• 한국항공우주학회지
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• 제38권3호
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• pp.207-212
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• 2010

본 논문에서는 고정익 무인항공기의 그물망 자동착륙을 위한 나선형 강하궤적과 종말 유도기법을 설계하였다. 시야가 확보된 좁은 지역에서 착륙하도록 고정익 항공기의 나선형 강하궤적을 설계하였고, 나선형 강하의 끝점에서 그물망 입사방향을 향하도록 비행경로각 명령을 생성하였다. 종말유도 단계에서는 그물망 중심으로의 정밀한 유도를 위하여 시선각 정보 기반 의사추적 유도기법을 설계하였다. 고정익 무인항공기의 시스템 인식 모델을 이용한 6자유도 수치 시뮬레이션을 수행하여 제안한 나선형 착륙비행의 성능을 검증하였다.

• 치위생과학회지
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• 제8권3호
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• pp.169-173
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• 2008

본 연구는 2007년 3월10일부터 2007년 6월3일까지 충남 당진에 위치한 S대학 치위생과 3학년들의 치면세마 실습환자 248명을 대상으로 치간칫솔 사용에 따른 치면세균막 제거효과를 비례오즈모형(proportional odds models)을 사용하여 분석한 결과 다음과 같은 결론을 얻었다. 1. 비례오즈모형의 적합도는 자유도가 3인 1.2552이고 p값이 .7398로 비례오즈모형이 적절함을 의미하고 치면세균막 제거효과와 치간칫솔 사용의 독립성문제는 $H_0:{\beta}=0$에 대한 검정으로 검정통계량은 자유도가 1인 15.5496이고 p 값은 <.0001 이다. 이는 치면세균막 제거 효과와 치간칫솔의 사용은 매우 연관성이 높음을 의미한다. 2. 모형의$\beta$에 대한 ML추정치는 $\hat{\beta}=1.2493$(ASE = 0.3207)임을 알 수 있고 반응이 매우 불량이다 보다는 매우 양호하다 에 속할(이를 라 표현할 수 있다) 경향은 치간칫솔을 사용하지 않는다. 라는 반응에 비해 치간칫솔을 사 용한다. 라는 경향이 추정오즈비 exp(1.2493) = 3.49배 높다. 3. 비례오즈모형의 추정반응은 치간칫솔을 사용한다. 라는 반응이 매우양호와 양호한 치면세균막 제거효과에 속할 추정(누적)확률은 0.38(0.50)이다.

• 한국농공학회지
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• 제38권3호
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• pp.82-91
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• 1996

This is a basic study for the static and dynamic analysis on the elasto-plastic and elasto-viscoplastic of an axi-symmetric shell. The objective of this study was to investigate the mechanical characteristics of a nuclear reinforced concrete containment structure, which was selected as a model, by a numerical analysis using a finite element method. The structure was modeled with discrete ring elements of 8-noded isoparametric element rotating against the symmetrical axis, and the interaction between the foundation and the structure was modeled by Winkler's model. Also, the meridional tendon was modeled with 2-node truss elements, and the hoop tendon was done with point elements in two degrees of freedom. The effect of the tendon was considered without the increasement in total degree of freedom as the stiffness matrix of modeled tendon elements was assembled on the stiffness matrix of ring elements linked with the tendon. The results obtained from the analysis of an example were summarized as follows : 1. The stresses in the hoop direction on the interior and exterior surfaces of the structure were shown in changes of similar trend, and high stresses appeared on the structure wall 2. The stresses in the meridional direction on the interior and exterior surfaces were shown in change of different trend. Especially, the stresses at the junctions between the dome and the wall and between the wall and the bottom plate of the structure were very high, compared with those at other parts of the structure. 3. The stress changes in the direction of thickness on the crown of the dome were much linearly distributed. However, as the amount of tendon increased, the stresses in the upper and lower parts of the wall established with the tendon were shown stress concentration. 4. The stress changes in the direction of thickness on the center of the structure wall was linearly distributed in the all cases, and special stress due to the use of the tendon was not shown.

