• The Bulletin of The Korean Astronomical Society
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• v.37 no.2
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• pp.198.1-198.1
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• 2012

저궤도 위성이 발사체에서 분리된 후 탑재 소프트웨어에 의한 초기 동작이 수행되고 나면 초기 운용이 시작된다. 초기 운용 기간에 수행할 모든 절차와 대처 가능한 긴급 상황이 발생할 경우 수행할 절차는 발사 전에 미리 준비된다. 위성의 각 부분의 설계 마진은 최악 조건을 기준으로 반영되어 있기 때문에 발사 이후의 버스 시스템 관점에서의 위성 특성은 요구 사항을 만족하는 범위가 될 것으로 예상이 가능하다. 실제로 발사 후 위성 텔레메트리 분석을 통해 대부분의 항목에서 요구 조건을 만족하는 것으로 확인되었다. 또한 텔레메트리 분석을 통해 설계 단계에서 예상했던 것 보다 정확한 궤도 특성이 반영된 위성 특성을 파악하였다. 이러한 특성은 설계 시 고려했던 상황과 다르더라도 실제 궤도 특성이 반영된 특성이므로 초기 운용 및 정상 운용 시에 정상적인 상황인 것으로 고려해야 한다. 첫째, 지구 알베도 특성에 따라 태양센서 값이 궤도에 따라 변화한다. 위성의 자세가 정확히 태양을 지향하고 있더라도 태양센서에 지구에서 반사된 빛이 입사되어 자세 제어에 영향을 주게 된다. 알베도의 영향은 적도에서 극지방으로 갈수록 커지며, 계절에 따라 다른 특성을 보인다. 알베도의 영향을 최소화하기 위해 자세 제어 모델에 알베도 효과를 고려하거나 알베도 효과를 무시할 수 있을 정도로 자세 제어 오차 한계를 조정할 수 있다. 둘째, 위성의 지구 회피 회전에 의해 태양 전지판의 온도가 궤도에 따라 변화한다. 위성체는 위성체에 장착된 두 개의 별센서의 가시성 확보를 위해 태양 지향 자세에서 요축으로 일정 속도로 회전한다. 남극 부근에서는 두 태양 센서가 모두 지구의 반대편인 남쪽을 지향하도록 하며, 북극 부근에서는 북쪽을 지향하도록 한다. 이 때 두 태양 센서의 방향에 장착된 태양 전지판은 극지방에서 지구 반대편에 위치하므로 다른 태양 전지판에 비해 낮은 온도를 갖게 된다. 이 논문에서는 위성의 궤도 특성에 따른 고려 사항에 대해 설명하였다.

• Journal of the Korean earth science society
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• v.42 no.1
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• pp.118-131
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• 2021

The purpose of this study was to investigate the characteristics of evidence-based reasoning practiced by middle school gifted students. Data were collected through an online task in which middle school students in gifted education institutes of a university located in the metropolitan area, Korea, performed inquiry about the shape of a planet's orbit. The students were given data of Mercury's greatest elongations and asked to draw the planet's orbit with the data. Each of the students was also asked to provide his or her hypothesis of Mercury's orbit before the drawing and to reason about the orbit again using his or her own drawing as evidence. The content analysis of the students' reports revealed 5 different types of judgement about the shape of Mercury's orbit, 4 types of reasoning about the hypothesis and evidence, and the characteristics of evidence-based reasoning within the judgement types. Based upon the analysis results, the importance of proper interpretations of evidence in evidence-based reasoning, the core role of the theory-evidence coordination, and the usefulness of working with multiple hypotheses were discussed. In addition, implications for earth science education were suggested.

