• 제목/요약/키워드: Lunar Effect

검색결과 61건 처리시간 0.034초

The Transition Effect of Korea's Space Development

  • Kim, Jong-bum
    • International Journal of Advanced Culture Technology
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    • 제6권2호
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    • pp.80-85
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    • 2018
  • In the 1990s, South Korea recently launched Space Development and is pushing for a step toward Space. In the Space Launch Vehicle field, the development of Practical satellite type Launch Vehicle (Korea Space Launch Vehicle II) has progressed to the stage of proprietary development, and in the field of Satellite development, they also have a great deal of competitiveness. This study will be a shortcut to rediscovering our potential and looking for breakthroughs by reviewing and re-examining the effects of past Space development.

A Refinement of Point Forecast Using Dependency Structure in Irregualr Component of BOK-X12-ARIMA

  • Hwang, S.Y.;Yang, S.K.
    • Journal of the Korean Data and Information Science Society
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    • 제17권1호
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    • pp.141-147
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    • 2006
  • BOK-X12-ARIMA has been developed by the Bank of Korea in order to accomodate special features such as lunar effect, labor day and election effect which are intrinsic in Korean seasonal time series. Irregular component resulting from BOK-X12-ARIMA is usually treated as white noise time series. If this shows dependency structure, it may be advisable to incorporate dependency in irregular component into prediction. This article illustrates how to refine point forecast using dependency structure in irregular component.

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The Effect of Day Length and Lunar Phases on the Spawning Activity in the Nile Tilapia Oreochromis niloticus

  • Kwon, Joon-Yeong;Kim, Jung-Hyun;Kim, Bo-Kyong
    • 한국발생생물학회지:발생과생식
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    • 제14권1호
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    • pp.21-25
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    • 2010
  • Nile tilapia (Oreochromis niloticus) are mouth-brooders so that the females holding eggs in their mouth sacrifice their somatic growth for reproduction. For this reason, artificial control of reproduction for the culture of this species has been of interest. Manipulation of photoperiod is an emerging technique for such purpose, but little information is available to establish appropriate photoperiod regime. To obtain necessary basic information, sexually mature females were individually accommodated to glass aquarium, and the spawning activity of these females were monitored for two years under natural photoperiod regime. Female tilapia spawned most frequently on March, April and May when the day length gradually increased from 11 hours to 14 hours and least frequently on September, October, November and December when the day length gradually decreased from 13 hours to less than 10 hours in the first year. The decrease of spawning frequency as day length decreased was also observed in the second year, although the increase of spawning frequency as day length increased was less clear. Spawning of female tilapia was less active when the night was dark due to the disappearance of moonlight (Dark Phase), compared to the Phase of Getting Lighter, Light Phase and Phase of Getting Darker. Results from this study suggest that long day length, particularly increasing phase, is favoured for active spawning of Nile tilapia, and that this species, as a tropical fish species, may utilize changing lunar phases as a secondary environmental cue for reproduction.

지반 조건 및 휠 형상에 따른 달탐사 로버 휠 주행 성능 평가 실험 연구 (Experimental Analysis of Lunar Rover Wheel's Mobility Performance Depending on Soil Condition and Wheel Configuration)

  • 왕성찬;김석중;한진태
    • 대한토목학회논문집
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    • 제37권4호
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    • pp.693-703
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    • 2017
  • 달 탐사 로버 휠의 주행 성능은 지반 조건과 휠의 형상에 따라 크게 달라진다. 이에 본 연구에서는 한국형 인공월면토 및 주문진 표준사에서 휠 형상을 변화시켜 달 탐사 로버 휠의 주행성능 평가를 실시하였다. 단일 휠 성능평가 실험장비를 이용하여 지반조건에 따른 영향을 검토하였고, 이와 더불어 인공월면토에서 그라우저 높이에 따른 휠 주행성능 평가를 실시하였다. 휠 주행성능 평가는 슬립율에 따른 토크, 견인력 및 침하량을 측정하여 각 조건별로 상대적인 비교를 하였다. 실험 결과 주문진 표준사에 비해 한국형 인공월면토에서 로버 휠 주행성능이 우수하였으며, 휠 주행성능이 흙의 점착력과 마찰각 특성에 큰 영향을 받는 것으로 나타났다. 또한, 휠 그라우저 높이에 따라 견인성능이 증가하는 것으로 나타났다.

