• 대한정형외과학회지
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• 제56권6호
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• pp.525-529
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• 2021

건활막 거대세포종은 관절 내에 드물게 발생하는 병변으로 양측 슬관절 내에 발생하는 경우는 국소형보다는 미만형에서 많은 것으로 알려져 있다. 따라서 양측 슬관절 내에 발생한 국소형 건막 거대세포종을 보고하는 문헌은 제한되어 있으며 특히 슬개대퇴간 동통을 초래한 양측에 발생한 국소형 건활막 거대세포종의 국내 보고는 없었다. 저자들은 양측 슬관절 전방부의 동통을 초래한 건활막 거대세포종 증례를 관절경하에서 절제 후 병리학적으로 확진 하였으며 임상적으로 좋은 결과를 보였기에 문헌고찰과 함께 보고하고자 한다.

• 항공우주정책ㆍ법학회지
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• 제26권1호
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• pp.177-213
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• 2011

현재 우주활동에 의하여 발생된 손해에 대한 배상책임과 관련된 국제조약으로 1967년 우주조약과 1972년 우주손해배상책임조약이 있으며, 또한 우리나라 국내법으로 2008년 우주손해배상법이 있다. 우주조약은 우주활동에 대한 국가의 국제적 책임과 우주물체에 의한 손해에 대한 국가의 불법행위 책임에 관하여 규정하고 있다. 우주손해책임조약은 발사국의 절대적 책임, 과실책임, 연대책임, 배상청구권자, 배상청구방법, 배상청구기한, 배상청구와 국내적 구제, 손해배상액, 청구위원회 설치 등에 관하여 규정하고 있다. 우리나라 우주손해배상법은 우주손해의 정의, 우주손해책임조약과의 관계, 발사자의 무과실책임 및 책임의 집중, 발사자의 손해배상책임한도액, 발사자의 책임보험 가입, 정부의 피해자 구조 및 발사자 지원 등에 관하여 규정하고 있다. 우주사고로 인한 손해배상책임 관련 사례들로 Iridium33과 Cosmos 2251 위성충돌 사건, Cosmos 954 위성추락 사건, Martin Marietta의 위성발사 실패 사건, Westar VI 위성 작동불량 사고 등이 있으며, 이러한 우주사건에 관한 분쟁 또는 소송에 있어서 위성의 발사국, 발사자 및 제조자의 손해배상책임 부담문제에 관련하여 절대책임(엄격책임)원칙 또는 과실책임원칙이 적용되어 해결되고 있다. 우주손해책임조약의 개선방안으로 손해배상청구권자의 명확한 규정, 청구위원회의 결정의 구속력 확보 등을 들 수 있고, 우리나라 우주손해배상법의 개선방안으로 손해배상범위에 간접손해 포함, 손해배상책임 한도액의 통화단위 변경, 공동발사자의 연대책임 및 구상권 신설, 우주손해배상심의위원회의 설치 등을 들 수 있다. 우리나라는 2009년 6월 전남 고흥군 외나로도에 우주센터가 준공되어 동년 8월 및 2010년 6월 우리나라 최초 소형 우주발사체 나로호(KSLV-1)를 두차례 발사하였다. 향후 우리나라는 우주활동 과정에서 우주관련 국제조약 및 국내법상의 국제적 책임 및 우주손해에 대한 배상책임 등 문제들이 발생할 가능성이 있으므로 우리정부 및 우주물체 발사기관은 이러한 문제들에 대한 법적 제도적 대응책을 마련해야 할 것이다.

• International Journal of Control, Automation, and Systems
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• 제3권3호
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• pp.411-418
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• 2005

This paper discusses an output-tracking control design method for Takagi-Sugeno fuzzy systems with parametric uncertainties. We first represent the concerned system as a set of uncertain linear systems. The tracking problem is then converted into a stabilization problem thereby leading to a more feasible control design procedure. A sufficient condition for robust practical output tracking is derived in terms of a set of linear matrix inequalities. A numerical example for a flexible-joint robot-arm model has been demonstrated, to convincingly show effectiveness of the proposed system modeling and control design.

• International Journal of Control, Automation, and Systems
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• 제3권3호
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• pp.453-460
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• 2005

In this paper, a prototype Cartesian Parallel Manipulator (CPM) is demonstrated, in which a moving platform is connected to a fixed frame by three PRRR limbs. Due to the orthogonal arrangement of the three prismatic joints, it behaves like a conventional X-Y-Z Cartesian robot. However, because all the linear actuators are mounted at the fixed frame, the manipulator may be suitable for applications requiring high speed and accuracy. Using a geometric method and the practical assumption that three revolute joint axes in each limb are parallel to one another, a simple forward kinematics for an actual model is derived, which is expressed in terms of a set of linear equations. Based on the error model, two calibration methods using full position and length measurements are developed. It is shown that for a full position measurement, the solution for the calibration can be obtained analytically. However, since a ball-bar is less expensive and sufficiently accurate for calibration, the kinematic calibration experiment on the prototype machine is performed by using a ball-bar. The effectiveness of the kinematic calibration method with a ball-bar is verified through the well­known circular test.

