• 한국측량학회지
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• 제30권6_2호
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• pp.593-605
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• 2012

LiDAR systems provide dense and accurate topographic information. A pre-requisite to achieving the potential accuracy of LiDAR is having a proper system calibration, which aims at estimating all the systematic errors in the system measurements and the mounting parameters relating the different components. This paper presents a rigorous and two approximate methods for LiDAR system calibration. The rigorous approach makes use of the LiDAR equation and the system raw measurements. The approximate approaches utilize simplified LiDAR equations using some assumptions, which allow for less strict requirements regarding the raw measurements. The first presented approximate method, denoted as quasi-rigorous, assumes that we are dealing with a vertical platform (i.e., small pitch and roll angles). This method requires time-tagged point cloud and trajectory position data. The second approximate method, denoted as simplified, assumes that we are dealing with parallel strips, vertical platform, and minor terrain elevation variations compared to the flying height above ground. Such method can be performed using the LiDAR point cloud only. Experimental results using a real dataset, whose characteristics deviate to some extent from the utilized assumptions in the approximate methods, are presented to provide a comparative analysis of the outcome from the introduced methods.

• 대한토목학회논문집
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• 제8권4호
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• pp.33-39
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• 1988

본(本) 연구(硏究)는 matrix 해석(解析)(rigorous-method)을 이용(利用)하여 정밀(情密) traverse망(網)을 조정(調整)하는데 목적이 있다. 본(本) 연구(硏究) 결과(結果), matrix 해석(解析)에 의(依)한 엄밀해법(嚴密解法)으로도 복잡(複雜)한 traverse망(網)을 신속(迅速) 정확(正確)하게 처리(處理)할 수 있다. 또한 종래(從來)의 근사해법(approximate-method)을 본(本) matrix 해법(解法)의 조정(調整)값과 비교(比較)한 결과(結果) 평균(平均)제곱오차범위이내(誤差範圍以內)에 있고, 조정좌표(調整座標)값의 비교차(比較差)도 0.4~0.9mm정도(程度)로 나타났으며, 이로써 근사해법(approximate-method)의 실용적(實用的) 가치(價値)를 입증(立證)하게 되었다.

• 한국해양공학회지
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• 제35권2호
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• pp.131-140
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• 2021

The paper deals with comparative study of various surrogate models based approximate optimization in the structural design of the passive type deck support frame under design load conditions. The passive type deck support frame was devised to facilitate both transportation and installation of 20,000 ton class topside. Structural analysis was performed using the finite element method to evaluate the strength performance of the passive type deck support frame in its initial design stage. In the structural analysis, the strength performances were evaluated for various design load conditions. The optimum design problem based on surrogate model was formulated such that thickness sizing variables of main structure members were determined by minimizing the weight of the passive type deck support frame subject to the strength performance constraints. The surrogate models used in the approximate optimization were response surface method, Kriging model, and Chebyshev orthogonal polynomials. In the context of numerical performances, the solution results from approximate optimization were compared to actual non-approximate optimization. The response surface method among the surrogate models used in the approximate optimization showed the most appropriate optimum design results for the structure design of the passive type deck support frame.

• Journal of Biosystems Engineering
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• 제20권3호
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• pp.205-216
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• 1995

A fast and inexpensive approximate analysis method to predict power output characteristics of the Stilting engines in a preliminary design stage was investigated. In basic equations proposed by Walker, typical temperatures of working fluids in expansion and compression spaces were treated as those of working fluids in heater and cooler respectively. While the temperature of working fluid in the expansion space was actually lower than that of working fluid in the heater, the temperature of working fluid in the compression space was higher than that of working fluids in the cooler. In this paper, the working fluid temperature of expansion space was treated as lower than the heater temperature and that of compression space was treated as higher than the cooler temperature. Also, according to them, the power output characteristics of the Stirling engine were evaluated with respect to the GPU-3 and 4-215 Stilting engines. The following conclusions were drawn from the analysis. 1. Using the available experimental data from the GPU-3 Stirling engine, it was shown that the approximate analysis predicts the brake power with a maximum error of 19 percent at 1, 000rpm and with a minimum error of 3 percent at 2, 000rpm. 2. The approximate analysis data which for the GPU-3 Stirling engine were much closer to the experimental data than those of adiabatic 2nd order and 3rd order analysis within 1, 500rpm to 2, 500rpm. 3. The approximate analysis data which for the GPU-3 and 4-215 Stilting engines were much closer to the experimental data than those of the Beal number analysis.

• 한국전산구조공학회:학술대회논문집
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• 한국전산구조공학회 1997년도 가을 학술발표회 논문집
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• pp.270-278
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• 1997

The purpose of this paper is to evaluate the effectiveness of eigen modes by modal analysis and the application of approximate eigen modes for continuum. This study proposes the appropriate selection technique of eigen modes by modal analysis and the method for the reasonable survey of post-buckling path. And the buckling characteristics of a latticed dome is studied by the application of these approximate eigen modes which have sufficient accuracy and praticallity for response analysis in symmetric and anti-symmetric state of continuous shell. To prove the effectiveness of eigen modes and application of approximate eigen modes for continuum, these results are compared with those of direct method.

