• Journal of Radiation Protection and Research
• /
• v.29 no.2
• /
• pp.105-115
• /
• 2004

The Monte Carlo simulation requires very much time to obtain a result of acceptable accuracy. Therefore we should know the optimum number of history not to sacrifice time as well as the accuracy. In this study, we have investigated the effects of statistical uncertainties of the photon dose calculation. BEAMnrc and DOSXYZnrc systems were used for the Monte Carlo dose calculation and the case of mediastinum was simulated. The several dose calculation result from various number of histories had been obtained and analyzed using the criteria of isodose curve comparison, dose volume histogram comparison(DVH) and root mean-square differences(RMSD). Statistical uncertainties were observed most evidently in isodose curve comparison and RMSD while DVHs were less sensitive. The acceptable uncertainties $(\bar{{\Delta}D})$ of the Monte Carlo photon dose calculation for the radiation therapy were estimated within total 9% error or 1% error for over than $D_{max}/2$ voxels or voxels at maximum dose.

• Proceedings of the Korean Operations and Management Science Society Conference
• /
• 1995.09a
• /
• pp.363-369
• /
• 1995

본 연구에서는 선형계획법 프로그램의 수치오차보정과 행렬희소도 유지를 통하여 수행 속도를 향상시키는 방안에 대해 다룬다. 수치오차를 줄이기 위 해 규모화를 도입하였으며, 계산 과정에서의 상하삼각행렬의 수치오차를 근 사적으로 측정하는 방법을 고려하였다. 기저행렬의 상하분해에 널리 사용되 는 Markowitz 순서화의 효율적인 구현에 대해 연구하였으며, Reid의 기저수 정방법의 효율성에 대해 실험적으로 검토하였다. 또, 행렬의 희소도에 의한 재역산 기준을 수립하여 수행 속도를 개선하였다.

• The Bulletin of The Korean Astronomical Society
• /
• v.37 no.2
• /
• pp.183.1-183.1
• /
• 2012

인공위성의 자세 제어 및 자세 결정에 사용되는 센서들의 정렬오차는 자세명령생성 오차, 자세제어 오차, 자세결정 오차 등과 더불어 지향정밀도를 저하시키는 하나의 요인으로 작용한다. 본 연구에서는 자이로 센서에만 정렬오차가 존재한다고 가정하는 상황에서 별추적기와 자이로 센서를 이용한 자세결정 필터에 의해 추정되는 자이로 바이어스 값만을 이용하여 자이로 센서의 정렬오차를 확인(Identification)하는 방법 및 결과에 대해 기술한다. 이를 추정하는 다른 방법으로는 여러 가지가 있으며 대표적으로 위성의 다축기동 정보를 입력으로 사용하는 확장칼만필터를 이용한 궤도상 보정(On-orbit Calibration) 방법이 있으나 본 연구에서는 위성의 기동 또는 많은 계산량을 소모하지 않고 비교적 간단하게 자이로 정렬오차를 추정하는 방법을 제시하였다. 그리고 실제 궤도상 위성의 거동 데이터를 이용하여 제안한 방법의 효율성을 검증하였다. 결과적으로, 제안된 방법을 이용했을 때 소수점 둘째 자리 이하의 정확도를 가지고 정렬오차가 추정됨을 확인하였다.

• 전기의세계
• /
• v.15 no.4
• /
• pp.27-38
• /
• 1966

본 고에서는 앞으로 신설된 배전계통에서의 고저압혼독시 전위상승에 대해 알아보고자 한다. A항의 검토에서 고목계통의 실측치와 D.C. board에 의한 계산치 사이에 약 10-20%의 오차는 있으나 계산치로써 전위상승을 추정할 수 있음을 알았음으로 신설될 23kv Y및 11.4kv Y배전방식에 대하여 계산한다.

