• 한국군사과학기술학회지
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• 제11권6호
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• pp.55-62
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• 2008

An Estimation of VHF datalink range for EW(Electronic Warfare) equipment in the sea environment was studied to predict the datalink range between transmitting and receiving station. We consider refraction and reflection in addition to the basic radar equation. The reflection especially includes propagation factor in case of spherical earth as well as flat earth. The estimation result can predict the real datalink range within 5% error.

• 천문학회보
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• 제40권1호
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• pp.65.2-65.2
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• 2015

We developed a three-dimensional magnetohydrodynamic (MHD) code to reproduce the structure of a solar wind, the properties of a coronal mass ejection (CME) and the interaction between them. This MHD code is based on the finite volume method incorporating total variation diminishing (TVD) scheme with an unstructured grid system. In particular, this grid system can avoid the singularity at the north and south poles and relax tight CFL conditions around the poles, both of which would arise in a spherical coordinate system (Tanaka 1994). In this model, we first apply an MHD tomographic method (Hayashi et al. 2003) to interplanetary scintillation (IPS) observational data and derive a solar wind from the physical values obtained at 50 solar radii away from the Sun. By comparing the properties of this solar wind to observational data obtained near the Earth orbit, we confirmed that our model captures the velocity, temperature and density profiles of a solar wind near the Earth orbit. We then insert a spheromak-type CME (Kataoka et al. 2009) into the solar wind to reproduce an actual CME event. This has been done by introducing a time-dependent boundary condition to the inner boundary of our simulation domain. On the basis of a comparison between a simulated CME and observations near the Earth, we discuss the physics involved in an ICME interacting with a solar wind.

• 제어로봇시스템학회논문지
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• 제13권10호
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• pp.962-969
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• 2007

In this paper, an approach is developed for relative state estimation of satellite formation flying. To estimate relative states of two satellites, the Extended Kalman Filter Algorithm is adopted with the relative distance and speed between two satellites and attitude of satellite for measurements. Numerical simulations are conducted under two circumstances. The first one presents both chief and deputy satellites are orbiting a circular reference orbit around a perfectly spherical Earth model with no disturbing acceleration, in which the elementary relative orbital motion is taken into account. In reality, however, the Earth is not a perfect sphere, but rather an oblate spheroid, and both satellites are under the effect of $J_2$ geopotential disturbance, which causes the relative distance between two satellites to be on the gradual increase. A near-Earth orbit decays as a result of atmospheric drag. In order to remove the modeling error, the second scenario incorporates the effect of the $J_2$ geopotential force, and the atmospheric drag, and the eccentricity in satellite orbit are also considered.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2005년도 Proceedings of ISRS 2005
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• pp.589-592
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• 2005

Gravity characteristics and Moho undulations are investigated in the Korean peninsula by using satellite gravity data. According to the development of satellite geodesy, gravity potential models which have high accuracy and resolution were released. Using the EIGEN-CGOIC model based on low orbit satellite data such as CHAMP and GRACE, geoid and gravity anomaly were calculated by spherical harmonic analysis. The study area is located at $123^{\circ}\sim132^{\circ}E, 33^{\circ}\sim43^{\circ}$N including Korea. Free-air anomalies, which show the effect of terrain, have the values between $-37\sim724 mgal. After Bouguer correction, the range of simple Bouguer anomalies is $-221\sim246$ mgal. Complete Bouguer anomalies after terrain correction increase from continent to marine. This phenomenon is related rise of Moho discontinuity. The cut-frequency for extraction of Moho undulation was determined by power spectrum analysis, and then 3D inversion modeling was implemented. The mean, maximum, minimum, and standard deviation of Moho depth undulation are -26, -36, -8, and 4.9 krn, respectively.

• 해양환경안전학회:학술대회논문집
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• 해양환경안전학회 2006년도 추계학술발표회
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• pp.137-141
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• 2006

선박용 디지털 컴퍼스를 사용하는 경우 선박의 진방위를 획득하기 위해서는 고정밀도의 자차와 편차가 필요하다. 편차는 지구자장의 주 자장과 경년변화에 대한 구면 지구 조화 모델을 이용한 WMM(World Magnetic Model)으로 예측 가능하였고, 자차는 포아송 방정식을 적용한 자차계수 합성과 분석 방법을 적용한 방법을 이용하여 획득 가능하였다. 실습선 '새누리호' 항해 중 디지털 컴퍼스에 편차와 자차를 가해준 결 과 정확한 진방위 획득이 가능하였다.

