• 제목/요약/키워드: mission operation

검색결과 552건 처리시간 0.028초

OVERALL LINK ANALYSIS ON HRIT AND LRIT IN COMS

  • Park Durk-Jong;Hyun Dae-Wan;Kang Chi-Ho;Ahn Sang-Il;Kim Eun-Kyu
    • 대한원격탐사학회:학술대회논문집
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    • 대한원격탐사학회 2005년도 Proceedings of ISRS 2005
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    • pp.98-100
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    • 2005
  • This paper describes link analysis on the processed data, HRIT (High Rate Information Transmission) and LRIT (Low Rate Information Transmission), for the preliminary design of interface between COMS (Communication, Ocean and Meteorological Satellite) and ground station. At the MODAC (MeteorologicaVOcean Data Application Center), the processed data are transmitted to user station via COMS with normalization and calibration by pre-processing of MI (Meteorological Imager) data. Due to consider satellite as radio relay, overall analysis containing uplink and downlink is needed. Specific link parameters can be obtained with using the outcomes of SRR (System Requirement Review) which was held on 13-14 June 2005, in Toulouse. From the relation between overall link margin and output power of HPA (High Power Amplifier) of MODAC, it is shown that even though the minimum power related with COMS receiving power range is transmitted at MODAC, the obtained link margin of HRIT could be above 3 dB at user station which antenna elevation angle is 10 degree.

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PERFORMING OF SOC DATS INTERFACE TEST WITH MODEM/BB

  • Park, Durk-Jong;Hyun, Dae-Hwan;Koo, In-Hoi;Ahn, Sang-Il;Kim, Eun-Kyou
    • 대한원격탐사학회:학술대회논문집
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    • 대한원격탐사학회 2006년도 Proceedings of ISRS 2006 PORSEC Volume I
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    • pp.64-66
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    • 2006
  • DATS will connect with IMPS and LHGS to perform the reception of sensor data and the transmission of user's meteorological data, LRIT and HRIT. MODEM/BB will perform the de-commutation of received sensor data as MI and GOCI raw data according to VCID before sending them to MI and GOCI IMPS, respectively. Especially, MODEM/BB in SOC needs to be connected to six clients that consist of the primary and backup IMPS of MSC, KOSC and SOC. On the other hand, LRIT and HRIT delivered from LHGS are encoded as VITERBI and modulated by MODEM/BB. Considering sensor data transmitted from COMS, the assumed format and size of CADU are described in this paper. Finally, results related to the status of received LRIT and HRIT by frame synchronizer in user station are also described.

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소형 무인기들의 군집비행을 위한 운영 네트워크 시스템과 PILS 개발 (Development of Operation Network System and Processor in the Loop Simulation for Swarm Flight of Small UAVs)

  • 김성환;조상욱;조성범;박춘배
    • 제어로봇시스템학회논문지
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    • 제18권5호
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    • pp.433-438
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    • 2012
  • In this paper, a operation network system equipped with onboard wireless communication systems and ground-based mission control systems is proposed for swarm flight of small UAVs. This operating system can be divided into two networks, UAV communication network and ground control system. The UAV communication network is intend to exchange the informations of navigation, mission and flight status with minimum time delay. The ground control system consisted of mission control systems and UDP network. Proposed operation network system can make a swarm flight of various UAVs, execute complex missions decentralizing mission to several UAVs and cooperte several missions. Finally, PILS environments are developed based on the total operating system.

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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군집위성 임무운영시스템 발전방향 및 자동화 우선순위 평가 (Future Direction of Mission Operation System for Satellite Constellation and the Automation Priority Evaluation)

  • 정인식;윤정훈;이명신;이정현;권기범
    • 항공우주시스템공학회지
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    • 제16권3호
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    • pp.10-22
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    • 2022
  • 우주개발진흥 기본계획에 따르면 2031년까지 110여 기의 위성이 운영될 것으로 예상되며, 이에 따라 기존의 소수의 다중위성 운영과는 다른 군집위성 운영을 위한 운영개념과 기술이 필요하다. 효율적인 군집위성 운영을 위해 임무운영시스템의 자동화 및 최적화가 필수적이며, 국내에서도 군집위성 운영을 위한 준비가 시급하다. 본 논문에서는 효율적인 군집위성 운영을 위해 자동화 및 최적화를 적용한 임무운영시스템 발전방향 및 추진전략을 제안하였으며, 임무운영시스템의 자동화 수준 및 우선순위 평가를 위한 프레임워크를 개발하여 자동화를 우선적으로 적용하여야 하는 업무를 식별하였다.

Operational Report of the Mission Analysis and Planning System for the KOMPSAT-I

  • Lee, Byoung-Sun;Lee, Jeong-Sook;Kim, Jae-Hoon;Lee, Seong-Pal;Kim, Hae-Dong;Kim, Eun-Kyou;Park, Hae-Jin
    • 한국우주과학회:학술대회논문집(한국우주과학회보)
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    • 한국우주과학회 2003년도 한국우주과학회보 제12권2호
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    • pp.46-46
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    • 2003
  • Since its launching on 21 December 1999, the KOrea Multi-Purpose SATellite-Ⅰ (KOMPSAT-Ⅰ) has been successfully operated by the Mission Control Element (MCE), which was developed by the Electronics and Telecommunications Research Institute (ETRI). Most of the major functions of the MCE have been successfully demonstrated and verified during the three years of the mission life of the satellite. The Mission Analysis and Planning Subsystem (MAPS), which is one of the four subsystems in the MCE, played a key role in the Launch and Early Orbit Phase (LEOP) operations as well as the on-orbit mission operations. This paper presents the operational performances of the various functions in MAPS. We show the performance and analysis of orbit determinations using ground-based tracking data and GPS navigation solutions. We present four instances of the orbit maneuvers that guided the spacecraft from injection orbit into the nominal on-orbit. We include the ground-based attitude determination using telemetry data and the attitude maneuvers for imaging mission. The event prediction, mission scheduling, and command planning functions in MAPS subsequently generate the spacecraft mission operations and command plan. The fuel accounting and the realtime ground track display also support the spacecraft mission operations. We also present the orbital evolutions during the three years of the mission life of the KOMPSAT-Ⅰ.

