• 제목/요약/키워드: Altitude of the sun

검색결과 243건 처리시간 0.023초

INTRODUCTION OF AOCS HARDWARE CONFIGURATION FOR COMS

  • Park, Young-Woong;Park, Keun-Joo;Lee, Hoon-Hee;Ju, Gwang-Hyeok
    • 대한원격탐사학회:학술대회논문집
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    • 대한원격탐사학회 2007년도 Proceedings of ISRS 2007
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    • pp.207-210
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    • 2007
  • A part of the big differences between LEO(Low Earth Orbit) and GEO(Geostationary Earth Orbit) satellite is that transfer orbit is used or not or what tolerance of the position on the mission orbit is permitted. That is to say, the transfer orbit is not used and the constraint of orbit position is not adapted on LEO satellite. Whereas for GEO satellite case, the transfer orbit shall be used due to the very high altitude and the satellite shall be stayed in the station keeping box which is permitted on the mission orbit. These phases are functions for AOCS mission. The aim of this paper is to introduce the AOCS hardware configuration for COMS (Communication, Ocean and Meteorological Satellite). The AOCS hardware of COMS consist of 3 Linear Analogue Sun Sensors (LIASS), 3 Bi-Axis Sun Sensors (BASS), 2 Infra-Red Earth Sensors (IRES), 3 Fiber Optical Gyroscopes (FOG), 5 momentum wheels and 14 thrusters. In this paper, each component is explained how to be used, how to locate and what relation between the AOCS algorithm and these components.

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아리랑 1호 임무기간 3년 동안의 궤도변화 분석 (An Analysis of the KOMPSAT-1 Operational Orbit Evolution Over 3 Years)

  • 김해동;최해진;김은규
    • 한국항공우주학회지
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    • 제31권10호
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    • pp.40-50
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    • 2003
  • 저고도, 태양동기궤도인 아리랑 1호의 최초 임무운영 목표였던 3년 동안 관측된 궤도 변화를 분석하였다. 초기운영기간 동안 최적화된 궤도를 획득하기 위해 총 4회의 궤도조정이 있었으며, 총 8회의 안전모드가 발생하였다. 예상치 않은 안전모드 발생과 임무기간 동안 최고조에 달했던 태양활동이 궤도변화에 미치는 영향을 분석하였고, 초기 궤도조정 완료 직후 임무운영 기간에 대해 예측되었던 장기 궤도예측 결과와 궤도결정을 통해 실측된 궤도와의 차이를 분석하였다. 최적화된 궤도에서부터 운영된 3년의 임무기간 동안 고도를 제외한 나머지 궤도요소들은 설계된 임무궤도 범위 내에서 변화하였고, 태양동기궤도 특성을 유지하였음을 확인하였다.

Launch and Early Orbit Phase Simulations by using the KOMPSAT Simulator

  • Lee, Sanguk;Park, Wan-Sik;Lee, Byoung-sun;Lee, Ho-Jin;Park, Hanjun
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 1999년도 제14차 학술회의논문집
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    • pp.33-36
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    • 1999
  • The KOMPSAT, which is scheduled to be launched by Taurus launch vehicle in late November of 1999, will be in a sun-synchronous orbit with an altitude of 685km, eccentricity of 0.001, inclination of 98deg and local time of ascending node of 10:50 a.m. Electronics and Telecommunications Research Institute and Daewoo Heavy Industry had jointly developed a KOMPSAT Simulator as a component of the KOMPSAT Mission Control Element. The MCE had been delivered to Korea Aerospace Research Institute for the KOMPSAT ground operation. It is being used for training of KOMPSAT ground station personnel. Each of satellite subsystems and space environment were mathematically modeled in the simulator. To verify the overall function of KOMPSAT simulator, a Launch and Early Orbit Phase(LEOP) operation simulations have been performed. The simulator had been verified through various tests such as functional level test, subsystem test, interface test, system test, and acceptance test. In this paper, simulation results for LEOP operations to verify flight software adapted into simulator, satellite subsystem models and environment models are presented.

