• Title/Summary/Keyword: 아리랑

Search Result 316, Processing Time 0.025 seconds

Introduction of Satellite Remote Sensing Technologies to Korea Coast Guard (해양경찰청 위성활용 방안)

  • Yang, Chan-Su;Oh, Jeong-Hwan
    • Proceedings of the Korean Institute of Navigation and Port Research Conference
    • /
    • 2011.11a
    • /
    • pp.154-155
    • /
    • 2011
  • 2010년 천리안위성의 성공적인 발사에 따라 인공위성의 활용에 대한 기대가 커지고 있다. 천리안 해양관측위성(GOCI)이외에 아리랑 2호가 현재 운용중인 우리나라 위성들이다. 가까운 시기에 아리랑 5호(2011년 말), 아리랑 3호(2012년), 아리랑 3A호(2013년)가 발사될 예정이다. 즉, 해양적용을 위한 위성환경은 이제부터 준비되고 있다고 볼 수 있다. 대외적으로 보면, 인공위성 자원은 아주 많다. 문제는 이와 같은 자원을 어떻게 활용할 것인가 인데 이의 활용 기술 개발적 측면에서는 많이 소홀한 것이 사실이다. 전세계적으로 이 시스템 개발을 위한 치열한 경쟁이 진행 중에 있다. 이미 소말리아 주변 감시체계는 많은 부분을 위성에 의지하고 있다. 우리나라에서 최초로 위성활용 가능성을 보여준 사건이 허베이스피리트호 원유유출 사고이다. 이 사고는 2007년 12월7일 아침 7시6분경 서해안 만리포 북서쪽 10km 해상에서 크레인을 적재한 1만1800t급 바지선이 정박 중인 홍콩 선적 유조선 허베이 스피리트호(14만6000t급)와 부딪치면서 발생했다. 이와 같은 기름 유출 사고의 경우, 유출 범위를 정확하게 이해하는 것이 중요하다. 거의 준비된 상태가 아님에도 불구하고 12월 8일 아침 최초로 유출된 기름을 모습을 보여주는 위성이미지(광학위성)가 얻어졌다. 하지만 이와 같은 자료가 관련 전문가가 이용할 수 있기까지 많은 시간이 소용되었고, 이 정보를 전달할 수 있는 방법도 없었다. 사실 단순한 이미지가 아니라 지리정보체계를 가진 오염정보를 제공할 방법도 준비도 되어 있지 못한 상황이었다. 본 발표를 통하여, 허베이스피리트호 사고뿐만 아니라, 2011년 6월부터 수개월간 지속된 발해만 오염사고 적용 등 다양한 사례 소개를 하고, 이를 기반으로 해양경찰청에서 업무활용을 위한 방안을 제시한다. 먼저, 해경청의 주요 임무인, 경비, 수색구조, 오염대응 분야별로 현황 분석을 수행하였다. 또한 국외사례에 대한 조사를 한 후, 최종 인공위성 원격탐사기술의 해경청 도입방안에 대한 설계를 실시하였다. 국제적으로 인공위성을 이용한 해양 경비, 수색구조, 오염 모니터링기술 개발이 이루어지고 있으며, 유럽 국가는 시범도입을 진행 중에 있다. 유럽해사안전국(EMSA)은 해양경비 및 수색구조를 위한 선박통항 및 보고 서비스와 오염대비대응(Pollution Preparedness and Response, PPR) 위성 서비스를 회원국에 제공하고 있다. 해양경찰청 임무 수행뿐만 아니라, 해양영토 관리적 측면에서 첨단 위성장비 활용, 선진국형 해상경비 패러다임의 전환 필요성이 크다고 할 수 있다.

  • PDF

Analysis of the Targeting Accuracy of KOMPSAT-1 EOC (아리랑위성1호EOC영상촬영의 지향정확도분석)

  • Jeon, Gap-Ho;Kim, Yun-Su;Seo, Du-Cheon
    • Aerospace Engineering and Technology
    • /
    • v.5 no.2
    • /
    • pp.220-226
    • /
    • 2006
  • At present the KOMPSAT-1 is operating for seven years, though mission life time was only three years. We expect the KOMPSAT-1's mission for several years ahead, considering the KOMPSAT-1's current conditions. However, a question that the plan and the result was not equal have being arises. Recently, we attempted to take a picture of the Mount Everest. But we don't take a picture of the Mount Everest in the center of image. This paper make clear the difference between target center from operating commender and image center from received data, for the continual and stable KOMPSAT operation.

