• 한국한의학연구원논문집
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• 제11권2호
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• pp.23-33
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• 2005

Four Properties and five Flavors of Drugs is interpreted by adaptation of human body to the environmental theory(天人相應). The Structural model of the body is compared with sky, earth, sun and moon (天, 地, 日, 月). The natural changes of the four seasons give rise to that of Four Properties and five Flavors of Drugs. On equal terms it is happened in our body. On this study we can draw an analogy between sky, earth, sun & moon (天, 地, 日, 月) and the body. The six bu(六腑) is related to the earth, the five ju(五主) to the sky, the five jang(五臟) to the sun, the meridians system (經絡) to the moon. When spring, the air is warm, the water element of the earth is ascending, and the earth gives birth to the sour flavor. Like this, the water element is absorbed by six bu and then is ascended to the meridian system. When summer, the air is hot and the water element of the earth is floated, the earth make the bitter flavor. In the same way, the six bu absorbed the hot air from the five ju and the water element is quickly absorbed by six bu and then the water element is ascended to the meridian system. When rainy season (長夏), the earth creates the sweet flavor The sweet flavor give warmer energy to the five jang and the six bu. When autumn, the earth change the sweet flavor into pungent. The earth gives warmer energy to the sky, because of cool weather According to same process, the pungent flavor give warmer energy to the five jang and the six bu, and the meridian system gets back the water element from the five ju. When winter, the air is cold and the water element of the earth is hidden. The sky and the earth are not interchangeable. At that time, the earth produce the salty flavor and the water element is keeping in the meridian system.

• 대한자원환경지질학회:학술대회논문집
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• 대한자원환경지질학회 2007년도 춘계 지질과학기술 공동학술대회
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• pp.127-129
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• 2007

See Full Text

• International Journal of Aeronautical and Space Sciences
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• 제15권3호
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• pp.267-280
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• 2014

A spacecraft placed in an Earth-Moon L2 quasi-halo orbit can maintain constant communication between the Earth and the far side of the Moon. This quasi-halo orbit could be used to establish a lunar space station and serve as a gateway to explore the solar system. For a mission in an Earth-Moon L2 quasi-halo orbit, a spacecraft would have to be transferred from the Earth to the vicinity of the Earth-Moon L2 point, then inserted into the Earth-Moon L2 quasi-halo orbit. Unlike the near Earth case, this orbit is essentially very unstable due to mutually perturbing gravitational attractions by the Earth, the Moon and the Sun. In this paper, an insertion maneuver of a spacecraft into an Earth-Moon L2 quasi-halo orbit was investigated using the global optimization algorithm, including simulated annealing, genetic algorithm and pattern search method with collision avoidance taken into consideration. The result shows that the spacecraft can maintain its own position in the Earth-Moon L2 quasi-halo orbit and avoid collisions with threatening objects.

• Journal of Astronomy and Space Sciences
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• 제16권1호
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• pp.69-78
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• 1999

인공위성의 임무분석기술 중 하나로 인공위성의 센서가 실제의 궤도상에서 감지하는 것과 거의 같은 자료를 생성하는 자세감지(attitude sensing) S/W 시스템을 개발하였다. 이 S/W 시스템은 두 개의 모듈로 구성되어 있는데, 하나의 천체력 서비스 (ephemeris service) 모듈로 4개 행성(금성, 화성, 목성, 토성)의 섭동향을 고려하여 태양과 달의 위치를 구하고 4 $\times$4 지구중력 포텐셜항을 고려하여 위성의 위치를 계산하여 준다. 또 하나는 자세감지 모듈로 위성체의 자세요소($alpha,delta$)와 태양, 지구, 달의 위치로부터 위성의 자전축에 대한 각 천제들의 시선고도각(look angle)과 이면각(digedral angle)을 산출한다. 개발된 S/W 시스템으로 무궁화 위성의 자전축과 궤도요소를 변화시키면서 모의실험한 결과를 논의하였다.