• Korean Journal of Remote Sensing
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• v.15 no.2
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• pp.119-130
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• 1999

At present, many ground stations all over the world are using NORAD orbit element data in order to track and communicate with Earth orbiting satellites. The North American Aerospace Defense Command (NORAD) observes thousands of Earth orbiting objects on daily basis and provides their orbital information via internet. The orbital data provided by NORAD, which is also called two line element (TLE) sets, allows ground stations to predict the time-varying positions of satellites accurately enough to communicate with the satellites. In order to complete the mission of a high resolution remote sensing satellite which requires very high positional determination and control accuracy, however, a mission control and tracking ground station is dedicated for the observation and positional determination of the satellite rather than using NORAD orbital sets. In the case of KITSAT-3, NORAD orbital elements are currently used for image acquisition planning and for the processing of acquired images due to the absence of a dedicated KITSAT-3 tracking ground system. In this paper, we tested and analyzed the accuracy of NORAD orbital elements and the appropriate prediction model to determine how accurately a satellite acquisites an image of the location of interest and how accurately a ground processing system can generate the catalog of the images.

• The Journal of the Convergence on Culture Technology
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• v.9 no.3
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• pp.633-640
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• 2023

In this study, numerical analysis was performed based on field investigation to derive an appropriate reinforcement method by analyzing the displacement behavior characteristics of concrete blocks generated in the direct fixation track on the bridges of the serviced light rail transit. The track of this study was a direct fixation track on a sharp curved track, and the problem of movement of the concrete blocks installed on the bridge deck in the longitudinal and lateral directions occurred. In this study, based on the finite element model using 3D solid elements, the behavior of the direct fixation track that could be occurred under operating load conditions was analyzed. In addition, the reinforcement effect of various reinforcement methods was analyzed. As a result of analyzing the lateral displacement before and after reinforcement, it was analyzed that the maximum lateral displacement after reinforcement under the extreme lateral wheel loads significantly decreased to about 3% (about 0.1mm) compared to before reinforcement. In addition, as a result of examining the generated stress of the filling mortar, bridge decks, and reinforcing bar, it was analyzed that all of them secured a sufficient safety factor of 2.6 or higher, and the optimal conditions for the reinforcement method were derived. Therefore, it is judged that the number of anchoring reinforcements and symmetrical anchor placement reviewed in this study will be effective in controlling the occurrence of lateral displacement of concrete blocks and securing the structural integrity of bridges and concrete blocks.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.48 no.10
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• pp.791-799
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• 2020

Launched in October 2019, Northrop Grumman's MEV-1 was the world's first unmanned mission demonstrating the practical feasibility of on-orbit servicing. Although the concept of on-orbit servicing was proposed several decades ago, it has been developed to various mission concepts providing services such as orbit change, station keeping, propellant and equipment supply, upgrade, repair, on-orbit assembly and production, and space debris removal. The historical success of MEV-1 is expected to expand the market of on-orbit servicing for government agencies and commercial sectors worldwide. The on-orbit servicing essentially requires the utilization of a highly propellant efficient electric propulsion system due to the nature of the mission. In this study, the space mission analysis for a simple on-orbit mission involving Hall thruster is conducted, which is life extension mission for geostationary orbit satellites. In order to analyze the mission, design space exploration for various Hall thruster design variable combinations is performed. The values of design variables and operational parameters of Hall thruster suitable for the mission are proposed through design space analysis and optimization, and mission performance is derived. In addition, the direction of further improvement for the current on-orbit mission analysis process and space mission analysis involving Hall thruster is reviewed.

• The Science & Technology
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• v.31 no.2 s.345
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• pp.33-35
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• 1998

6천만년 전부터 지구의 기온이 냉각한 것은 대기 속의 이산화탄소가 줄어들었기 때문이라는 데는 대부분의 과학자들의 의견이 일치한다. 무슨 이유로 이산화탄소의 수준이 떨어졌느냐에는 해석이 다양하다. 2백50만년 전부터 유럽과 북미 지역에서 시작된 국지적인 빙하의 원인은 지구의 궤도가 천천히 바뀌면서 햇빛의 패턴에 변화가 생겼기 때문이라는 「밀란코비치 모델」이 널리 받아들여지고 있다. 그러나 빙하시대의 기상데이터를 정확히 알 수 없기 때문에 빙하시대를 일으킨 원인에 대한 해답을 얻을 수 엇다는 비관론도 있다.