  • PDF

A Study on the Efficient Orthorectification of KOMPSAT Image (아리랑 영상의 효율적 정사보정처리 연구)

  • Oh, Kwan-Young;Lee, Kwang-Jae;Hwang, Jeong-In;Kim, Youn-Soo
    • Korean Journal of Remote Sensing
    • /
    • v.37 no.6_3
    • /
    • pp.2001-2010
    • /
    • 2021
  • The purpose of this study is to efficiently improve orthorectification of KOMPSAT images. As the development of domestic and abroad earth observation satellites accelerates, the number and amounts of satellite images acquired are rapidly increasing. Accordingly, various studies are being conducted to improve orthorectification for the acquired image more quickly and efficiently. This study focused on enhancing processing efficiency through algorithm improvement, except for improving hardware computing capabilities such as GPU. Accordingly, the algorithm was improved with the LUT-based RFM method, and compared and analyzed in terms of accuracy and time-efficiency that vary depending on offset settings.

Definition and Monitoring of Image data Quality for KOMPSAT-3 from users (사용자 측면에서의 아리랑위성 3호 영상자료의 품질 정의 및 관리)

  • Lee, DongHan;Kim, Mina;Seo, DooChun;Jeong, JaeHeon;Jeon, KyeongMi
    • Aerospace Engineering and Technology
    • /
    • v.13 no.2
    • /
    • pp.87-98
    • /
    • 2014
  • Generally there is a technical gap for the image data quality between from the satellite requirement values and from the users. After Cal/Val for KOMPSAT-3 had been done by Dec. 31, 2012, all requirements for KOMPSAT-3 image data quality have been validated, and then the normal operation of it started from Jan. 2013. In the normal period, the image data quality for the users has been defined and managed, and according to the result of it, the additional Cal/Val items have been doing. Cal/Val team and Processing team in KARI made the quality report (QR) for KOMPSAT-3 image data quality for the users, and have determined the quality level of KOMPSAT-3 product generated by Processing system (PMS; Product Management System) and managed the quality report for it. According to the result of the quality report, Cal/Val team defined six additional Cal/Val items, and has done five items of them and has been implementing the result of them into the Processing system.

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

  • Lee, Myeong-Shin;Jung, Ok-Chul;Chung, Dae-Won;Park, Sun-Ju;Shin, Jung-Hoon
    • Current Industrial and Technological Trends in Aerospace
    • /
    • v.6 no.1
    • /
    • pp.105-115
    • /
    • 2008
  • The organization for satellite operation team is mainly based on the number of satellites to be controlled, operator's workload of payload operation support and the degree of automation of the operation system. Although the structure and its functionality of satellite operation organization are a little different according to the complexity of the operation, most satellite control centers have adapted the similar architecture for single or multiple satellite support. KARI Satellite Operation Center(KSOC) has started its simple mission operations since the launch of KOMPSAT-1(21st Dec. 1999) and has been evolving into multiple mission operations for various satellites such as KOMPSAT-2, KOMPSAT-3, KOMPSAT-5 and COMS(Communication Ocean Meteorological Satellite). This paper presents the appropriate direction of future deployment for KSOC by comparing the current status with the recommendation of the advanced satellite operation organization and analyzing their experiences in order to propose the better solution for efficient and safe satellite operations.

  • PDF

Traditions and performance of oral folk song singers - focusing on the case of Taebaek Ararei singers for 3 generations /Lee Chang-Sik(Semyung Uni. Prof) (아리랑유산 가창자의 전승과 공연)