• Journal of Astronomy and Space Sciences
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• 제5권2호
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• pp.129-141
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• 1988

제한 3체 문제의 수치해를 이용하여 태양-목성계와 지구-달계의 $L_5$점 근처에서 각각 490여개, 1,600여개의 주기 궤도를 구하였다. 태양-목성계의 경우에서는 주기의 증가에 따라 에너지와 주기 궤도 크기가 단조롭게 커졌다. 그러나 지구-달계에서의 주기 궤도 모양은 복잡하고 변곡점이 나타나며 서로 겹치는 경우도 있다. 또한, 지구-달계에서 단일주기에 3개의 에너지가 동시 대응하는 영역이 존재하며 이 영역에소는 주기와 에너지가 반비례하는 구역이 있다. 태양-목성계의 $L_5$ 점 근처에서 목성의 중력 섭동 외의 기타의 작은 섭동에 의해 불안정한 주기 궤도가 될 수 있는 영역이 존재 가능하다. 이 영역 중 $L_5$점(5.2AU)에 가장 가까운 지역들이 a~5.12AU와 a~5.29AU 근처인데, 이 곳에는 이심률과 궤도 경사각이 작은 Trojan 소행성들이 존재하기 어렵다고 할 수 있다.

• Journal of Astronomy and Space Sciences
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• 제12권1호
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• pp.78-89
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• 1995

상대론올 포함한 행성의 운동방정식을 중심으로 9개의 행성과 달, 그리고 4개의 소행성을 포함한 태양계의 n체 문제를 다루었다. 이 기본방정식에 지구와 달의 figure potential과 지구의 solid tidal effect를 외력으로 하는 섭동방정식을 추가하였다. 지구의 orientation을 J2000.0을 기준으로 하는 세차와 장동에 관한 식을 채택하였고, 달의 orientation에 대해 서는 J2000.0을 기준으로 하는 달의 칭동 모델을 션택하고 Eckert의 행성섭동효과를 추가 하였다. 각각의 subroutine별로 테스트를 거쳐 이들을 결합하여‘SSEG (Solar System Ephemerides Generator)’ 라는 소프트웨어 package를 개발한 후, CRAY-2S 슈퍼컴퓨터를 사용하여 프로그램을 수행하였다. 기준 시각인 JD2440400.5를 기준으로 하여, 1일 간격으로 40,000일 (약 110년) 동안 각 행성의 위치 (태양중심 황도직교좌표값)를 계산한 후, 이 결과의 정확도를 검증하기 위하여 JPL의 DE200 자료와 우리의 결과를 비교하였다. 이 연구로부터 얻은 결과로서 행성들의 위치 성분에 대한 최대오차가 100년 동안 $\pm2\times10^{-8}AU(약\pm3km)$ 이하로 나타났다

• 동국한의학연구소논문집
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• 제5권
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• pp.281-306
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• 1996

