT-2 X-Band Antenna Motion Control

  • Kang C. H.;Park D. J.;Seo S. B.;Koo I. H.;Ahn S. I.;Kim E. K.
    • 대한원격탐사학회:학술대회논문집
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    • 대한원격탐사학회 2005년도 Proceedings of ISRS 2005
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    • pp.485-488
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    • 2005
  • The 2nd KOrea Multi-Purpose Satellite (KOMPSAT -2) has been developed by Korea Aerospace Research Institute (KARI) since 2000. Multi Spectral Camera (MSC) is the payload for KOMPSAT -2, which will provide the observation imagery around Korean peninsula with high resolution. KOMPSAT-2 has adopted X-band Tracking System (XTS) for transmitting earth observation data to ground station. For this, data which describes and controls the pre-defined motion of each on-board X-Band antenna in XTS, must be transmitted to the spacecraft as S-Band command and it is called as Tracking Parameter Files (TPF). In this paper, the result of the development of TPF Generation S/W for KOMPSAT-2 X-Band Antenna Motion Control.

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Atmospheric Effects during Solar Storms

  • Lee, J.H.;Choi, G.H.;Kim, J.W.;Seo, S.B.;Lee, S.H.
    • 대한원격탐사학회:학술대회논문집
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    • 대한원격탐사학회 2003년도 Proceedings of ACRS 2003 ISRS
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    • pp.840-842
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    • 2003
  • Recent satellite data have revealed a correlation between the Sun’s activities and the Earth’s atmosphere . Many scientists have been conjectured a more direct connections between solar variability and the Earth’s atmosphere from satellite data analysis. During solar storms, more energetic particles reach the Earth’s atmosphere and this phenomenon have effects on the Earth’s atmospheric environment. Consequently, scientists suggest that these variations will affect a global climate change. In this study, we investigate the confirmative research results of atmospheric effects due to solar activities, especially solar storms.

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Performance Enhancement of a Satellite's Onboard Antenna Tracking Profile using the Ground Station Searching Method

  • Song, Young-Joo;Lee, Jung-Ro;Kang, Jihoon;Jeon, Moon-Jin;Ahn, Sang-Il
    • International Journal of Aeronautical and Space Sciences
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    • 제17권3호
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    • pp.391-400
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    • 2016
  • In satellite operations, stable maneuvering of a satellite's onboard antenna to prevent undesirable vibrations to the satellite body is required for high-quality high-resolution images. For this reason, the onboard antenna's angular rate is typically minimized while still satisfying the system requirement that limits the speed of the onboard antenna. In this study, a simple yet effective method, called the ground station searching method, is proposed to reduce the angular rate of a satellite's onboard antenna. The performance of the proposed method is tested using real flight data from the KOMPSAT-3 satellite. Approximately 83% of arbitrarily selected real flight scenarios from 66 test cases show reductions in the onboard antenna's azimuth angular rates. Additionally, reliable solutions were consistently obtained within a reasonably acceptable computation time while generating an onboard antenna tracking profile. The obtained results indicate that the proposed method can be used in real satellite operations and can reduce the operational loads on a ground operator. Although the current work only considers the KOMPSAT-3 satellite as a test case, the proposed method can be easily modified and applied to other satellites that have similar operational characteristics.

Development of the integration information search reference system for a Test-bed area

  • Lee, D.H.;Lee, Y.I.;Kim, D.S.;Kim, Yoon-Soo;Kim, I.S.;Kim, Y.S.
    • 대한원격탐사학회:학술대회논문집
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    • 대한원격탐사학회 2003년도 Proceedings of ACRS 2003 ISRS
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    • pp.1418-1420
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    • 2003
  • This presentation summarizes the development of the integration information search system for a Test-bed area located in Daejeon. It will be used for the validation of software components developed for the high resolution satellite image processing. The system development utilizes the Java programming language and implements the web browse capabilities to search, manage, and augment the satellite image data, the Ground Control Point(GCP) data, the spectral information on land cover types, the atmospheric data, and the topographical map.

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End-to-End Soft QoS Approach for IMS-based Integrated Satellite/Terrestrial Network Architecture

  • Chowdhury, Mostafa Zaman;Jang, Yeong-Min
    • 한국위성정보통신학회논문지
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    • 제2권2호
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    • pp.85-91
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    • 2007
  • The satellite networks provide global coverage. The integration of terrestrial networks with a satellite network is the most attractive approach to develop a global communication system. The IP Multimedia Subsystem (IMS) is intended to be the system that will merge the internet with the telecom world. A user with a dual-mode terminal can access both the satellite network and terrestrial network. The seamless handoff between two networks and a user's QoS level is the major issue concerning this integration. In this paper, we propose IMS-based satellite/terrestrial integrated network architecture for a global communication system. Based on the proposed architecture, an inter-network handoff and end-to-end soft QoS procedure is discussed. Our proposed soft QoS scheme is also analyzed to calculate the number of rejected calls.

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저궤도 5G-NTN 서비스 동향 (LEO 5G-NTN Service Trends)

  • 김병운;최가은
    • 전자통신동향분석
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    • 제38권5호
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    • pp.114-124
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    • 2023
  • Recently, there have been the World Economic Forum's space economy guidelines, the International Telecommunication Union's regulations for each satellite orbit, the development of chips using satellite communication by global manufacturers and service providers, and the registration of key telecommunication businesses. Accordingly, trends in low-orbit 5G satellite communication services in Korea were investigated and analyzed, and the current situation in Korea was diagnosed. Korea's satellite communications accounts for 0.31% of all satellites when analyzed centering on countries with 20 or more satellites. Korea's communication satellite holdings are insufficient compared to 187 times that of the United States, 45 times that of Russia, and 18 times that of China. There is no link technology between 5G and LEO, and the cost of launch vehicles is high. In addition, it is judged that the ecosystem of equipment companies in the low-orbit 5G-NTN business model is insufficient.

