• 대한전기학회:학술대회논문집
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• 대한전기학회 2000년도 하계학술대회 논문집 B
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• pp.699-701
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• 2000

It leaves much room for improvement that UTM-01 is of practical use. Therefor we will design of UTM-02 system. The design of new magnet is based on light weight for bogie system. We used Maxwell-3D FEM for design of new magnet. The new magnet for UTM-02 that was reduced weight of magnet. 22kg, then it was increased ratio lift to weight is 9.87.

• 한국측량학회지
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• 제24권4호
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• pp.313-318
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• 2006

전국 규모의 연속적인 자료구조를 가진 기본지리정보의 생산 및 구축을 효율적으로 수행하기 위해서는 하나의 원점을 가진 좌표계의 도입이 요구된다. 이를 위해서 우리나라는 한반도 전역을 포괄하는 한국형 UTM 좌표계(UTM-K)를 도입하였으며, 본 연구에서는 UTM-K 좌표계에서 설정된 투영중앙 자오선 및 투영중앙 자오선의 축척계수에 대한 왜곡정도를 분석하였다. 투영왜곡의 분석을 위해서 2005년 말까지 제작된 1/25,000 수치지도들의 중심 경위도 좌표를 이용하여 투영으로 인한 축척계수를 계산하고, 이를 왜곡정도의 지표로 사용하였다. 그 결과, 현행 UTM-K에서 정의한 것을 근거로 했을 경우 지도투영으로 인한 축척계수의 누적 왜곡량은 $23.744{\times}10^{-2}$로 나타났다. 반면에 투영중앙 자오선이 $127^{\circ}\;42'$이고, 이때의 축척계수가 0.99994로 설정했을 경우 $5.1435{\times}10^{-2}$의 최소 누적 왜곡량을 보였다.

• 한국해안·해양공학회논문집
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• 제20권3호
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• pp.277-290
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• 2008

경도 $14^{\circ}$ 범위보다 넓은 구역에 대한 UTM 좌표변환을 위하여 12차 Taylor 전개에 의한 새로운 변환식을 유도하였고 이는 Thomas(1952)의 식을 확장한 것임을 보였다. WGS84와 UTM 좌표의 상호변환에 대한 계산 결과를 나타내었고 차수에 따른 수렴의 정도도 분석하였다. 본 변환식은 우리나라 주변의 조석 또는 지진해일과 같은 장주기 파랑의 전파를 위한 수치모형의 직교좌표 격자구성에 사용될 수 있다.

• Structural Engineering and Mechanics
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• 제51권2호
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• pp.215-228
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• 2014

Traditional beam connections to the minor axis of a column have relatively low strength and stiffness. A modified detail, using a plate welded between the toes of the column flange - referred to as a toe plate connection - is examined in this paper. The results of an experimental investigation for both flush and extended end-plate connections connected to a 25 mm thick end-plate are presented. The tests are complemented by finite element modelling which compares very well with the test observations. The results show a significant increase in both moment resistance and initial stiffness for this connection detail compared with connections made directly to the column web. This offers the prospect of more optimal solutions taking advantage of partial strength frame design for the minor axis as well as major axis.

• Steel and Composite Structures
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• 제22권6호
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• pp.1281-1299
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• 2016

This paper deals with the analysis of vibration of antisymmetric angle-ply plates using spline method for higher order shear theory. Free vibration of laminated plates is addressed to show the capability of the present method in the vicinity of higher order shear deformation theory and simply supported edges of plates. The coupled differential equations are obtained in terms displacement and rotational functions. These displacement and rotational functions are approximated using cubic and quantic spline. A generalized eigenvalue problem is obtained and solved numerically for an eigenfrequency parameter and an associated eigenvector of spline coefficients. The antisymmetric angle-ply fiber orientation are taken as design variables. Numerical results enable us to examine the frequencies for various geometric and material parameters and accuracy and effectiveness of the proposed method is also verified by comparative study.