• Journal of Aerospace System Engineering
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• v.15 no.5
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• pp.89-97
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• 2021

STEP Cube Lab-II (Cube Laboratory for Space Technology Experimental Project-II) is a 6U Cube satellite equipped with optical and infrared cameras for monitoring Mt. Paektu volcanic eruption signs and earth observation in the Korean peninsula. To guarantee successful mission operation of the cube satellite in orbit, thermal design is essential for the electronic equipment, and must be kept within the allowable temperature range during the mission period. Thus, it is necessary to analyze the predictable orbital thermal environment. The STEP Cube Lab-II is launched through the KSLV-II, however, the operation orbit has not been determined due to the unknown launch time. In this study, we performed a thermal analysis of the satellite and investigated the heat flux according to launch time to analyze the worst orbital conditions that could occur.

• 전기의세계
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• v.13 no.1
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• pp.16-19
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• 1964

한강대교의 전식상황을 예비조사한 결과 철교상에 가설된 전차궤도의 누설전류로 인하여 한강대교가 전식당하고 있음을 발견하였다. 그리하여 금반 건설부와 서울특별시 건설국의 예산으로 본 전력연구소 전식연구실에서 전식작용의 실태를 본격적으로 조사하여 교량의 유지관리를 합리화 시키고자 본 조사를 착수하여든 것이다. 전식에 대한 개요는 본 학회지 제 12집에서 양론하였으므로 본 논문에서는 생략하기로 한다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.41 no.12
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• pp.950-958
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• 2013

The Lunar orbiter is expected to be inserted into a ~300km low Earth orbit using Korea Space Launch Vehicle-II(KSLV-II). After the states are successfully determined with obtained tracking data, the Trans Lunar Injection(TLI) burn has to be done at appropriate epoch to send the lunar orbiter to the Moon. In this study, we describe in detail the mission scenario of the Korean lunar orbiter from the launch at NARO Space Center to lunar orbit insertion(LOI) stage following direct transfer trajectory. We investigate the launch window including launch azimuth, delta-V profile according to TLI and LOI burn positions. We also depict the visibility conditions of ground stations and solar eclipse duration to understand the characteristics of the direct transfer trajectory. This paper can be also helpful not only for overall understanding of ${\Delta}V$ trend by changing TOF and coasting time but for selecting launch epoch and control parameters to decrease fuel consumption.

• Korean Journal of Remote Sensing
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• v.38 no.6_1
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• pp.1069-1080
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• 2022

The tropospheric ozone is a pollutant that causes a great deal of damage to humans and ecosystems worldwide. In the event that ozone moves downwind from its source, a localized problem becomes a regional and global problem. To enhance ozone monitoring efficiency, geostationary satellites with continuous diurnal observations have been developed. The objective of this study is to derive the Tropospheric Ozone Movement Vector (TOMV) by employing continuous observations of tropospheric ozone from geostationary satellites for the first time in the world. In the absence of Geostationary Environmental Monitoring Satellite (GEMS) tropospheric ozone observation data, the GEOS-Chem model calculated values were used as synthetic data. Comparing TOMV with GEOS-Chem, the TOMV algorithm overestimated wind speed, but it correctly calculated wind direction represented by pollution movement. The ozone influx can also be calculated using the calculated ozone movement speed and direction multiplied by the observed ozone concentration. As an alternative to a backward trajectory method, this approach will provide better forecasting and analysis by monitoring tropospheric ozone inflow characteristics on a continuous basis. However, if the boundary of the ozone distribution is unclear, motion detection may not be accurate. In spite of this, the TOMV method may prove useful for monitoring and forecasting pollution based on geostationary environmental satellites in the future.