• 자원환경지질
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• 제38권3호
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• pp.299-304
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• 2005

GRACE 위성자료를 이용하여 한반도를 포함한 동아시아 지역에서 지오이드와 중력이상을 계산하였다. 지오이드의 기복은 중국 내륙에서 한반도를 거쳐 태평양쪽으로 갈수록 음에서 양으로 -60 m에서 60m로의 변화가 나타난다 중력이 상은 섭입대에서의 특징적인 -100 mgal 이하의 저이상대를 제외하면 전체적으로 $-60\~60\;mgal$의 분포를 보이며, 북한 지역의 백두산과 개마고원, 남한지역의 태백산맥에서 고이상이, 동해의 울릉분지, 일본분지, 야마토 분지에서 저이상이 관찰된다. 지각 성분만을 고려하기 위한 방법으로 구면조화분석시 degree 10이하의 광역성분을 제거하여 잔여이상을 계산하였다. 계산된 잔여이상에서 한반도 육상 북부 산간 지역과 경상분지 일대에서 고이상이 보이고, 한반도 주변 해상지역의 서한만 분지와 남한 군산분지, 제주분지, 울릉분지 등지에서 저이상대가 관찰된다. 육상지역과 해상지역에서 계산된 잔여이상과 degree별 분리된 이상대의 분포는 지하 지질 규모 및 심도별 분포와 관련하여 대규모 지구조를 규명하거나, 나아가 지하자원 탐사에 유용하게 활용할 수 있을 것으로 판단된다.

• Journal of Astronomy and Space Sciences
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• 제14권1호
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• pp.136-141
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• 1997

임의의 순간 인공위성의 위치와 속도를 정밀하게 계산하기 위해서는 섭동력을 일으키는 우주공간의 환경을 정확하게 이해하고 분석하여 정량화함으로써 섭동력에 대한 수리적인 모형을 만들어야 한다. 이들 우주환경모델에 의해서 인공위성이 받는 총가속도는 2계 미분방정식으로 표현되며, 이 방정식을 두 번 적분함으로써 원하는 시각에서의 인공위성의 위치와 속도를 얻는 코웰방법을 사용하여 궤도예측 알고리즘을 완성하였다. 정지위성의 궤도에 미치는 주요한 섭동력으로는 지구의 비대칭 중력 포텐셜에 의한 섭동력, 태양과 달의 중력에 의한 섭동력, 태양의 복사압에 의한 섭동력들이 있는데, 그것들의 정밀성을 최대한 높이기 위해 spherical harmonic 계수들을 40 $\times$ 40까지 적용할 수 있도록 했으며, JPL DE 403 ephemeris의 polynomial 내삽을 통해 지구로부터 태양과 달까지의 거리를 정밀하게 계산하였다. 그리고 수치적분 방법으로는 적분간격을 자동으로 조절하는 8계 Runge-Kutta single step 방법을 사용하였다.

• 한국군사과학기술학회지
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• 제21권6호
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• pp.799-806
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• 2018

In this paper, we analyzed the communication distances in the flat and spherical earth model using the main specifications of the wireless communication device under development to be installed in the unmanned surface vehicle(USV). We installed the wireless communication device on the test ship and the actual communication test was performed in the South Sea of Korea, it compared the experimental result with the simulated results. If the installation altitude of the transmitting and receiving antennas is low, there is not the big difference between the two models. However, when the altitude of one of the two antennas is high, the spherical earth model has similar results to the experimental data. As the altitude of the antenna installation increases, fading occurs in a certain section. We expect that this fading can be overcome through antenna technologies such as space diversity.