• Journal of Satellite, Information and Communications
• /
• v.9 no.2
• /
• pp.119-125
• /
• 2014

In this paper, we developed the signal generator of GNSS navigation signals and analysis the performance of DCO(Digitally Clock Oscillator) compensation algorithm for cumulative distance error thorough simulation. In general, To generate a GNSS signal calculates the Doppler and Initial Pseudorange by using the location information of the receiver and the satellite. The GNSS signal generator generates a signal by determine the carrier and code output frequency using the Doppler information which is calculated as a function of time. The output frequency of the carrier and code would be used the DCO scheme. At this time, It extract the bit and code information on a for each sample by accumulating the DCO. an error of Pseudorange is generated by the cumulative error of the DCO. If Pseudorange error occurs, so that the influence to and operation of the receiver. Therefore, in this paper, we implemented the accumulated error compensation algorithm of the DCO to remove the accumulated error components DCO thereof, Pseudorange accumulated error is removed through the experiment, it was confirmed to be a high accuracy can be operated.

• Spatial Information Research
• /
• v.11 no.1
• /
• pp.23-32
• /
• 2003

TIN is applied in pondage calculation and topography analysis. And much processing time and storage capacity are needed because TIN contains information as elevation, slope and aspect. In the construction of TIN using contour, weed tolerance that is used for the simplification of line is influenced on the sampling distance of contour. The processing time and storage capacity of TIN are calculated in according to the weed tolerance of various size in this research. And we estimated OEMs standard error that is created from TIN to present reasonable weed tolerance and decided the size of weed tolerance that satisfy DEM standard error. We got TINs weed tolerance that satisfy DEM standard error(5m) was 70m and DEMs resolution is 20m as estimation result.

• The Journal of Korean Institute of Communications and Information Sciences
• /
• v.17 no.4
• /
• pp.387-397
• /
• 1992

The spatial domain design of 2-dimensional separable denominator digital filters(SDDF) based on the reduced dimensional decomposition can be realized when the given 2-D impulse response specifications are decomposed into a pair of 1-D specifications via singular value decompositions(SVD). Because of use of the balaned approximation and equivalent transform as 1-D design algorithm, 2-D design algorithm retains the advantage that is numerically stable and can minimize quantization errors. In this paper in order to analyze and reduce these errors, minimum comfficient quantization realization is directly derived from impulse response specification. And using the equivalent trans form relation between mininum coefficient quantization error and minimum roundoff error realizations, we optimally realize a SDDF. This algorithm is analyzed by the simulation, which shows that it is superior to direct or balanced realization in quantization errors.

• The Journal of Korean Institute of Communications and Information Sciences
• /
• v.32 no.4C
• /
• pp.396-400
• /
• 2007

This paper proposes the fast partial difference elimination (PDE) algorithm. When the conventional PDE cannot skip the rest of matching procedure in a candidate block using a partial matching error, the proposed algorithm estimates to skip it again using the block matching error predicted from the computed partial matching error. The proposed algorithm can eliminate impossible candidate blocks earlier than the conventional PDE since the predicted block matching error is always bigger than the partial matching error. The simulation results show that the proposed algorithm can significantly reduce the computations while keeping image quality as good as the conventional PDE.

• Aerospace Engineering and Technology
• /
• v.7 no.1
• /
• pp.223-228
• /
• 2008

In order to acquire the images requested by users, it is very important to calculate mission schedule parameters such as imaging execution time and attitude tilt angle accurately. These parameters are based on orbit prediction. This paper describes the accuracy of orbit propagation for image planning. The orbit prediction data from PSS and MAPS has a certain discrepancy due to different orbit propagator. It is necessary for mission planner to confirm this value during mission planning phase. The pointing error which means the difference between target center and real image received is calculated and analyzed using KOMPSAT-2 image data.

• Korean Journal of Optics and Photonics
• /
• v.12 no.5
• /
• pp.362-370
• /
• 2001

We prove that 3-D profile mapping using white light interferometry has systematic errors caused by aberrations of the optimal system. The tilt of an object invokes an offset between the object and the reference ray, which eventually makes the aberration cancel incompletely. The fringe peak of a white light interferogram is mainly affected by the aberration effect while the envelope peak remains stable. By the difference between the two peaks, it is easily confirmed how much the error existed in the fringe peak. Experimental results prove that the error caused by aberration is varied by object tilt, microscope NA, optics alignment within the range of $\pm$50nm.