• International Journal of Aeronautical and Space Sciences
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• 제18권3호
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• pp.450-466
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• 2017

This paper defines the modified effective membrane stiffness, bending stiffness considering the directionally dependent mechanical properties and mode shape function of a composite lattice rectangular plate, which is assumed to be a Kirchhoff-Love plate. It subsequently presents an approximate method of conducting a buckling analysis of the composite lattice rectangular plate with various boundary conditions under uniform compression using the Ritz method. This method considers the coupled buckling mode as well as the global and local buckling modes. The validity of the present method is verified by comparing the results of the finite element analysis. In addition, this paper performs a parametric analysis to investigate the effects of the design parameters on the critical load and buckling mode shape of the composite lattice rectangular plate based on the present method. The results allow a database to be obtained on the buckling characteristics of composite lattice rectangular plates. Consequently, it is concluded that the present method which facilitates the calculation of the critical load and buckling mode shape according to the design parameters as well as the parametric analysis are very useful not only because of their structural design but also because of the buckling analysis of composite lattice structures.

• Structural Engineering and Mechanics
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• 제59권1호
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• pp.1-14
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• 2016

In this paper, an alternative analytical method is presented to evaluate the nonlinear vibration behavior of single and double tapered cantilever beams. The admissible lateral displacement function satisfying the geometric boundary conditions of a single or double tapered cantilever beam is derived by using Rayleigh-Ritz method. Based on the Lagrange method and the Newton Harmonic Balance (NHB) method, analytical approximate solutions in closed and explicit form are obtained. These approximate solutions show excellent agreement with those of numeric method for small as well as large amplitude. Moreover, due to brevity of expressions, the present analytical approximate solutions are convenient to investigate effects of various parameters on the large amplitude vibration response of tapered beams.

• 지질공학
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• 제11권2호
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• pp.153-161
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• 2001

암반사면의 안정성 평가에 있어서 경험적 평가에 중점을 둔 RMR분류법과 여러 가지 변수들을 이용한 평가방법인 평사투영·한계평형·유한차분·개별요소해석을 실시하였다. 그리고 여러 가지 암반사면의 안정성에 영향을 미치는 변수들의 불확실성을 고려할 수 있는 점추정법에 의한 신뢰성해석과 더불어 퍼지언어를 이용한 퍼지근사추론법의 구조화에 따른 평가방법을 비교·분석 하였다. 그 결과 점추정법의 신뢰성해석을 전 구간의 안정성을 평가 할 수 있으며 퍼지근사추론법에 의한 안정성평가는 다른 기존의 안정성해석 결과와 전반적으로 일치함을 알 수 있다. 이와 같이 RMR분류·평사투영·한계평형·유한차분·개별요소해석과 점추정법의 신뢰성해석, 퍼지근사추론법을 병행하면 암반사면의 특수성을 체계적이고 종합적으로 평가할 수 있다.

• 한국항공운항학회지
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• 제16권2호
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• pp.21-27
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• 2008

An inverse method is introduced to construct the problem for the error analysis of the numerical solution of initial value problem. These problems constructed through this method have a known exact solution, even though analytical solutions are generally not obtainable. The process leading to the exact solution makes use of an initially available approximate numerical solution. A smooth interpolation of the approximate solution is forced to exactly satisfy the differential equation by analytically deriving a small forcing function to absorb all of the errors in the interpolated approximate solution. Using this special case exact solution, it is possible to investigate the relationship between global errors of a candidate numerical solution process and the associated tuning parameters for a given problem. Under the assumption that the original differential equation is well-posed with respect to the small perturbations, we thereby obtain valuable information about the optimal choice of the tuning parameters and the achievable accuracy of the numerical solution.

• 한국산학기술학회논문지
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• 제12권8호
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• pp.3689-3696
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• 2011

의사결정 지원시스템에서 작업자들은 대량의 데이터 집계 연산을 요구하며, 데이터에 대한 정확한 응답보다는 경향 분석에 더 많은 관심을 가진다. 그러므로 정확한 응답보다 빠른 근사 질의응답을 제공하는 것이 필요하며 그것을 실현하기 위한 근사질의 응답 기법의 연구가 필요하다. 따라서 본 논문에서는 기존 연구들의 단점을 보안하고 근사 응답의 정확성을 향상시킬 수 있는 Fuzzy C-Means (FCM) 클러스터링 기반 Adaptive Neuro-Fuzzy Inference System (ANFIS)을 이용한 근사 질의응답 기법을 제안한다. FCM-ANFIS을 이용한 근사 질의응답 기법은 다차원 데이터의 지식 표현 모델을 생성함으로써 거대한 다차원 데이터 큐브에 직접적인 접근 없이 집계 질의 수행이 가능하다. 비교실험을 통하여 제안된 기법이 기존의 NMF 기법보다 근사 질의응답의 정확성이 향상되었음을 확인한다.