• Title/Summary/Keyword: 위성군

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Analysis of Anti-Jamming Techniques for Satellite Navigation Systems (위성항법시스템을 위한 항재밍 기술 분석)

  • Kim, Ki-Yun
    • The Journal of Korean Institute of Communications and Information Sciences
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    • v.38C no.12
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    • pp.1216-1227
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    • 2013
  • GNSS(Global Navigation Satellite System) is now being widely used in both civilian and military applications where accurate positioning and timing information are required and it is considered as a representative convergence technique in IT-Military application techniques. However, GNSS has low sensitivity level of GNSS receivers and is vulnerable to jamming signal, since the signals come from the satellite located at approximately 20,000 Km above the earth. The studies for the anti-jamming techniques in military applications have been passively performed in the domestic, because the information related GNSS are dependent on the countries that have GNSS. In this paper, we show the effect of jammer ERP by analyzing the link budget of GPS J/S power as a function of distance between jammer and receiver. Also, we categorize the anti-jamming techniques based on the functional block diagram of GNSS receiver structure and analyze the recent anti-jamming GNSS products and their technologies developed in domestic and foreign countries.

Development of On-board Computer Module for Formation Flying and Cluster Operation Nano-satellites (초소형 위성의 편대 및 군집 운용을 위한 모듈형 온보드 컴퓨터 개발)

  • Oh, Hyungjik;Kim, Do-hyun;Park, Ki-Yun;Lee, Ju-in;Jung, Insun;Lee, Seonghwan;Park, Jae-Pil
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.47 no.10
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    • pp.728-737
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    • 2019
  • In this study, the minimized on-board computer (OBC) module for integrated navigation is developed, which provides satellites' relative position information in formation flying and cluster operation situations. The scalability is considered to apply the user-selected wireless communication module and Global Positioning System (GPS) receiver for navigation, while considering to meet the structural design standard of nano-satellites. As a result of the product development and production, the processing speed of integrated navigation and real-time data synchronization is satisfied for cluster operation nano-satellites by using micro controller unit (MCU). From a heat/vacuum, vibration and radiation test, the OBC was confirmed to be operated in space environments. From these results, a mass production system of OBC was made which is a key part of development on satellite formation flying and cluster/constellation missions that the community demands are increasing.

Estimation of Hwanggang dam operation rule using satellite-based water level and reservoir operation algorithm (인공위성 기반 수위와 저수지운영 알고리즘을 이용한 북한 황강댐 운영방식 추정)

  • Jin Gyeom Kim;Chan Young Son;Ki Mook Kang;Ki Bum Nam;Jun Hyuk Choi;Eui Ho Hwang
    • Proceedings of the Korea Water Resources Association Conference
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    • 2023.05a
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    • pp.64-64
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    • 2023
  • 황강댐은 임진강 상류 군사분계선으로부터 약 42km떨어진 위치에 존재하며 약 3~4억톤의 규모로 추정된다. 이에 우리나라는 약 7천만톤 규모의 군남홍수조절지를 건설하여 임진강 상류로부터 기인하는 홍수를 방어하고 황강댐의 무단방류에 대비하고 있다. 과거 2009년 9월 6일 임진강 상류 황강댐에서의 대규모 방류로 인해 경기도 연천군 일대에 홍수가 발생하여 이로 인한 인명 및 재산피해가 발생한 바 있으며, 2020년 8월 5일에는 장마전선으로 인한 폭우와 더불어 임진강 필승교 수위관측소의 수위가 급상승하면서 관측 이래 역대 최고수위가 발생하여 홍수경보가 발령되고 인근 주민이 대피하는 사례가 발생하였다. 또한, 2022년 6월 27일부터 발생한 장마전선 및 집중호우로 인해 임진강 필승교 수위관측소의 수위가 급상승하면서 홍수주의보가 발령되고 인근 주민이 대피하는 사례가 발생하였으며, 7월에는 비가 내리지 않는 상황에서 황강댐의 방류로 추정되는 유입량이 필승교 수위관측소와 군남홍수조절지에서 관측되었다. 이에 본 연구에서는 인공위성 영상에서 추출한 황강댐의 수위를 이용하여 수문모형과 저수지 운영 알고리즘을 구축하고 당시 발생한 홍수사례를 분석하여 황강댐의 운영방식을 추정하였다. 분석결과, 2020년 8월 5~7일 사이에 발생한 유입량의 경우 자체 유역 유입량은 전체 유입량대비 약 33%이나 북한 황강댐으로부터 추가로 방류된 양은 약 67%로 군남홍수조절지 유입량의 3/2 가량이 북한 황강댐의 방류량으로부터 발생된 것으로 보이며 2021년 6월에도 유사한 양상을 보였다. 하지만, 북한 황강댐의 운영방식이 용수공급을 위한 고수위 유지 운영방식에서 홍수기에 댐 월류 및 파괴를 방지하기 위한 사전방류를 수행하는 것으로 추정되었다.