미래 한국형 항법위성을 위한 위성항법메세지에 대한 연구 (A study on the navigation message contents of the future Korean navigation satellite)

  • 조중현;이우경;최남미;백정호
    • 한국위성정보통신학회논문지
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    • 제7권1호
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    • pp.108-115
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    • 2012
  • 현재까지 국내 위성항법 연구는 기존 위성항법체계기술을 활용한 연구가 주를 이루었으나, 새로운 위성항법 체계에 대한 연구도 점차 그 중요성이 부각되고 있다. 심지어 대한민국 독자적인 항법위성을 보유하자는 의견도 대두되었다. 지리적, 경제적, 기술적인 이유로 아직 수면 위로 떠오른 적은 없지만 자체 항법위성 관련 우주개발 로드맵이 제 1차 우주개발기본계획에 막연하게 제시되어 있다. 그러나 전세계적으로 4개의 전지국적 위성항법체계가 운영 중이거나 구축 중이고, 여러 개의 지역위성항법 시스템이 계획 중에 있다. 특히 아시아에서 중국은 독자의 전지구적 위성항법시스템 (COMPASS을 2020년에 완성하고자 위성을 발사 중에 있으며, 일본은 지역위성항법 시스템인 QZSS(Quasi Zenith Satellite System)를 2013년 완성을 목표로 제작 및 발사하고 있다. 이제 대한민국도 독자적인 위성항법시스템을 국내 우주개발 기술확보 및 항법안보를 위해서 꼭 개발해야 할 시기이다. 이 연구에서는 대한민국 자체의 위성항법시스템의 개발 여부나 그 개발 가능성을 논하지 않고, 다만 자체의 항법위성을 보유할 경우, 그 항법 메시지에 기존의 정보 외에 어떤 종류의 정보를 실을 수 있는지 조사하여 보았다. 대한민국의 지리적, 경제적 특성상 지역항법위성체계가 첫 번째 항법위성의 탑재체가 될 가능성이 높다. 따라서 이 연구도 이에 준해서 이루어졌다.

Calibration Slope Adjustment for De-Striping KOMPSAT-1 EOC Images

  • Kang, C.H.;Park, D.J.;Ahn, S.I.;Koo, I.H.;Hyun, D.H.;Yang, H.M.;Kim, D.S.;Keum, J.H.;Choi, H.J.
    • 대한원격탐사학회:학술대회논문집
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    • 대한원격탐사학회 2003년도 Proceedings of ACRS 2003 ISRS
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    • pp.1406-1408
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    • 2003
  • KOMPSAT-1 (KOrea Multi-Purpose SATellite ? 1) EOC (Electro Optic Camera) raw images are radiometrically corrected on ground based on the characteristics of EOC. They consist of each CCD (Charge?Coupled Device) pixel’s calibration slope which was measured on ground, electrical gains which are applied to amplify for increasing output pixel counts. Currently, radio-metrically corrected EOC images with calibration slope have still shown defective features by residual stripes. So, it should be compensated by adjusting the calibration slope. In this paper, the adjustment of current calibration slope for de-striping EOC images is addressed and test results are shown.

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TRACKING CONTROL DESIGN USING SLIDING MODE TECHNIQUES FOR SATELLITE FORMATION FLYING

  • Lim, Hyung-Chul;Bang, Hyo-Choong;Park, Kwan-Dong;Park, Pil-Ho
    • Journal of Astronomy and Space Sciences
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    • 제20권4호
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    • pp.365-374
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    • 2003
  • Satellite formation flying is currently an active area of research in the aerospace engineering. So it has been researched by various authors. In this study, a tracking controller using sliding mode techniques was designed to control a satellite for the satellite formation flying. In general, Hill's equations are used to describe the relative motion of the follower satellite with respect to the leader satellite. However the modified Hill's equations considering the $J_2$ perturbation were used for the design of sliding mode controller. The extended Kalman filter was applied to estimate the state vector based on the measurements of relative distance and velocity between two satellites. The simulation results show that the follower satellite tracks the desired trajectory well by thruster operations based on the sliding mode control law.

Study on the Coverage by COMS OCI FOV

  • Kang C. H.;Seo S. B.;Lim H. S.;Park D. J.;Ahn S. I.;Koo I. H.;Hyun D. H.;Yang H. M.;Choi H. J.
    • 대한원격탐사학회:학술대회논문집
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    • 대한원격탐사학회 2004년도 Proceedings of ISRS 2004
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    • pp.336-339
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    • 2004
  • Communication, Ocean and Meteorological Satellite (COMS) has been developed by Korean Aerospace Research Institute (KARI) since 2003. Ocean Color Imager (OCI) is the one of COMS payloads, which will monitor the marine environment around Korean peninsula routinely with the intermediate resolution. But considering COMS is to be located in the geostationary orbit, required geographical coverage is not positioned in the nadir direction of COMS but in specific location with horizontal and vertical offsets from the nadir. In this study, coverage by OCI Field Of View (FOV) is analyzed. First of all, OCI is modeled as the sensor which is a $2,500{\times}2,500$ sized 2-D CCD and the pixel resolution is about 500m. And then, OCI is simulated to be controlled to target the required coverage accurately. As a result of it, coverage by OCI FOV is determined. Finally, all coverages by OCI FOV are mapped.

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