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Measuring the Earth's Size Using the Sun's Altitude and The Responses

  • Chae, Dong-Hyun
    • 대한지구과학교육학회지
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    • 제5권1호
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    • pp.88-94
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    • 2012
  • This study was created to resolve the problems embedded in the formal measuring experiments to determine the earth's size in the current curriculum, to develop an updated measuring experiment to determine the earth's size and to establish its effect. For this study, pre-service elementary teachers, who had attempted the experiment of measuring the size of the earth when they were in middle school, performed the experiments in the existing national curriculum, and their responses, collected through in-depth interviews, were examined. To begin with, the pre-service elementary teachers conducted the experiment of measuring the earth size and they recorded the problems while performing it. At the end, an in-depth interview was administered. Based on the problems, an updated measuring experiment to determine the earth's size was suggested to be applied to the same contents and be analyzed through the in-depth interviews. Common themes which were mutually categorized and analyzed by the two researchers were obtained based on the records produced while conducting the experiment and the in-depth interview data. The teachers mentioned that the experiments for measuring the size of the earth in the current curriculum gave rise to difficulties in measuring precisely the angles between the string and the post. Also, there has been a scientific contradiction that solar altitudes were increased in a high latitude region, instead of decreased. For this reason, an alternative method has been developed to measure the earth's size using the distance and the solar altitude difference of two places. The teachers all agreed that by using the updated measuring experiment, they can acquire more precise measurements and it is easier, faster and consequently more effective than the existing methods. Through the results of this study, I suggest that the newly developed experiment by the researchers can overhaul the problems of the current experiments and it can be an effective alternative to the current experiment.

소백산맥 북부 지역 하천의 하각률 분포 (Incision Rate Distribution of Streams on the Northern Part of the Sobaek Mountain Range)

  • 이광률;박충선
    • 한국지형학회지
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    • 제27권3호
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    • pp.41-51
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    • 2020
  • This study tried to reveal incision rate distribution of streams on the northern part of the Sobaek Mountain Range with OSL age dating and geomorphic analysis, and factors influencing on the distribution were also discussed. With results from the previous studies, a total of 10 sites from 7 streams in the study area showed the rates ranging from 0.220 m/ka to 0.297 m/ka. Namhan-gang and Geum-cheon indicated the highest and lowest rates, respectively. Both sides in the northern section in the study area showed similar rates, while the western side in the middle section and the eastern side in the southern section showed higher rates than the other sides. Higher rates were also found from the eastern and northern sides where the Range runs N-S and E-W directions, respectively. Certain relationships with altitude and distance from the divide can be recognized from the rates and may be attributed to active incision with altitude and location of the uplift axis near the present divide. The rates on granite and sedimentary rock were higher than those on metamorphic rock, indicating that bedrock type is one of the important factors influencing on stream incision. Tectonic movement seemed to play some roles in the rates, because areas with lineaments showed lower rates. This study suggests that incision rate distribution of streams on the northern part of the Sobaek Mountain Range reflects various local geomorphic and geologic conditions.

Computation of geographic variables for air pollution prediction models in South Korea

  • Eum, Youngseob;Song, Insang;Kim, Hwan-Cheol;Leem, Jong-Han;Kim, Sun-Young
    • Environmental Analysis Health and Toxicology
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    • 제30권
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    • pp.10.1-10.14
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    • 2015
  • Recent cohort studies have relied on exposure prediction models to estimate individual-level air pollution concentrations because individual air pollution measurements are not available for cohort locations. For such prediction models, geographic variables related to pollution sources are important inputs. We demonstrated the computation process of geographic variables mostly recorded in 2010 at regulatory air pollution monitoring sites in South Korea. On the basis of previous studies, we finalized a list of 313 geographic variables related to air pollution sources in eight categories including traffic, demographic characteristics, land use, transportation facilities, physical geography, emissions, vegetation, and altitude. We then obtained data from different sources such as the Statistics Geographic Information Service and Korean Transport Database. After integrating all available data to a single database by matching coordinate systems and converting non-spatial data to spatial data, we computed geographic variables at 294 regulatory monitoring sites in South Korea. The data integration and variable computation were performed by using ArcGIS version 10.2 (ESRI Inc., Redlands, CA, USA). For traffic, we computed the distances to the nearest roads and the sums of road lengths within different sizes of circular buffers. In addition, we calculated the numbers of residents, households, housing buildings, companies, and employees within the buffers. The percentages of areas for different types of land use compared to total areas were calculated within the buffers. For transportation facilities and physical geography, we computed the distances to the closest public transportation depots and the boundary lines. The vegetation index and altitude were estimated at a given location by using satellite data. The summary statistics of geographic variables in Seoul across monitoring sites showed different patterns between urban background and urban roadside sites. This study provided practical knowledge on the computation process of geographic variables in South Korea, which will improve air pollution prediction models and contribute to subsequent health analyses.