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Capacity of a DS-CDMA Satellite Communication System under a Multitone Jamming (톤 재밍환경에서 DS-CDMA방식 위성통신 링크의 용량분석)

  • Choi, Young-Kyun
    • Journal of the Korean Institute of Telematics and Electronics S
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    • v.36S no.6
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    • pp.30-36
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    • 1999
  • Jamming is an important factor in the military satellite communication system. In this paper, link capacity and jamming margin of the DS-CDMA(Direct Sequence-Code Division Multiple Access) military satellite communication system are analyzed and calculated under a multitone jamming. The analysis was performed with two types of transponders loaded on a geosynchronous satellite. Calculation methods for link capacity and jamming margin were obtained. The results of the analysis show that capacity of a transponder which does modulation/demodulation, decoding/encoding in addition to despreading/respeading is twice as much as that of a tranponder which does despreading /respreading only.

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Analysis of inundation tracing using advanced image (첨단영상기반 침수흔적 분석)

  • Kim, Soo Hyun;Kim, Dong Kyun
    • Proceedings of the Korea Water Resources Association Conference
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    • 2019.05a
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    • pp.66-66
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    • 2019
  • 침수흔적도는 풍수해로 인한 침수기록(침수심, 침수위, 침수시간 등)을 조사하여 표시한 도면으로 자연재해 경감 및 신속한 대피를 위하여 작성하도록 자연재해대책법에 따라 규정되어있다. 이러한 침수흔적도는 국가 방재에 따른 기초자료로 사용되지만 광범위한 지역을 신속 정확하게 조사하기에는 예산 부족 및 관리 미흡으로 한계가 있다. 따라서 본 연구는 2018년 10월초 경북 영덕군에서 발생한 태풍 콩레이 침수피해사상을 대상으로 위성영상기반 침수판별지도를 작성하였고, 이를 실제자료와 비교하여 침수흔적도 작성 시 첨단영상의 활용가능성을 확인하였다. 위성영상으로는 ESA의 Sentinel-1과 PlanetLab사(社)의 PlanetScope를 활용하였고, 검증에 활용한 자료는 CCTV를 영상자료를 활용하여 정확성을 평가하였다. 침수심과 침수규모를 확인하기 위해 사용한 지형자료는 10m DEM자료와 드론영상자료를 통해 구축한 DSM을 활용하였다. 그 결과 위성영상을 활용한 침수판별지도는 실제 CCTV영상자료와 높은 상관관계를 보이는 것으로 나타났으며, 드론영상을 통해 지형자료를 구축한 경우 DEM에 비해 정확도가 높아지는 것을 확인할 수 있었다. 또한 위성영상자료의 해상도가 높을수록 실제자료와 유사하게 침수규모를 판별할 수 있는 것으로 나타났다. 첨단영상을 활용한 침수흔적도 작성은 기존조사보다 신속하고 광범위하게 자료를 수집할 수 있을 것으로 기대한다.

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The Study on The Application of QAM-OFDM Scheme for Nonlinear Satellite Channel (비선형 위성 채널에서 QAM-OFDM 방식의 적용에 관한 연구)

  • Lee, Hae-Seon
    • 전자공학회논문지 IE
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    • v.45 no.1
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    • pp.44-49
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    • 2008
  • In this paper, the performance for the non-linear satellite channel including the characteristics of group delay and gain ripple of transponder is analyzed with multi-level QAM-OFDM schemes. Comparing the BER performances between general OFDM and CI(Carrier Interferometry)-OFDM for various QAM schemes, the degree of performance improvement is presented in AWGN environments for specified nonlinear characteristics. The simulations are performed with the 36MHz bandwidth of transponder channel and 120Mbps transmission rate for QPSK, 8QAM, 16QAM, 32QAM, 64QAM schemes between normal and worst case condition. It is shown that the improvement measure by the CI-OFDM for the group delay of channel and nonlinear characteristic of HPA outperforms that for the gain ripple in the case of higher level QAM scheme in normal condition. And the simulation results show that the additional techniques like the channel coding and compensation scheme against the nonlinear characteristic are required for 32QAM and higher level QAM in worst case condition.

