• 대한원격탐사학회지
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• 제33권5_1호
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• pp.547-557
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• 2017

본 연구에서는 탐지하고자 하는 표적신호를 초기 엔드멤버로 하여 Iterative Error Analysis를 통해 배경물질들의 반사 스펙트럼을 순차적으로 엔드멤버로 추출하고, 추출된 엔드멤버들을 이용하여 분광 혼합분석함으로써 표적물질의 분포를 탐지하는 새로운 초분광 표적탐지 기법을 제안한다. 제안된 기법에서는 표적물질에 대한 점유율의 변화가 주어진 문턱값보다 작아질 때 엔드멤버 추출을 위한 반복을 멈추게 된다. 이 기법은 Orthogonal Subspace Projection과 같은 모델 기반 표적 탐지기법들과 달리 사전에 엔드멤버들을 확보해야 할 필요가 없으며, Matched Filter와 같은 확률론적 표적 탐지 기법들과 달리 배경 전체를 하나의 신호로 특징화하지 않기 때문에 표적의 희소성 여부에 의한 영향을 받지 않는다는 장점을 가지고 있다. 실제 항공 초분광 영상자료 및 다양한 인공 표적물질들이 삽입된 모의 초분광 영상자료를 이용한 실험 결과, 제안된 방법이 희소 및 비 희소 표적의 탐지에 매우 효과적임이 확인되었다. 제안된 방법은 표적 물체 탐지뿐만 아니라 광물, 오염물질 등 자원 및 환경 분야에서 다양한 피복 물질을 탐지하는데 효과적으로 사용될 수 있을 것으로 기대된다.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 1994년도 Proceedings of the Korea Automatic Control Conference, 9th (KACC) ; Taejeon, Korea; 17-20 Oct. 1994
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• pp.319-323
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• 1994

In this paper, we discuss a design method of iterative learning control systems for parabolic linear distributed parameter systems(DPSs). First, we discuss some aspects of boundary control of the DPS, and then propose to employ the Karhunen-Loeve procedure to reduce the infinite dimensional problem to a low-order finite dimensional problem. An iterative learning control(ILC) for non-square transfer function matrix is introduced finally for the reduced order system.

• 로봇학회논문지
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• 제17권3호
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• pp.373-380
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• 2022

This paper considers a method of fast correspondence matching for iterative closest point (ICP) algorithm. In robotics, the ICP algorithm and its variants have been widely used for pose estimation by finding the translation and rotation that best align two point clouds. In computational perspectives, the main difficulty is to find the correspondence point on the reference point cloud to each observed point. Jump-table-based correspondence matching is one of the methods for reducing computation time. This paper proposes a method that corrects errors in an existing jump-table-based correspondence matching algorithm. The criterion activating the use of jump-table is modified so that the correspondence matching can be applied to the situations, such as point-cloud registration problems with highly curved surfaces, for which the existing correspondence-matching method is non-applicable. For demonstration, both hardware and simulation experiments are performed. In a hardware experiment using Hokuyo-10LX LiDAR sensor, our new algorithm shows 100% correspondence matching accuracy and 88% decrease in computation time. Using the F1TENTH simulator, the proposed algorithm is tested for an autonomous driving scenario with 2D range-bearing point cloud data and also shows 100% correspondence matching accuracy.

• 한국공간구조학회논문집
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• 제3권4호
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• pp.85-92
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• 2003

In this work, a finite element model is presented for geometrically non-linear analysis of shell structures. Finite element by using a three-node flat triangular shell element is formulated. The non-linear incremental equilibrium equations are formulated by using an updated Lagrangian formulation and the solutions are obtained with the incremental/iterative Newton-Raphson method and arc length method. Some of results are presented for shell structures. The obtained results are in good agreement with the results available in existing literature.

• Advances in nano research
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• 제12권1호
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• pp.37-47
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• 2022

In this paper, the non-linear static analysis of Timoshenko nanobeams consisting of bi-directional functionally graded material (BFGM) with immovable ends is investigated. The scratching in the FG nanobeam mid-plane, is the source of nonlinearity of the bending problems. The nonlocal theory is used to investigate the non-linear static deflection of nanobeam. In order to simplify the formulation, the problem formulas is derived according to the physical middle surface. The Hamilton principle is employed to determine governing partial differential equations as well as boundary conditions. Moreover, the differential quadrature method (DQM) and direct iterative method are applied to solve governing equations. Present results for non-linear static deflection were compared with previously published results in order to validate the present formulation. The impacts of the nonlocal factors, beam length and material property gradient on the non-linear static deflection of BFG nanobeams are investigated. It is observed that these parameters are vital in the value of the non-linear static deflection of the BFG nanobeam.

• Journal of applied mathematics & informatics
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• 제29권5_6호
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• pp.1167-1178
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• 2011

In this paper, we further investigate the local Hermitian and skew-Hermitian splitting (LHSS) iteration method and the modified LHSS (MLHSS) iteration method for solving generalized nonsymmetric saddle point problems with nonzero (2,2) blocks. When A is non-symmetric positive definite, the convergence conditions are obtained, which generalize some results of Jiang and Cao [M.-Q. Jiang and Y. Cao, On local Hermitian and Skew-Hermitian splitting iteration methods for generalized saddle point problems, J. Comput. Appl. Math., 2009(231): 973-982] for the generalized saddle point problems to generalized nonsymmetric saddle point problems with nonzero (2,2) blocks. Numerical experiments show the effectiveness of the iterative methods.