  • Lee, Chang Sik
    • (The) Research of the performance art and culture
    • /
    • no.32
    • /
    • pp.171-208
    • /
    • 2016
  • Female folk song singers do not necessarily recognize the indigenous elements, which are, however, naturally reflected in the narration in the context. Singers of Taebaek Ararei recognize the dialect, the tone and the song when performing. Traditional Ararei had been performed by singers in the village of slash-and-burn field in Hwangji. Cheolam and Jangseong do not have their own traditional songs sing they are mining regions but had adopted songs from other areas including Gyeonggbuk, which still remain as alternative versions. Many elements of Jeongseon Arari and Samcheok Menari are in the narration and the songs. In terms of the context, alternative versions of Ararei are old Arirang melodies from slash-and-burn fields and were confirmed to be a very old form of oral folk songs in Gangwondo. Female singers of 3 generations, Hwaok Mun, Geumsu Kim and Hyojeong Kim, who keep the tradition and identity of Taebaek Ararei, show the integration of the past, present and future of Ararei. The Ararei Preservation Society continuously organizes singers' performances and maintains the tradition. The singer Hwaok Mun was born in Taecheon, Pyeongannamdo and moved to south at 5 and lived in Hajang, Samcheok and then moved to Jangseong and lived in Jaemungok. She is a mother of 6 children and has been a farmer for most of her life. She currently resides in Mungokdong and would sing Ararei at village feasts or events. She says she learned the song naturally because Ararei was sung very often in the past around Taebaek area. She is a typical native Arirang singer. The singer Geumsu Kim is a daughter of Hwaok Mun and leads the Taebaek Ararei Preservation Society to study, maintain and introduce the sound of Taebaek(Taebaek Arirang). She introduces Miner Arirang and Taebaek Ararei to the society members and the local residents. The singer Hyojeong Kim is a granddaughter of Hwaok Mun and follows the tradition of her grandmother and mother while adopting more modern Arirang contents.

The Design of Inter-processor Synchronization of KOMPSAT (아리랑위성 프로세서간 동기화 설계)

  • 천이진;정창호
    • Proceedings of the Korean Information Science Society Conference
    • /
    • 1998.10a
    • /
    • pp.42-44
    • /
    • 1998
  • 위성 시스템은 전력 분배, 자세 제어, 열 제어 및 임무 수행에 필요한 탑재체 지원과지상과의 명령 수신 및 측정데이터의 수집을 위해서 프로세서를 내장하고 있다. 임무 수행 및 시스템의 복잡성 여부에 따라서 하나의 프로세서만을 탑재하기도 하지만 여러 개의 프로세서를 탑재하여 기능에 적합하게 분배하여 운용하기도 한다. 아리랑위성은 3개의 프로세서사 탑재되며, 크게 나누어 원격 측정 명령계, 자세 제어계 그리고 전력계에 기능을 담당하게 된다. 하나 이상의 프로세서를 탑재하게 되면 프로세서간의 동기화가 요구되며 프로세서간의 정보 전달을 위해서 통신 채널이 필요하게 된다. 실제로 프로세서간의 동기화는 상호 통신에 있어서 기준 점을 제공하므로 매우 중요한 의미를 가진다. 본 논문에서는 아리랑위성의 동기화는 어떤 방식으로 설계되었으며, 어떻게 운영되는지에 대해 설명한다.

  • PDF

Comparison of Carcass Characteristics, Meat Quality, and Sensory Quality Characteristics of Male Laying Hens, Meat-Type Chickens under Identical Rearing Conditions (동일 사육 조건에서 산란계 수평아리 및 육용계의 도체 특성, 계육 품질 및 관능적 특성 비교)

  • Woo-Do Lee;Hyunsoo Kim;Hee-Jin Kim;IkSoo Jeon;Jiseon Son;Eui-Chul Hong;Hye Kyung Shin;Hwan-Ku Kang
    • Korean Journal of Poultry Science
    • /
    • v.51 no.1
    • /
    • pp.11-19
    • /
    • 2024
  • This study was conducted to evaluate the potential of using laying hens as meat type chickens. Male broiler (Ross 308, R3), laying hens (Hy-Line Brown, HL), and Korean native chickens (Hanhyup-3, H3) were used, and 100 heads of each were prepared. Carcass characteristics, meat quality, and sensory quality characteristics were compared as analysis items. The rearing environment and feed for all treatments were identical to the broiler rearing manual, and the lighting system was maintained at 23L:1D. Feed and water were provided ad libitum. The test ended when the average weight of each treatment group reached 1.5 kg, and individuals of similar weight were randomly selected and compared. As a result of this study, the live weight of the selected individuals was approximately 1.5 kg, which was similar for all treatments (P>0.05). However, carcass weight and ratio and breast meat production were highest in R3, while HL had higher ratios of legs, wings, and neck (P<0.05). The H3 group showed high pH and WHC levels and low cooking loss, and R3 improved chicken meat color (P<0.05). In particular, the fat content in meat was lowest in HL (P<0.01). Nucleic acid substances ATP, Hx, ADP, AMP, and INO were abundant in R3, and IMP content was highest in HL (P<0.05). In sensory evaluation, all treatments showed similar characteristics and overall preferences (P>0.05). Based on the findings, it appears that HL, a male laying hen, produces meat with unique characteristics such as low fat content and high IMP content.