• 한국측량학회지
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• 제25권1호
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• pp.39-45
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• 2007

한국형 UTM 좌표계는 현행 좌표계의 문제점 및 한계를 극복할 수 있으며 GIS를 기반으로 하는 첨단 산업에도 다양하게 적용 될 수 있도록 도입되었다. 본 연구에서는 한반도 전역에 적용 가능한 최적의 UTM-K 투영 중앙자오선과 축척계수를 결정하기 위하여 여러 가지 조합을 설정한 후 각각의 경우에 발생하는 지도의 누적 투영 왜곡량을 비교함으로써 결론을 도출하였다. 남한 지역에 적용하기 위해 도입된 현행 UTM-K에서 정의한 기준을 한반도 전역에 적용해 본 결과, 지도 투영으로 인한 누적 투영 왜곡량은 $47.0837{\times}10^{-2}$로 나타났다. 반면에 투영 중앙 자오선을 $127^{\circ}26'$, 축척계수를 0.99991로 설정했을 경우 누적 투영 왜곡량이 $21.0495{\times}10^{-2}$으로 최소값을 보였다. 따라서 한반도 전역에 적용할 최적의 UTM-K 투영 자오선은 $127^{\circ}26'$, 축척계수는 0.99991라는 결론을 얻었다.

• Structural Engineering and Mechanics
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• 제58권6호
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• pp.1001-1020
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• 2016

The study is to investigate the free vibration of antisymmetric angle-ply conical shells having non-uniform sinusoidal thickness variation. The arbitrarily varying thickness is considered in the axial direction of the shell. The vibrational behavior of shear deformable conical shells is analyzed for three different support conditions. The coupled differential equations in terms displacement and rotational functions are obtained. These displacement and rotational functions are invariantly approximated using cubic spline. A generalized eigenvalue problem is obtained and solved numerically for an eigenfrequency parameter and an associated eigenvector of spline coefficients. The vibration characteristic of the shells is examined for cone angle, aspect ratio, sinusoidal thickness variation, layer number, stacking sequence, and boundary conditions.

• Steel and Composite Structures
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• 제20권5호
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• pp.1087-1102
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• 2016

The paper proposes to characterize the free vibration behaviour of non-uniform cylindrical shells using spline approximation under first order shear deformation theory. The system of coupled differential equations in terms of displacement and rotational functions are obtained. These functions are approximated by cubic splines. A generalized eigenvalue problem is obtained and solved numerically for an eigenfrequency parameter and an associated eigenvector which are spline coefficients. Four and two layered cylindrical shells consisting of two different lamination materials and plies comprising of same as well as different materials under two different boundary conditions are analyzed. The effect of length parameter, circumferential node number, material properties, ply orientation, number of lay ups, and coefficients of thickness variations on the frequency parameter is investigated.

• 한국항공운항학회지
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• 제28권4호
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• pp.47-54
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• 2020

This study carries out a basic study of ways to calculate navigation errors for aircraft operating in the unmanned aerial system traffic management(UTM). Recently, research by UTM has been carried out both at home and abroad, along with the initial study of system definitions at the basic stage, operational techniques of the aircraft, and the practicality of the concept of necessary operations at the actual operational stage. This study presented after a review the factors that should be considered for the calculation of navigation errors among the factors that examine whether the actual low altitude aircraft can operate properly within UTM during its actual operation and the need to apply them in practice.

• Steel and Composite Structures
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• 제26권4호
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• pp.473-484
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• 2018

Free vibration of cross-ply laminated plates using a higher-order shear deformation theory is studied. The arbitrary number of layers is oriented in symmetric and anti-symmetric manners. The plate kinematics are based on higher-order shear deformation theory (HSDT) and the vibrational behaviour of multi-layered plates are analysed under simply supported boundary conditions. The differential equations are obtained in terms of displacement and rotational functions by substituting the stress-strain relations and strain-displacement relations in the governing equations and separable method is adopted for these functions to get a set of ordinary differential equations in term of single variable, which are coupled. These displacement and rotational functions are approximated using cubic and quantic splines which results in to the system of algebraic equations with unknown spline coefficients. Incurring the boundary conditions with the algebraic equations, a generalized eigen value problem is obtained. This eigen value problem is solved numerically to find the eigen frequency parameter and associated eigenvectors which are the spline coefficients.The material properties of Kevlar-49/epoxy, Graphite/Epoxy and E-glass epoxy are used to show the parametric effects of the plates aspect ratio, side-to-thickness ratio, stacking sequence, number of lamina and ply orientations on the frequency parameter of the plate. The current results are verified with those results obtained in the previous work and the new results are presented in tables and graphs.