• 제목/요약/키워드: precession

검색결과 103건 처리시간 0.024초

수치모델을 이용한 홀로세 중기의 아시아 몬순순환 변화 연구 (Numerical Simulation of the Asian Monsoon for the Mid-Holocene Using a Numerical Model)

  • 김성중;이방용;박유민;석봉출
    • Ocean and Polar Research
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    • 제27권3호
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    • pp.289-297
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    • 2005
  • The change in global climate and Asian monsoon patterns during the mid-Holocene, 6000 years before present (6 ka), is simulated by a climate model at spectral truncations of T170 with 18 vertical layers, corresponding to grid-cell sizes of roughly 75km. The present simulation is forced with the observed monthly data of sea surface temperatures, and the specified concentration of atmospheric carbon dioxide, while in the mid-Holocene experiment, orbital parameters such as obliquity, precession, and eccentricity are changed to the 6ka conditions. Under such conditions, the precipitation associated with the summer monsoon is enhanced over a wider zonal band from the Middle East to Southeast Asia, while no significant alteration takes Place in winter. The monsoonal wind also increases over the Arabian Sea, showing the enhanced southwesterly wind during summer and northeasterly wind during winter. Overall, the showing of the Asian monsoon is enhanced during the mid-Holocene, especially in summer, which is consistent with the proxy estimates and other previous model simulations.

유도탄 성능분석을 위한 실시간 병렬처리 시뮬레이터 연구 (Study on Real-time Parallel Processing Simulator for Performance Analysis of Missiles)

  • 김병문;정순기
    • 제어로봇시스템학회논문지
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    • 제11권1호
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    • pp.84-91
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    • 2005
  • In this paper, we describe the real-time parallel processing simulator developed for the use of performance analysis of rolling missiles. The real-time parallel processing simulator developed here consists of seeker emulator generating infrared image signal on aircraft, real-time computer, host computer, system unit, and actual equipments such as auto-pilot processor and seeker processor. Software is developed from mathematic models, 6 degree-of-freedom module, aerodynamic module which are resided in real-time computer, and graphic user interface program resided in host computer. The real-time computer consists of six TIC-40 processors connected in parallel. The seeker emulator is designed by using analog circuits coupled with mechanical equipments. The system unit provides interface function to match impedance between the components and processes very small electrical signals. Also real launch unit of missiles is interfaced to simulator through system unit. In order to apply the real-time parallel processing simulator to performance analysis equipment of rolling missiles it is essential to perform the performance verification test of simulator.

유한회전과 4원수를 이용한 유니버설 조인트 시스템의 기구해석 비교 (Comparisons of Kinematical Analysis for the Universal-joint System by Using Finite Rotations and Quaternions)

  • 윤성호
    • 한국전산구조공학회논문집
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    • 제23권2호
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    • pp.183-189
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    • 2010
  • 본 논문에서는 자동차의 구동계 등에 사용되는 유니버설 조인트의 기구학적 거동을 관찰하기 위하여 오일러 각과 4원수(quaternion)를 적용한 두 가지 방법을 비교하였다. 이와 관련된 종래의 연구자들은 오일러 각을 사용하여 회전체의 동적인 거동을 해석하였으나 결과의 일관성과 정확도가 부족하였다. 유니버설 조인트 시스템 해석에서도 이러한 단점을 확인하였고 이를 극복하고자 4원수를 적용하였다. 구동시 원동축 1개축 회전과 원동축과 직각방향 회전축 2개의 축이 동시에 존재하는 경우에 대하여 수치해석을 통하여 기하학적인 물리량을 산출하였다. 4원수를 채용한 방법이 세차운동을 포함하는 2개축 회전에서 유니버설 조인트 시스템을 해석하는데 있어 더욱 유용한 방법임을 보여 주었다.