Analysis of NWP GRIB Data for LEO Satellite Mission Planning (저궤도 관측위성 임무계획(Mission Planning)을 위한 기상수치예보 GRIB Data 분석)

  • Seo Jeong-Soo;Seo Seok-Bae;Bae Hee-Jin;Kim Eun-Kyou
    • Proceedings of the KSRS Conference
    • /
    • 2006.03a
    • /
    • pp.178-186
    • /
    • 2006
  • 기상 수치예보는 (Numerical Weather Pridiction, NWP)는 바람, 기온, 등과 같은 기상요소의 시간 변화를 나타내는 물리방정식을 컴퓨터로 풀어 미래의 대기 상태를 예상하는 과학적인 방법으로 지구를 상세한 격자 2진부호(GRIdded Binary, 이하 GRIB)로 나누어 그 격자점에서의 값으로 대기 상태를 나타낸다. 지구 각지에서의 각종 관측자료를 기초로 격자점상의 현재값을 구한다. 대용량의 격자데이터는 이진형태이어서 컴퓨터, 서버 저장장치에서 동일형태 데이터로 존재한다. 우리나라 최초의 저궤도 관측 위성인 다목적 실용위성 KOMPSAT-1호(이하, 아리랑 위성1호)는 전자광학카메라(Electro Optical Camera, EOC)를 탑재하여 1999년 12월 21일에 발사된 이후 2006년 1월 현재까지 6여년간 성공적으로 임무를 수행, 7049여회의 영상을 획득하여 국가적으로 귀중한 자료로 활용하고 있다. 아리랑 위성1호는 일일 2-3회 EOC영상을 획득하고 있으며, 임무계획(Mission Planning)은 MP(Mission Planner)가 사용자로부터 자료를 수집하여 임무분석 및 계획 서브시스템(MAPS)에 의해 계산되어진 위성의 제도예측 데이터에 촬영하고자하는 목표지점 좌표를 입력하여 자동명령생성기(KSCG)에 의해 계산된 촬영 경사각도(Tilt)값을 위성에 전송하여 목표지역의 영상을 획득하게 된다. 위성영상 획득에 있어 고가의 위성을 운영하면서 기상의 상태를 정확히 예측하여 실패없이 유효한 영상을 획득하는 것이 무엇보다 중요하다. 본 논문에서는 효율적인 위성임무계획을 위한 기상수치예보 자료를 분석하여 앞으로 발사하게 될 고해상 카메라 탑제위성인 아리랑 위성2호와 3호에 적용하고자 한다. the sufficient excess reactivity to override this poisoning must be inserted, or its concentration is decreased sufficiently when its temporary shutdown is required. As ratter of fact, these have an important influence not only on reactor safety but also on economic aspect in operation. Considering these points in this study, the shutdown process was cptimized using the Pontryagin's maximum principle so that the shutdown mirth[d was improved as to restart the reactor to its fulpower at any time, but the xenon concentration did not excess the constrained allowable value during and after shutdown, at the same time all the control actions were completed within minimum time from beginning of the shutdown.및 12.36%, $101{\sim}200$일의 경우 12.78% 및 12.44%, 201일 이상의 경우 13.17% 및 11.30%로 201일 이상의 유기의 경우에만 대조구와 삭제 구간에 유의적인(p<0.05) 차이를 나타내었다.는 담수(淡水)에서 10%o의 해수(海水)

  • PDF

A Study of the Disposal Maneuver Planning for LEO Satellite (저궤도 위성의 폐기기동 계획 연구)

  • Seong, Jae-Dong;Kim, Hae-Dong;Choi, Ha-Yeon
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.44 no.4
    • /
    • pp.352-362
    • /
    • 2016
  • In this paper, a disposal maneuver which complies the space debris mitigation guideline was analysed for KOMPSAT-2 as an example of LEO satellite. Definition of disposal altitude which comply the '25 year rule', re-entry survivability analysis of KOMPSAT-2 parts inside and casualty area analysis were performed using STK and ESA's DRAMA. Finally, assuming that there were several survival objects during uncontrolled re-entry stage, the re-entry initial orbit elements which show the low casualty probability were found even if there were various uncertainties about the initial orbit. As a result, KOMPSAT-2 should be descended its altitude at least 43km or up to 105km to comply '25 year rule' and there were heavy or heat resistant survival objects which generated $4.3141m^2$ casualty area. And if RAAN of re-entry initial orbit was 129 degree, total casualty probability was lower than standard value of space debris mitigation guideline even if there were uncertainties about the initial orbit.