실시간 영상 기반 산불 추적 및 매핑기법 개발 (Development of a Forest Fire Tracking and GIS Mapping Base on Live Streaming)

  • 조인제;김규범;박범순
    • 융합정보논문지
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    • 제10권10호
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    • pp.123-127
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    • 2020
  • 야간 중대형 산불의 전체적인 화선정보를 얻기 위하여 누락되는 산불에 대한 반복적인 임무비행과 임무수행 종료 후 획득되는 정사영상 정합에 대한 소요시간을 줄이기 위하여 실시간 동영상으로 산불발생 여부를 판단하고 드론의 위치와 영상카메라의 각도정보, 지도상의 고도정보를 활용하여 판단된 산불위치를 계산하여 지도에 도시할 수 있는 지상통제시스템을 개발하였다. 개발된 기능의 신뢰성을 검증하기 위하여 비행고도 별, 영상카메라의 지향하는 위치정보의 오차거리를 측정하였으며, 신뢰할 수 있는 범위내의 위치정보를 지도에 표시하였다. 본 논문에 개발된 기능으로 다수의 산불 발생위치를 실시간 식별이 가능하므로 산불 진화대책 수립을 위한 전체적인 화선정보를 보다 신속하게 획득할 수 있을 것으로 예상된다.

Modeling of Space Radiation Exposure Estimation Program for Pilots, Crew and Passengers on Commercial Flights

  • Hwang, Junga;Dokgo, Kyunghwan;Choi, Enjin;Park, Jong-Sun;Kim, Kyung-Chan;Kim, Hang-Pyo
    • Journal of Astronomy and Space Sciences
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    • 제31권1호
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    • pp.25-31
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    • 2014
  • There has been a rapid increase of the concern on the space radiation effect on pilots, crew and passengers at the commercial aircraft altitude (~ 10 km) recently. It is because domestic airline companies, Korean Air and Asiana Airlines have just begun operating the polar routes over the North Pole since 2006 and 2009 respectively. CARI-6 and CARI-6M are commonly used space radiation estimation programs which are provided officially by the U.S. federal aviation administration (FAA). In this paper, the route doses and the annual radiation doses for Korean pilots and cabin crew were estimated by using CARI-6M based on 2012 flight records. Also the modeling concept was developed for our own space radiation estimation program which is composed of GEANT4 and NRLMSIS00 models. The GEANT4 model is used to trace the incident particle transports in the atmosphere and the NRLMSIS00 model is used to get the background atmospheric densities of various neutral atoms at the aircraft altitude. Also presented are the results of simple integration tests of those models and the plan to include the space weather variations through the solar proton event (SPE) prediction model such as UMASEP and the galactic cosmic ray (GCR) prediction model such as Badhwar-O'Neill 2010.

추력 1000 kgf급 하이브리드 로켓(KHyRoc-II)의 개발 (Development of Hybrid Rocket(KHyRoc-II) with 1000 kgf Thrust level)

  • 문근환;오지성;이선재;최원준;김학철;이정표;문희장;성홍계;김진곤
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2012년도 제38회 춘계학술대회논문집
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    • pp.58-62
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    • 2012
  • 본 연구에서는 추력 1000 kgf 급 하이브리드 로켓 (KHyRoc-I)의 지상 연소 실험을 수행하였다. 지상 연소 실험 결과 약 700 kgf의 추력을 획득하였으며, 비행 궤적 계산 결과 최대 고도 12.5 km로 계산 되었다. 그리고 KHyRoc-I의 큰 L/D비(28)로 인한 구조 안전성의 문제점을 보완하기 위해, 직경 250 mm의 알루미늄 seamless tube를 사용하여 L/D비가 작은(18.3) KHyRoc-II를 재설계하였다. 내탄도 해석을 통하여 추력 900 kgf 하이브리드 로켓 엔진을 설계하였으며, 비행 궤적 계산 결과 최대 고도는 약 7.4 km로 계산되었다.

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고고도 장기체공 무인기와 의사위성/트랜시버를 활용한 국지적 대체항법에 관한 연구 (Regional Alternative Navigation Using HALE UAV, Pseudolite & Transceiver)

  • 최민우;유선경;김오종;기창돈;박병운;서승우;박준표
    • 한국항행학회논문지
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    • 제19권6호
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    • pp.499-506
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    • 2015
  • GNSS (global navigation satellite systems)은 민 군 차원에서 매우 다양한 분야에 활용되고 있다. 그러나 GNSS 신호는 재밍에 상당히 취약해 쉽게 방해 받을 가능성이 상존하기에 GNSS을 사용 불가능할 시에도 일정 수준의 항법성능을 보장하여 주는 일련의 백업 또는 대체항법 시스템이 필요하다. 본 논문에서는 의사위성 또는 트랜시버를 장착한 고고도 장기체공 무인기(HALE UAV; high altitude long endurance unmanned aerial vehicle)의 개념을 도입하여 국지적인 지역에서 백업 또는 대체항법 시스템을 제안하고자 하였다. 제안된 대체항법 시스템을 기반으로 고고도 장기체공 무인기의 위치 오차를 추정하고, 이를 바탕으로 최종적인 사용자 위치정확도를 산출하여 본 연구에서의 국지적 대체항법의 성능을 나타내었다.