Performance Evaluation of a Rapid Three Dimensional Diffusion MRI

  • Numano, Tomokazu;Homma, Kazuhiro;Nishimura, Katsuyuki
    • 한국의학물리학회:학술대회논문집
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    • 한국의학물리학회 2002년도 Proceedings
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    • pp.356-358
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    • 2002
  • MRI, particularly diffusion weighted imaging (DWI), plays vital roles in detection of the acute brain infarction$\^$1-4/ and others metabolic changes of biological tissues. In general, every molecule in biological tissues may diffuse and move randomly in three-dimensional space. However, in clinical diagnosis, only 2D-DWI is used. The authors have developed a new method for rapid three-dimensional DWI (3D-DWI). In this method, by refocusing of the magnetized spin with the applied gradient field, direction of which is opposite to phase encoding field. Magnetized spin of $^1$H is kept under the SSFP (steady state free precession)$\^$5-6/. Under SSFP, in addition of FID, spin echo and stimulated echo are also generated, so the acquired signal is increased. The signal intensity is increased depending on flip angle (FA) of magnetized spin. This phenomenon is confirmed by human brain and phantom studies. The performance of this method is quantitatively analyzed by using both of conventional spin echo DWI and 3D-DWI. From experimental results, three dimensional diffusion weighted images are obtained correctly for liquid phantoms (water, acetone and oil), diffusion coefficient is enhanced in each image. Therefore, this method will provide useful information for clinical diagnosis.

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Spin 안정형 구형 로켓트에 관한 이론 및 실험적 연구 (Theoretical and Experimental Study on a Spin-Stabilized Spherical Rocket)

  • 이종훈
    • 한국국방경영분석학회지
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    • 제3권1호
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    • pp.83-96
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    • 1977
  • The combustion chamber and nozzle of an end burning, small spherical rocket is designed. A spherical external shape has a number of advantages such as fixed center-of-gravity and minimum aerodynamic precession torques during flight and a better mass distribution for gyro-stabilization as contrasted to a conventional ogive rocket shape. It is shown that the cross-sectional variation of the end burning solid propellant with length is an exponential geometry to provide a constant thrust-weight ratio of the rocket device during the propellant burning period, and that the factors which affect the attainment of the constant relationship of thrust to weight in the design are the initial propellant area, initial weight of the rocket and propellant density. The measurement of the transient thrust in the ground static test using black powder propellant supports the predicted results. A wind tunnel having a $30{\times}30{\times}75cm$ test section and Mach number 0.11 is constructed, and a simple balance-type device is designed for the measurement of the drag of a spinning sphere. The experimental results indicate that the. spinning has no effect on the magnitude of the drag up to the Reynolds number $3{\times}10^5$. Numerical computation of the flight trajectories for various launching angles is presented, and the gyro-stabilization of spinning sphere is discussed.

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3-블레이드 회전익 항공기에서 기하학적 정밀 보의 공탄성 모델을 이용한 무베어링 로터의 자이로스코픽 세차 진동 제어

  • 임병욱;김용세;신상준
    • EDISON SW 활용 경진대회 논문집
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    • 제6회(2017년)
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    • pp.270-281
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    • 2017
  • 본 논문에서는 헬리콥터 블레이드에서 발생하는 자이로스코픽 세차 진동에 대해 연구하고, 능동 제어기 설계를 통하여 진동 저감 시뮬레이션을 수행한다. 이를 위해, 헬리콥터의 전진 비행시 동역학적 응답을 외팔보 조건을 갖는 회전익의 해석이 가능한 EDISON의 기하학적 정밀 보 구조동역학 프로그램을 이용하여 구조 해석을 진행하고 이를 단순 공기력 모델과 연성하여 공탄성 해석을 수행하였다. 실시간 구조 응답을 구하기 위해 EDISON 프로그램 해석 결과를 비선형 수식으로 모델링하는 기법과 트림해석에는 Newton-Raphson 기법 등이 사용되었다.

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대전지자기관측소에서 측정된 지자기 값과 시간에 따른 변화 (Geomagnetism measured in DZN (Daejeon) Geomagnetic Observatory and its time-variation)