태양계 행성의 고정확도 위치계산에 과한 연구(II) (SOFTWARE DEVELOPMENT OF HIGH-PRECISION EPHEMERIDES OF SOLAR SYSTEM (II))

  • 신종섭;안영숙;박필호;박은광;박종옥
    • 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

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한국 사춘기 소녀들의 골밀도와 환경요인들과의 관계(II) (The Relationship Between Bone mineral Density and The Environmental Factors in Korean Pubescent Girls)

  • 최미자
    • 동아시아식생활학회지
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    • 제5권1호
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    • pp.41-51
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    • 1995
  • Bone mass accretion during puberty appears to be critical in the development of peak bone mass. Although bone density of females in Korea has been studied, only a few studies have related bone mass with anthropometric patterns or puberty in the pubescent girls. This study was conducted as part of a study of major determinants of bone development during puberty. Subjects were aged 14∼16 yr(mean 14.97), and had no history of disorders or dedication use likely to influence bone or calcium metabolism. Bone mineral density and content were measured by dual energy X-ray absorptiometry using a Lunar DPX+Scanner (Lunar Madison, WI). Also, total body fat, and total lean body mass were assessed using a Lunar DPX dual-energy X-ray absorptiometer, Pubertal status was assessed according to the Marshall and Tanner guidelines. Serum levels of osteocalcin was measured by RIA using a commercial kit assay. Skinfold measurements were taken with a skinfold caliper(Lange Caliper, USA). Data were analyzed using the regression and GLM procedure of the statistical package SAS. The results indicated that the observed means for lumbar spine BMD and femoral BMD correspond to approximately 91% and 96% of the means for young adult females, respec tively. All subjects were menarchal, with the majority being in the middle to end stages of pubertal development. Total body BMD was positively related to fat mass(P<0.001), lean body mass and time since menarche, and negatively related to urine pyridinoline, serum alkaline phosphatase and osteocalcin. The data indicate that girls who reported lower age for menarche had significantly higher bone densities than girls who reported higher age for menarche. Attaining peak skeletal bone mass during puberty may reduce the incidence of osteoporosis in later life. this finding suggests that early menarche may augment peak bone mass, influencing the extent of bone loss later in adulthood. The results suggest that good nutrition in childhood appears to be needed not for growth and development, but possibly also to assure an optimal peak of bone mass and thus greater latitude for the maintenance or skeletal integrity in the face of bone losses. Troeps skinfold thickness was a better predictor of total BMD and total BMC than was any other skinfold thickness. The study did not find a relationship between total BMD and body fat %, but total fat was significantly positively related to total BMD(r=0.49) and total BMC(r=0.60). It supports earlier report that there was a significant correlation between TBMD and body weight. Conclusively, total fat, lean body mass and pubertal development could influence BMD in pubescent girls. Clearly, longitudinal studies are required to assess the effect of puberty on peak bone mass, and to define further the potential determinants of peak bone mass.

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FRICTION UNITS FOR THE MOON

  • Drozdov, Yu.N.
    • 한국윤활학회:학술대회논문집
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    • 한국윤활학회 2002년도 proceedings of the second asia international conference on tribology
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    • pp.389-396
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    • 2002
  • In XXI century it is necessary to expect the recommencement and development of activities on mastering the Moon. In the long term it is construction of manned lunar bases with industrial, astrophysical, procuring, repair equipment and services. Interplanetary flights from the Moon demand smaller power expenditures, than from the Earth, therefore it is favourable to use its surface for the construction of space-vehicle launching sites. Flights of devices in libration points in the system 'Earth - Moon' are considered. Experience of engineering system creation for the Moon displays the great complexity in provision of serviceability and reliability of friction units. Open friction units should operate under following conditions on the Moon: pressure of environment (vacuum) $p\;>10\;^{-10}$ Pa; wide range of temperature change $+150^{\circ}C\;...170^{\circ}C$; high evaporability of lubricants; influence of temperature gradients and warping of constructions; sublimation of elements of constructional materials; irradiation of different physical nature; effect of micrometeorites; reduced gravitation; influence of abrasive particles of lunar ground; requirements on minimization of size and weight characteristics of a construction (high tension); undesirability (impossibility) of application of liquid and plastic lubricants; vibration, shock, acoustic loadings during start and landings to the Earth; difficulties in repair-regenerative operations in conditions of the Moon etc. Adhesive interaction of conjugated surfaces is the principal reason of possible failures of rubbed units on the Moon. In the research of the Moon automatic interplanetary stations of 'Luna' (USSR), 'Surveyer', 'Apollo' (USA) series were used. Stations executed functions of flying, landing, artificial satellites of the Moon, moon-rovers and manned spacecrafts such as 'Apollo'. The experimental- theoretical researches carried out in the sixtieth years on tribology for conditions of the Moon appeared to be rather useful to engineering of an outer space exploration and the decision of complex problems for the friction units operating in extreme conditions on the Earth. For the creation of highly loaded friction units for the long service life on the Moon it is required not only to use accumulated experience and designed technologies, but also to carry out wide scientific research.