• Advances in Computational Design
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• 제8권1호
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• pp.1-12
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• 2023

To consider the effects of the increasing speed of next-generation high-speed trains, the existing traffic safety code for railway bridges needs to be improved. This study suggests a numerical method of evaluating the new effects of this increasing speed on railway bridges. A prestressed concrete (PSC) box bridge with a 40 m span length on the Gyeongbu track sector is selected as a representative example of high-speed railway bridges in Korea. Numerical models considering the inertial mass forces of a 38-degree-of-freedom train and the interaction forces with the bridge as well as track irregularities are presented in detail. The vertical deflections and accelerations of the deck are calculated and compared to find the new effects on the bridge arising with increasing speed under simply and continuously supported boundary conditions. The ratios between the static and dynamic responses are calculated as the dynamic amplification factors (DAFs) under different running speeds to evaluate the traffic safety. The maximum deflection and acceleration caused by the running speed are indicated, and regression equations for predicting these quantities based on the speed are also proposed.

• Journal of Power Electronics
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• 제4권1호
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• pp.28-38
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• 2004

In this paper, the position control of a detuned indirect field oriented control (IFOC) induction motor drive is studied. A proposed Simple-Neuro-Controllers (SNCs) are designed and analyzed to achieve high-dynamic performance both in the position command tracking and load regulation characteristics for robotic applications. The proposed SNCs are trained on-line based on the back propagation algorithm with a modified error function. Four SNCs are developed for position, speed and ｄ-ｑ axes stator currents respectively. Also, a synchronous proportional plus integral-derivative (PI-D) two-degree-of-freedom (2DOF) position controller and PI-D speed controller are designed for an ideal IFOC induction motor drive with the desired dynamic response. The performance of the proposed SNCs and synchronous PI-D 2DOF position controllers for detuned field oriented induction motor servo drive is investigated. Simulation results show that the proposed SNCs controllers provide high-performance dynamic characteristics which are robust with regard to motor parameter variations and external load disturbance. Furthermore, comparing the SNC position controller with the synchronous PI-D 2DOF position controller demonstrates the superiority of the proposed SNCs controllers due to attain a robust control performance for IFOC induction motor servo drive system.

• Structural Engineering and Mechanics
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• 제38권1호
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• pp.39-63
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• 2011

Referring to the formulation of physical stochastic optimal control of structures and the scheme of optimal polynomial control, a nonlinear stochastic optimal control strategy is developed for a class of structural systems with hysteretic behaviors in the present paper. This control strategy provides an amenable approach to the classical stochastic optimal control strategies, bypasses the dilemma involved in It$\hat{o}$-type stochastic differential equations and is applicable to the dynamical systems driven by practical non-stationary and non-white random excitations, such as earthquake ground motions, strong winds and sea waves. The newly developed generalized optimal control policy is integrated in the nonlinear stochastic optimal control scheme so as to logically distribute the controllers and design their parameters associated with control gains. For illustrative purposes, the stochastic optimal controls of two base-excited multi-degree-of-freedom structural systems with hysteretic behavior in Clough bilinear model and Bouc-Wen differential model, respectively, are investigated. Numerical results reveal that a linear control with the 1st-order controller suffices even for the hysteretic structural systems when a control criterion in exceedance probability performance function for designing the weighting matrices is employed. This is practically meaningful due to the nonlinear controllers which may be associated with dynamical instabilities being saved. It is also noted that using the generalized optimal control policy, the maximum control effectiveness with the few number of control devices can be achieved, allowing for a desirable structural performance. It is remarked, meanwhile, that the response process and energy-dissipation behavior of the hysteretic structures are controlled to a certain extent.

• 한국항공우주학회지
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• 제38권3호
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• pp.274-279
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• 2010

본 논문에서는 원 형상에 비해 20% 축소 설계된 수평 핀을 부착한 전투기의 외부 연료 탱크의 정적인 세로 안정성을 해석하고 투하궤적을 분석하였다. 얇은 에어포일의 공력 자료를 이용하여 연료 탱크의 정적 피칭 안정성을 해석한 결과는 풍동 실험 결과와 거의 일치하였다. 연료탱크의 6자유도 운동방정식에 대한 수치적인 모사에서 얻은 낙하 궤적을 실제 모델의 투하 실험 궤적과 비교 분석한 결과 투하 시 항공기의 자세가 연료 탱크의 수직 이동 궤적에는 영향을 미치지 않지만 수평 이동 궤적에는 상당한 영향을 미치게 됨을 알 수 있었다. 이와 같은 이론 해석 및 실험 결과의 분석을 통해 재설계 핀을 부착한 외부 연료 탱크를 비행 중 항공기로 부터 분리할 때 비행운용 규범을 기준으로 수행한다면 항공기의 안전성을 보장할 수 있음이 검증되었다.