The Performance Improvement of the OFDM Based Satellite Communication System with the Consideration of Transponder Characteristics (위성 중계기 특성을 감안한 OFDM 기반 위성 통신 시스템의 성능 개선)

  • Lee, Hae-Seon
    • The Journal of Korean Institute of Electromagnetic Engineering and Science
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    • v.18 no.10
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    • pp.1196-1202
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    • 2007
  • In this paper, the effects of performance improvement far the OFDM based satellite communications are analyzed with applying the CI(Carrier Interferometry)-OFDM and channel coding scheme considering the group delay and gain ripple characteristic as well as the nonlinear characteristic of the transponder. Comparing the BER between traditional OFDM and CI-OFDM, the degree of performance improvement is presented in AWGN channel environments for specified backoff condition of HPA. The simulations are performed with the 36 MHz bandwidth of transponder channel, 120 Mbps transmission rate, and 16 QAM modulation scheme between ideal and worst case condition. It is shown that the improvement measure by the CI-OFDM and channel coding for the group delay and nonlinear characteristic outperforms that for the gain ripple in terms of performance degradation presented by the individual characteristics. And the simulation results show that the effects of improvement by the CI-OFDM outperforms the effect by the applied channel coding, particularly in worst case condition.

네트워크 전쟁에서 실시간 지휘 통제 기술들

  • O, Je-Sang
    • Defense and Technology
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    • no.7 s.293
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    • pp.50-57
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    • 2003
  • 이라크 전쟁에서 네트워크 체계는 우주의 인공위성에 의한 정찰과 고고도, 중고도 및 저고도의 용도별 정찰 항공기들로부터 수집한 정보의 분석 및 융합을 거의 실시간으로 처리하여 그 정보를 요구하는 부대에 신속히 전파할 수 있는 네트워크 체계로서 우주선을 활용하여 전파할 수 있으므로 필요한 부대에서 정확한 정보를 이용한 정밀 공격이 가능하였던 것으로 판단된다. 이러한 네트워크 전쟁의 양상으로 판단할 때, 우리 군도 미래 네트워크 전쟁에 대비한 군사력 건설을 강화하여 앞서 언급한 기술들을 기반으로 하는 네트워크 체계 중심의 우주 및 공중 정찰로부터 필수적으로 요구되는 정보를 수집할 수 있는 정보 수집 및 분석/융합 네트워크 체계와 우주 및 공중으로부터 정밀 유도할 수 있는 정밀 유도 네트워크 체계를 건설하여야 할 것이다.

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A Linkage Based Space Debris Capture Device Utilizing Kevlar Wires (Kevlar wire를 이용한 링크 구동형 우주잔해 포획장치)

  • Jung, Jinwon;Hwang, Bohyun;Kim, Heekyung;Lee, Gunhee;Seo, Minseok;Lee, Dongyun;Kim, Byungkyu
    • Journal of Aerospace System Engineering
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    • v.11 no.5
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    • pp.36-41
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    • 2017
  • As the space debris in the satellite orbit increases, the risk of collision between the currently operating satellites and the space debris is continuously increasing. Therefore, in this study, we designed one-degree-of-freedom capture device using simple deployment mechanism. The capture device consists of four link groups connected with net. To increase the reliability, each link group is connected to one driving part so that the total degree of freedom is 1. In addition, the links were stowed on each side of the satellites so that they would not affect the janitor satellite mission. Finally, to confirm the possibility of deployment in the space environment, we carried out deployment experiments in water similar to the microgravity environment, and confirmed the deployment of capture device and the possibility of capturing target satellite.

A Study on the Applicability of Air Launch Vehicle (공중발사체의 활용가능성 분석 연구)

  • Kwon, Kybeom;Lee, Kanghyun;Cho, Ye Rang;Ji, Wan Gu;Kim, Kyu Hong
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.50 no.3
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    • pp.203-214
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    • 2022
  • As the global demand for small satellites weighing less than 500 kg increases, the development and operation of dedicated small launch vehicles increase significantly. The responsiveness of a launch vehicle that puts a small satellite into a target orbit at the desired time is attracting attention. As a result, interest in the air launch is increasing in the rapid establishment of a constellation. As the demand for small satellites in south Korea increases, this study performed analyses on the applicability of an air launch vehicle using a large civil aircraft considering the geographical environment. In terms of responsiveness, mission response times were compared and analyzed for air launch vehicles and ground small and large vehicles. In addition, an air vehicle and a small ground vehicle were quantitatively compared and analyzed for the orbital insertion performance. As a result of the analysis, the air launch vehicle has limited responsiveness in Korea regarding rapid satellite constellation establishment. However, it can be an effective alternative for low inclination angle orbit insertion with the benefit of a fast turnaround time. Furthermore, the performance of the orbital injection is close to that of the ground small launch vehicle, and the high efficiency in terms of the required propellant mass is possible, so air launch can be an effective launch means for putting small satellites into orbit in Korea.