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소형 무인항공기의 임무 및 제어를 위한 시스템 구성과 통신 장비 운용에 대한 연구 (A Study on the System Configuration and Communication Equipment Operation for Mission and Control of Small UAV)

  • 하영석
    • 융합정보논문지
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    • 제9권11호
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    • pp.118-124
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    • 2019
  • 무인항공기의 기술이 많이 보급화 되면서 다양한 종류의 무인항공기 및 임무 다변화에 따라 다양한 종류의 임무 장비가 개발되고 있다. 그중에서도 국내에서는 소형 무인항공기가 활발히 개발되고 있으며 소형 무인기의 효과적인 조정을 위한 비행제어 시스템과 임무 장비의 연동 시스템이 필요하고, 또한 데이터를 처리하여 지상 운용시스템으로 전송을 위한 효율적인 통신장비의 구성 및 운용이 요구되고 있다. 본 논문에서는 소형 무인항공기의 임무 및 제어를 위하여 비행제어 시스템과 임무 장비 제어 시스템을 이용한 임무 장비의 확장, 데이터 링크 통합 및 통신장비 운용에 대하여 서술하였으며 이를 통하여 효과적인 소형 무인항공기의 운용에 대하여 정리하였다.

위성 임무운영팀 동향 (The Trend of Satellite Mission Operations Team)

  • 이명신;정옥철;정대원;박선주;신정훈
    • 항공우주산업기술동향
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    • 제6권1호
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    • pp.105-115
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    • 2008
  • 위성의 임무운영팀 조직은 운영되는 위성의 개수,탑재체 운영지원의 여부,임무운영센터 내에서의 안테나 운영 여부, 지상시스템 자동화 정도 및 임무운영에 대한 기술지원 기능 여부에 따라서 다양한 구성이 존재할 수 있다. 위성운영 업무를 담당하는 운영조직의 구성이나 기능은 임무운영의 복잡도에 따라 약간씩 차이가 있으나 대부분의 위성운영센터는 단일 또는 복합 임무운영 지원을 위해 유사한 조직 구성을 갖는다. 항우연 임무운영센터는 아리랑위성1호 발사(1999년 12월 21일)이후 임무운영팀의 업무를 시작한 이래, 아리랑 위성 2호, 아리랑위성 3호와 5호 및 통신해양기상위성에 대한 다중임무운영의 개념으로 진화하고 있다. 본 동향에서는 본격적인 다중임무운영에 앞서 체계적인 임무운영센터의 조직을 구성하고자 해외 선진 임무운영 개념에 대한 권고사항과 실제 적용되고 있는 사례를 살펴본 후, 항우연 임무운영센터의 현재 현황과 비교분석함으로써 조직 운영의 적합성과 향후 발전방향에 대해서 살펴보고자 한다.

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Link-16 기반의 효율적인 공대지 항공작전 모델 설계 (Establishment for Efficiency Air-To-Ground Air Operation Model in Link-16)

  • 이형헌;장형준;김영구;임재성
    • 한국군사과학기술학회지
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    • 제13권5호
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    • pp.861-868
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    • 2010
  • As CAS, X-ATK, and INT models considered as the most typical Air-to-Ground operation models in ROKAF are mainly designed as the voice-centered system between aircraft and ground control facilities, it is critical to newly develop the Link-16 based model for the ROK-US combined operation between F-15K, AWACS, M-SAM, and KDX-III equipped with Link-16. Former studies had been limited to the CAS operation, and they had mainly focused on reducing the voice transmission time to exchange the information between each mission step with maintaining existing operation steps. Therefore, this paper makes up the weak point in former studies, thereby designing new Air-to-Ground operation model for CAS, X-ATK, INT mission using Enterprise Architecture OV6c, which enables both aircraft and ground control facilities or between aircraft to obtain the real-time information on the location, identification, armament and the real-time image data through the broadcasting function. Based on the analysis of new operation model, we come to a conclusion that by simultaneously exchanging the information on mission between nodes concerned through the broadcasting function of Link-16. It is possible to cut down superfluous steps among the mission steps, and to reduce the mission time. It is clear that it gives rise to improve the battle efficiency and the decision-making tempo as well as the battlefield situational awareness.

BITSE Ground Software

  • Baek, Ji-Hye;Park, Jongyeob;Choi, Seonghwan;Kim, Jihun;Yang, Heesu;Kim, Yeon-Han;Swinski, Joseph-Paul A.;Newmark, Jeffrey S.;Gopalswamy, Nat.
    • 천문학회보
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    • 제44권2호
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    • pp.58.1-58.1
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    • 2019
  • We have developed Ground Software (GSW) of BITSE. The ground software includes mission operation software, data visualization software and data processing software. Mission operation software is implemented using COSMOS. COSMOS is a command and control system providing commanding, scripting and data visualization capabilities for embedded systems. Mission operation software send commands to flight software and control coronagraph. It displays every telemetry packets and provides realtime graphing of telemetry data. Data visualization software is used to display and analyze science image data in real time. It is graphical user interface (GUI) and has various functions such as directory listing, image display, and intensity profile. The data visualization software shows also image information which is FITS header, pixel resolution, and histogram. It helps users to confirm alignment and exposure time during the mission. Data processing software creates 4-channel polarization data from raw data.

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