A study on the effect of the Sun-Moon-Stars(日月星辰) in Huang Ti Nei Ching("黃帝內經") on the formation of the Yunqi theory(運氣理論) have revealed following conclusions. 1. There was a record of Stars(星辰) written by Gabgol-Character(甲骨文字) in the Yin(殷) Dynasty. But the very first documentary records of Stars(星辰) is Shu Jing("書經"). Ancient astronomy had the tendency of astrology of combined with theory of the Five Elements(五行) and finally effects the theory of formation of Huang Ti Nei Ching("黃帝內經"). 2. Shu Jing("書經") said that Junrak(錢樂) made an Armillary sphere(運天儀) in the Sung(宋) Dynasty. And in the Jin(秦) and the Han(漢) Dynasty, they already observed the stars. The Sunkiokhyung(璿機玉衡) which is machinery of star-observing, became to be called an Armillary sphere (運天儀) by the pass of times. 3. As of the theory of the Cosmos-structure(宇宙-構造論) in Ohanunhangdaeron("五運行大論"), Guiyugu(鬼兒區) announced the Hypothesis of Covering Heaven(蓋天說) but Kibak(岐伯) supported the Hypothesis of chaosheven's(蓋天說) and in the theory of atmosphere(大氣論) in Ohanunhangdaeron("五運行大論") said that the earth was in Great Empty(太虛) and it was floating in the universe by the Great Chi(大氣). 4. The knowledge about the Five stars(五星) in Huang Ti Nei Ching("黃帝內經") is presented in the section of Gemgwejineonron("金?眞言論"), Gigoupyondaeron("氣交變大論"), Youkwonjeonggidaeron("六元正紀大論").ln the method of identifying the Five stars(五星) presented the criteria of the brightness, the altitude, the colours and the orbit etc. 5. The jupiter which has twelve year's revolution cycle was the basis of determination on the Twelve constellation(12辰), the Twelve field of heaven(12次), the Twelve Houses in the ecliptic(黃道 12宮), the Twelve Earth's Branches(12支) and the Twelve fields of Earth(12分野) and also it became the origin of the duodecimals(12進法). 6. The saturn having about twenty-eight year's revolution cycle became the criterion in identifying the Twenty Eight Constellations(28宿) which was used as the coordinates of the Celestial sphere (天球). 7. By the Percussional movement(歲差運動), the position of polaris and the Vernal-Antumal equinox(春秋分点) were shifted. Therefore the ancient the Heaven Gate-Earth Door(天門-地戶) changed from the position of Sil-Byuk(室壁), Yik-Jin(翼軫). And the precisional movements brought about the concept of the WunHoyYunSe(元會運世) that is a method of dividing a period. Also the precisional movement gave three dimension(三次元) foundation interpreted the Sixty JiaZi (六十甲子) which is revolving through sixty years uniformally. 8. The Hypothesis of the Nine Houses and Eight Winds(九宮八風論) which is one field of the astrology of ancient polaris-nine Houses divination plate(太一九宮占盤) brought about the concept of deficiency and excess and the concept of the Wind Vice(風邪). In the Calendar System(曆法) presented in Huang Ti Nei Ching("黃帝內經") the tropical year of the Sun-Moon-Stars(日月星辰) and the revolution and the rotation of the earth give explanations the changes of Yin-Yang(陰陽) by the use of the ten Celestial branches(十干) and the twelve Earth branches(十二支).

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 1991년도 한국자동제어학술회의논문집(국내학술편); KOEX, Seoul; 22-24 Oct. 1991
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• pp.425-430
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• 1991

For satellite orbit determination, a satellite (K-3H) which is affected by the earth's gravitational field and the earth's atmospheric drag, the sun, and the moon is chosen as a dynamic model. The state vector include orbit parameters, uncertain parameters associated with perturbations and tracking stations. These perturbations include gravitational constant, atmospheric drag, and jonal harmonics due to the earth nonsphericity. Early orbit was obtained with given the predicted orbital parameter of the satellite. And orbit determination, which is applied to Extended Kalman Filter(EKF) for real time implementation , use the observation data which is given by satellite tracking radar system and then orbit estimation is accomplished. As a result, extended sequential estimation algorithm has a fast convergence and also indicate effectiveness for real time operation.

• 한국경영과학회:학술대회논문집
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• 한국경영과학회/대한산업공학회 2003년도 춘계공동학술대회
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• pp.704-707
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• 2003

The Purpose of carrier tracking and tracing is to achieve more information over shipments via carrying in mobile business .At multimodes, especially consignor wants to be aware of the exact situation and position of goods. As an innovate business model, we present CGPS(Carrier Global Positioning System) scheme usiug LEO(Low Earth Orbital) satellite. The LEO collects the data periodically and sends to the web server, and eventually customer's PC or PDA. This provides shipping company or freight forwarder with more robust information such as door status, container inside condition, etc.

• Journal of Astronomy and Space Sciences
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• 제8권2호
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• pp.141-148
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• 1991

In order to obtain a complete picture of the time dependent dynamic of 360 fragments in space, the program IODS (ISSA Orbit Determination System) has been set up. Using The program IODS, all fragments orbits of one break-up event can be generated. Perturbations due to the Earth's asymmetrical potential, the Sun, moon, air drag and solar radiation force are considered. We summarize our results as follows : I) Due to J2 term, precessional motion of all fragment orbits are (수식생략) ii) The other perturbations have very small effects.