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달 착륙선의 위험 상대거리 기반 착륙지 선정기법 성능 분석 (Performance Analysis of Landing Point Designation Technique Based on Relative Distance to Hazard for Lunar Lander)

  • 이충민;박영범;박찬국
    • 한국항공우주학회지
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    • 제44권1호
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    • pp.12-22
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    • 2016
  • 달착륙선의 라이다 기반 위험회피 착륙시스템은 기본적으로 목표 착륙지역에 대한 지형 파라미터인 경사와 험준도로 위험도를 계산하고 해당 지역에 대하여 위험도가 최소값을 갖는 점을 안전한 착륙 지점으로 선정한다. 이때, 경사와 험준도만을 고려할 경우 라이다 측정오차에 의해 착륙지가 위험요소 근처로 선정될 수 있으며 이는 착륙선에 위협적이다. 이러한 문제를 해결하고 최대한 안전한 착륙지점을 선정하기 위하여 위험상대거리 기반의 위험도를 기존의 지형파리미터 기반의 위험도와 함께 고려하여야 한다. 본 논문에서는 경사와 험준도 각각에 대한 위험상대거리 기반 위험도가 지형 특성에 따라 착륙지 선정결과에 미치는 영향을 분석하였고, 두 가지 위험상대거리를 동시에 고려하였을 때 가장 좋은 위험회피 착륙 성능을 나타냄을 시뮬레이션과 3차원 뎁스 카메라를 이용한 실험을 통해 확인하였다.

시간대별 상대계수를 이용한 특수일이 포함된 평일의 전력수요예측 (Daily Load Forecasting Including Special Days Using Hourly Relative factors)

  • 안대훈;이상중
    • 조명전기설비학회논문지
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    • 제19권5호
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    • pp.94-102
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    • 2005
  • 본 논문은 전력계통에서의 전력수요예측을 하기 위한 네가지중 하나의 방법으로 특수일에 적용기법인 수요예측 담당자의 Know-How를 기반으로 예측하는 전문가법에 대하여 과거 15년간의 수요실적과 기상실적을 근거로 년중 모든 특수일에 대해서 수요패턴 분석을 실시하고 패턴의 변화되는 과정을 살펴보았다. 과거 전력수요 실적의 근거로 산출된 시간대별 상대계수의 수요패턴을 가지고 모의 운영한 결과 설 연휴 수요예측 오차율은 과거 5일간(2002, 2003년도)의 평균값 $3.23{[\%]}$에서 2005년도 설 연휴 실적대비 $1.78{[\%]}$로 상당한 개선효과가 있었다. 본 논문의 내용을 바탕으로 전력수요 예측 편람을 작성하는 것도 입문교재로서 수요예측 전문가 양성에 큰 도움을 줄 수 있을 것으로 기대된다.

무궁화위성의 궤도결정 (Orbit determination of moogunghwa satellite)

  • 박수홍;조겸래
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 1992년도 한국자동제어학술회의논문집(국내학술편); KOEX, Seoul; 19-21 Oct. 1992
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    • pp.692-697
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    • 1992
  • This study concerns about the orbit prediction and orbit determination of Korean future communication satellite, called "Moogunghwa", which will be motioned in the geo-stationary orbit. Perturbation effect on the satellite orbit due to nonspherical geopotential term, lunar and solar gravity, drag force of the atmosphere and solar radiation pressure was investigated. Cowell's method is used for orbit prediction. Orbit determination was performed by using EKF which is suitable for real-time orbit determination. The result shows that the characteristics of the satellite orbit has drift. So the periodic control time and control value in the view of the periodic of error can be provided. The orbit determination demonstrated the effectiveness since the convergence performance on the position and velocity error , and state error standard deviation is reasonable.easonable.

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