• International Journal of Automotive Technology
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• 제3권4호
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• pp.157-163
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• 2002

It is well recognized that the ultrasonic method is one of the most common and reliable nondestructive testing (NDT) methods for the quantitative estimation of defects in welded structures. However, NDT techniques applying for adhesively bonded joints have not been clearly established yet. In this paper, the detection of interface crack by the ultrasonic method was applied for the measurement of interfacial crack length in the adhesively bonded joints of double-cantilever beam (DCB). An optimal condition of transmission coefficients and experimental accuracy by the ultrasonic method in the adhesively bonded joints have been investigated and discussed. The experimental values are in good agreement with the computed results by boundary element method (BEM) and Ripling's equation.

• International Journal of Automotive Technology
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• 제6권3호
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• pp.285-291
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• 2005

In this paper, the author proposes a fatigue damage parameter of spot welded joints under proportional loading. The proposed fatigue damage parameter is developed based on von Mises' equivalent stress and local structural stress at the edge of spot weld nugget. The structural stress at the edges of the weld nugget in each sheet is calculated using the forces and moments that are determined by finite element analysis. A structural equivalent stress is then calculated by von Mises' equivalent stress equation. The structural equivalent stresses are correlated to experimental fatigue life of the spot welded joints. The proposed parameter is evaluated with fatigue test data of spot welds subjected to multi axial and tensile-shear loads. Sheppard's parameter and Rupp and co-workers' parameter are also evaluated with the same test data to compare with the author's parameter. This proposed parameter presents a better correlation with experimental fatigue data than those of Sheppard's and Rupp and co-workers' parameter. The proposed parameter should be very effective for durability calculations during the early design phase since coarsely meshed finite element models can be employed.

• International Journal of Automotive Technology
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• 제7권7호
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• pp.833-839
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• 2006

In this paper, roll behavior of three planar half car models are compared. The first model is a simple model whose contact point between a wheel and the ground is assumed to be fixed with a revolute joint. The second model is a modified model of the fIrst model, whose wheel tread width can vary. In this model, the instant center of a wheel with respect to the ground, which is crucial to find the roll center, is assumed to be at the contact point of a wheel and the ground. The last model uses the pole of a wheel with respect to the ground for small displacement as the instant center of a wheel with respect to the ground. Loci of the center of gravity point, the fixed and the moving centrodes which are traces of roll center position in the ground and the body frame respectively, wheel contact points, and instant centers of a wheel with respect to the ground are calculated.

• International Journal of Automotive Technology
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• 제5권4호
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• pp.303-309
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• 2004

In this paper, an interfacial crack length has been detected by using the ultrasonic attenuation coefficient on the adhesively bonded double-cantilever beam (DCB) joints. The correlations between energy release rates which were investigated by experimental measurement, the boundary element method (BEM) and Ripling's equation are compared with each other. The experimental results show that the interfacial crack length for the ultrasonic attenuation coefficient and energy release rate increases proportionally. From the experimental results, we propose a method to detect the interfacial crack length by using the ultrasonic attenuation coefficient and discuss it.

• International Journal of Precision Engineering and Manufacturing
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• 제4권1호
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• pp.43-48
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• 2003

A linear laser-vision sensor called ‘Perception TriCam Contour' is mounted on an industrial robot and often used for various application of the robot such as the position correction and the inspection of a part. In this paper, a sensor center position calibration is presented for the most accurate use of the robot-Perceptron system. The obtained algorithm is suitable for on-site calibration in an industrial application environment. The calibration algorithm requires the joint sensor readings, and the Perceptron sensor measurements on a specially devised jig which is essential for this calibration process. The algorithm is implemented on the Hyundai 7602 AP robot, and Perceptron's measurement accuracy is increased up to less than 1.4mm.

• International Journal of Aeronautical and Space Sciences
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• 제18권1호
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• pp.63-69
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• 2017

In this paper, composite laminate pull-through resistance was analyzed using the FEM method and compared with test results. 2D and 3D simplified FEM models, a nonlinear analysis, and a progressive failure analysis utilizing three composite laminate failure theories Maximum Stress, Maximum Strain, and Tsai-Wu were used to predict the FEM results with the test results. The load and boundary conditions of the test were applied to the FEM to simulate the test. A composite laminate pull-through test (ASTM D7332 Proc. B) was designed with a special fixture to collect more precise data. The test results were compared with the FEM analysis results.