• 자원환경지질
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• 제12권2호
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• pp.95-104
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• 1979

The position of any point on the earth's surface can be. represented in the spherical coordinates by surface spherical harmonics. Since geomagnetic field is a function of position on the earth, it can be also expressed by spherical harmonic analysis as spherical harmonics of trigonometric series of $a_m({\theta})$ cos $m{\phi}$ and $b_m({\theta})$ sin $m{\phi}$. Coefficients of surface spherical harmonics, $a_m({\theta})$ and $b_m({\theta})$, can be drawn from the components of the geomagnetic field, declination and inclination, and vice versa. In this paper, components of geomagnetic field, declination and inclination in the Korean peninsula are obtained by spherical harmonic analysis using the Gauss coefficients calculated from the world-wide magnetic charts of 1960. These components correspond to the values of normal geomagnetic field having no disturbances of subsurface mass, structure, and so on. The vertical and total components offer the zero level for the interpretation of geomagnetic data obtained by magnetic measurement in the Korean peninsula. Using this zero level, magnetic anomaly map is obtained from the data of airborne magnetic. prospecting carried out during 1958 to 1960. The conclusions of this study are as follows; (1) The intensity of horizontal component of normal geomagnetic field in Korean peninsula ranges from $2{\times}10^4$ gammas to $2.45{\times}10^4$ gammas. It decreases about 500 with the increment of $1^{\circ}$ in latitude. Along the same. latitude, it increases 250 gammas with the increment of $1^{\circ}$ in longitude. (2) Intensity of vertical component ranges from $3.85{\times}10^4$ gammas to $5.15{\times}10^4$ gammas. It increases. about 1000 gammas with the increment of $1^{\circ}$ in latitude. Along the same latitude, it decreases. 150~240 gammas with the increment of $1^{\circ}$ in longitude. Decreasing rate is considerably larger in higher latitude than in lower latitude. (3) Total intensity ranges from $4.55{\times}10^4$ gammas to $5.15{\times}10^4$ gammas. It increases 600~700 gammas with the increament of $1^{\circ}$ in latitude. Along the same latitude, it decreases 10~90 gammas. with the increment of $1^{\circ}$ in longitude. Decreasing rate is considerably larger in higher latitude as the case of vertical component. (4) The declination ranges from $-3.8^{\circ}$ to $-11.5^{\circ}$. It increases $0.6^{\circ}$ with the increment of $1^{\circ}$ in latitude. Along the same latutude, it increases $0.6^{\circ}$ with the increment of l O in longitude. Unlike the cases of vertical and total component, the rate of change is considerably larger in lower latitude than in higher latitude. (5) The inclination ranges from $57.8^{\circ}$ to $66.8^{\circ}$. It increases about $1^{\circ}$ with 'the increment of $1^{\circ}$ in latitude Along the same latitude, it dereases $0.4^{\circ}$ with the increment of $1^{\circ}$ in longitude. (6) The Boundaries of 5 anomaly zones classified on the basis of the trend and shape of anomaly curves correspond to the geologic boundaries. (7) The trend of anomaly curves in each anomaly zone is closely related to the geologic structure developed in the corresponding zone. That is, it relates to the fault in the 3rd zone, the intrusion. of granite in the 1st and 5th zones, and mountains in the 2nd and 4th zones.

• 대한공간정보학회지
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• 제16권3호
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• pp.117-126
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• 2008

지구중력장모델은 지오이드 모델링에 있어서 기준면을 결정하기 위하여 사용되어 왔으며, 1980년대 이후로 많은 전지구적 지오포텐셜모델이 개발되었다. 오늘날 EGM96과 EIGEN-GL04C 모델이 전세계적으로 가장 많이 사용되어 왔으나 EGM2008이라고 불리우는 지구중력장모델이 미국의 NGA에 의해 올해 개발되었다. 본 연구에서는 이러한 세 개의 지구중력장모델에 대하여 구면조화분석을 실시하고 그 결과를 비교하고자 하였다. 따라서 구면조화분석은 한반도 일원에 대하여 $1'{\times}1'$격자간격으로 EGM96과 EIGEN-GL04C 모델은 최대차수 360으로, EGM2008의 경우 차수를 360, 720, 1440, 2190으로 변화시켜 가면서 실시하였다. 정확도 평가를 위하여 464점의 GPS/leveling 데이터에서 기하학적 지오이드고가 계산되었으며, 평가결과 EGM2008 모델이 EGM96이나 EIGEN-GL04C 모델에 비하여 상당한 수준으로 정확도를 개선시킴을 알 수 있었으며 한반도 일원에서 14cm 이내의 정밀도로, LSC적합 이후에는 5.5cm의 정밀도로 지오이드고를 계산할 수 있음을 알 수 있었다.