  • 임무택;박영수;임형래;구성본;이영철;나재신
    • 한국지구물리탐사학회:학술대회논문집
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    • 한국지구물리탐사학회 2007년도 공동학술대회 논문집
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    • pp.353-360
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    • 2007
  • KIGAM has installed a FLARE+ continuous geomagnetic observation system in 1998 in Daejeon of which the IAGA identification code is DZN. The coordinates of the absolute measurement plinth precisely determined by the PDGPS(Post-Processing Differential Global Positioning System) is (127-21-37.19E, 36-22-43.96N, 45.93 m) in WGS84 for the horizontal and from the geoid surface for the vertical. Periodically we have conducted the absolute geomagnetic measurement on the plinth above. We have processed the continuous time-variation 3-axis geomagnetic data measured on arbitrary sensors' coordinates in the observatory and absolute geomagnetic data together to get as the results the time-variation H(orizontal), D(eclination), Z(vertical down), F(scalar calculated from 3 components) and P(Proton Precession Magnetometer Data). We have compared our own data with those calculated from the 10th generation IGRF(International Geomagnetic Reference Field). All the measured data in the DZN Observatory can be acquired through the website http://geomag.kigam.re.kr.

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남북 천문분야 협력방안 기초 연구 II : 남북한 천문역서 비교 (A STUDY OF COOPERATION BETWEEN SOUTH AND NORTH KOREA IN THE FIELD OF ASTRONOMY II : ASTRONOMICAL ALMANAC)

  • 양홍진;임인성;이용복;최현규
    • 천문학논총
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    • 제33권1호
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    • pp.1-7
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    • 2018
  • In order to encourage collaboration with North Korea in astronomy research field, we have studied the astronomical almanacs published in South and North Korea. The almanac contains fundamental astronomical data including not only daily calendar data but also unique characteristics selected by necessity in each country. We compared the South and North Korean astronomical almanacs in terms of contents, detailed descriptions, unique items, and so forth. We used the 2017 almanac for South Korea and 1993 almanac which is useful for this research for North Korea. We found that there were several differences between South and North Korean almanacs. The North Korean almanac is published for the astronomer or navigator, thus it has supplementary information about spherical astronomy such as precession of the north pole and position of celestial bodies. Whereas the South Korean almanac is published for the general public, and it distinctively contains luni-solar calendar, 24 solar terms, national holidays, etc. This study could be helpful for research cooperation between South and North Korea in astronomy.

LONG-TERM VARIATION STUDY OF CATACLYSMIC VARIABLES WITH PALOMAR TRANSIENT FACTORY

  • YANG, MICHAEL TING-CHANG;CHOU, YI;HU, CHIN-PING;SU, YI-HAO;HSIEH, HUNG-EN;LIN, CHING-PING;CHUANG, PO-SHENG;LIAO, NAI-HUI
    • 천문학논총
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    • 제30권2호
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    • pp.193-195
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    • 2015
  • The Palomar Transient Factory is a project making use of a Schmidt 48 inch telescope located on the Palomar Mountain, which is surveying the sky with dynamical cadences. It was deployed in 2009 and the observed sky region is over 1200 square degrees. We have studied the long-term periodic variabilities of the known galactic cataclysmic variables (CVs). More than 20 of the sources had been found to have long term periodic signals, ranging from several tens of days to several hundreds of days. Some possible scenarios are proposed to explain the results, such as a magnetic field change of the companion star, precession of the accretion disk, triple systems and superoutburst cycles. Some preliminary discussion will be presented in this article.

THE ZERO-POINT OF THE ZODIAC OF THE HINDU ASTRONOMERS IN ANCIENT INDIA

  • BANDYOPADHYAY, AMALENDU
    • 천문학논총
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    • 제30권2호
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    • pp.709-711
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    • 2015
  • In modern Astronomy the vernal equinoctial (VE) point is taken as the starting point for measuring celestial longitudes. Due to the precession of equinoxes, the above point is receding back along the ecliptic. As a result, the longitudes of fixed stars are increasing every year. In ancient India, the Hindu astronomers did not favour the idea of fixed stars changing their longitudes. In order to stabilize the zodiac, they had taken as the origin a point which is fixed on the ecliptic and as such is quite different from the VE point. This initial point being a fixed one, the longitude of stars measured from this origin remain invariable for all time. There was an epoch in the past when this initial point coincided with the VE point and thus the epoch may be called the zero-year. There is controversy over the determination of the zero-year. The reasons for the choice for the fixed zodiacal system by the Hindu astronomers as well as the epoch of zero-year have been found out on the basis of information available in various astronomical treatises of ancient India written in Sanskrit.