• Journal of Gastric Cancer
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• 제21권1호
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• pp.38-48
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• 2021

Purpose: As the number of gastric cancer survivors is increasing and their quality of life after surgery is being emphasized, single-port surgery is emerging as an alternative to conventional gastrectomy. A novel multi-degree-of-freedom (DOF) articulating device, the ArtiSential® device (LivsMed, Seongnam, Korea), was designed to allow more intuitive and meticulous control for surgeons facing ergonomic difficulties with conventional tools. In this study, we evaluated the feasibility of this new device during single-port laparoscopic distal gastrectomy (SP-LDG) for early gastric cancer (EGC) patients. Materials and Methods: Consecutive patients diagnosed with EGC who underwent SP-LDG with ArtiSential® (LivsMed) graspers between April 2018 and August 2020 were enrolled in the study. The clinical outcomes were compared with those of a control group, in which prebent graspers (Olympus Medical Systems Corp) were used for the same procedures. Results: Seventeen patients were enrolled in the ArtiSential® group. There was no significant difference in operative time (205.4±6.0 vs. 218.1±9.9 minutes, P= 0.270) or the quality of surgery, in terms of the number of retrieved lymph nodes (49.5±3.5 vs. 45.9±4.0, P=0.473), length of hospital stay (15.4±2.0 vs. 12.4±1.3 days, P=0.588), and postoperative complications (40.0% vs. 41.2%, P=0.595), between the ArtiSential® group and the control group. Conclusions: The new multi-DOF articulating grasper is feasible and can be used as an alternative for prebent graspers during SP-LDG.

• 한국전산유체공학회지
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• 제10권2호
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• pp.38-47
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• 2005

Substructuring methods are often used in finite element structural analyses. In this study a multi-level substructuring(MLSS) algorithm is developed and proposed as a possible candidate for finite element fluid solvers. The present algorithm consists of four stages such as a gathering, a condensing, a solving and a scattering stage. At each level, a predetermined number of elements are gathered and condensed to form an element of higher level. At the highest level, each sub-domain consists of only one super-element. Thus, the inversion process of a stiffness matrix associated with internal degrees of freedom of each sub-domain has been replaced by a sequential static condensation of gathered element matrices. The global algebraic system arising from the assembly of each sub-domain matrices is solved using a well-known iterative solver such as the conjugare gradient(CG) or the conjugate gradient squared(CGS) method. A time comparison with CG has been performed on a 2-D Poisson problem. With one domain the computing time by MLSS is comparable with that by CG up to about 260,000 d.o.f. For 263,169 d.o.f using 8 x 8 sub-domains, the time by MLSS is reduced to a value less than $30\%$ of that by CG. The lid-driven cavity problem has been solved for Re = 3200 using the element interpolation degree(Deg.) up to cubic. in this case, preconditioning techniques usually accompanied by iterative solvers are not needed. Finite element formulation for the incompressible flow has been stabilized by a modified residual procedure proposed by Ilinca et al.[9].

• 한국시뮬레이션학회논문지
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• 제27권1호
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• pp.33-38
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• 2018

본 연구에서는 선유도 중어뢰의 전술 효과도 예측을 위하여 개발한 교전수준 시뮬레이터에 대해서 시뮬레이터 개발에 적용된 개념 및 구성요소 모델에 대해서 소개하고 있다. 특히 어뢰의 공격문제 해결을 위하여 기하학적 모델에 따른 해(Closed-form solution)를 도출하였고, 어뢰의 공격유도 방법에 비례항법 유도를 적용하여 구현하였다. 표적함에 대해서는 속도와 소음의 상충관계로 인한 피탐 가능성을 고려하였다. 어뢰의 초기위치에 따른 공격 소요 시간을 계산하고 이를 도시화하는 과정을 통하여 도출된 해의 정확성을 확인 할 수 있었고, 현실적인 공격유도 방법 및 소음원 모사를 통하여 시뮬레이터 충실도를 높일 수 있었다. 시뮬레이터는 다양한 전술상황을 가정하여 결과를 분석 할 수 있도록 자유도가 높게 개발되었으며, 구성요소 궤적 분석 및 전방위 요격 성공률 분석이 가능하여 전장 상황의 흐름을 파악하고 전술에 대한 이해를 높이는데 도움이 된다.