• 한국전산구조공학회:학술대회논문집
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• 한국전산구조공학회 2002년도 봄 학술발표회 논문집
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• pp.335-342
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• 2002

A continuum-based design sensitivity analysis (DSA) method fur non-shape problems is developed for geometrically nonlinear elastic structures. The non-shape problem is characterized by the design variables that are not associated with the domain of system like sizing, material property, loading, and so on. Total Lagrangian formulation with the Green-Lagrange strain and the second Piola-Kirchhoff stress is employed to describe the geometrically nonlinear structures. The spatial domain is discretized using the 4-node isoparametric plane stress/strain elements. The resulting nonlinear system is solved using the Newton-Raphson iterative method. To take advantage of the derived analytical sensitivity In topology optimization, a fast and efficient design sensitivity analysis method, adjoint variable method, is employed and the material property of each element is selected as non-shape design variable. Combining the design sensitivity analysis method and a gradient-based design optimization algorithm, an automated design optimization method is developed. The comparison of the analytical sensitivity with the finite difference results shows excellent agreement. Also application to the topology design optimization problem suggests a very good insight for the layout design.

• 대한전자공학회논문지TC
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• 제45권12호
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• pp.105-113
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• 2008

유비쿼터스 사회에서는 사용자의 요구를 충족시키기 위하여 사용자가 갖고 있는 기기에 대한 정밀한 위치측정을 필요로 한다. 위치 측정은 송수신기간에 신호의 전송을 기반으로 한 거리측정을 통해 이뤄지기 때문에 위치측정의 오차는 거리측정의 오차로부터 발생한다. 신호가 전송되는 기기 간에 장애물이 존재하게 되면 LoS(Line of Sight)신호 성분이 줄어들게 되어 NLoS(Non-Line of Sight) 채널이 발생하게 되고 정확한 시점에서 신호를 검출할 수 없게 되어 거리오차가 발생하게 된다. 일반적인 위치측정 알고리즘은 참조기기(Reference Device)의 거리측정 성능에 관계없이 참조기기와 목표기기(Target Device)간의 거리측정 값을 위치 계산에 그대로 사용하기 때문에 거리측정 값으로부터 발생되는 오차가 위치 계산에 더해지게 된다. 따라서 본 논문에서는 각 참조기기가 속해 있는 채널특성을 판별하고 NLoS채널로부터 계산된 거리와 LoS채널로부터 계산된 거리를 다른 비율로 적용하여 위치측정의 오차를 줄이는 Iterative Calculation 기법을 제안한다. 참조기기는 수신된 신호의 Kurtosis, Mean, Excess Delay, RMS Delay spread를 통해 NLoS와 LoS 채널을 구분한다. 이를 통해 구분된 채널마다 각기 다른 비율로 랜덤 거리를 계산된 거리에 더하여 위치를 계산하는 것을 반복적으로 수행한 뒤 평균값을 계산하여 확률적으로 존재할 가능성이 높은 목표기기의 위치를 찾아감으로써 NLoS채널로부터 계산된 거리오차가 위치측정에 미치는 영향을 줄이는 방법을 제안하고 시뮬레이션을 통해 기존의 방식과 비교했을 때 성능향상을 확인하였다.

• Journal of Ship and Ocean Technology
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• 제11권2호
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• pp.10-25
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• 2007

With the sharp increase of the oil price, the issue of the energy saving requires even higher propulsive efficiency of the propellers. Traditionally the propellers have been designed with the criteria such as that of Lerbs optimum based on the lifting line theory and the empirical formulae of Lerbs and van Manen giving relations of the wake pitch with the wake non-uniformity. With the aid of the high speed computer, it is now possible to apply the time-consuming iterative approaches for the solution of the lifting surface problems. In this paper we formulate the variational problem to optimize the efficiency of the propeller operating in the given ship wake using the lifting surface method. The variational formulation relating the spanwise circulation distribution with the propulsive efficiency to be maximized is however non-linear in circulation distribution functions, thus the iterative method is applied to the quasi-linearized equations. The blade shape design also requires the iterative procedures, because the shape of the blade which is represented by the lifting surface is unknown a priori. The numerical code was validated with the DTNSRDC propeller 4119 which is well-known to be optimum in uniform inflow condition. In addition existing (well-designed) commercial propellers were selected and compared with the results of the open water tests and the self-propulsion tests.

• 한국공작기계학회:학술대회논문집
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• 한국공작기계학회 1999년도 춘계학술대회 논문집
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• pp.141-146
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• 1999

A new method, so called MMA(Method of Moving Asymptotes) was applied to the optimization problems of non-linear functions and non-linear structures. In each step of the iterative process, tile MMA generates a strictly convex approximation subproblems and solves them by using the dual problems. The generation of these subproblems is controlled by so called 'moving asymptotes', which may both make no oscillation and speed up tile convergence rate of optimization process. By contrast in generalized dual function, the generated function by MMA is always explicit type. Both the objective and behaviour constraints which were approximated are optimized by dual function. As the results of some examples, it was found that this method is very effective to obtain the global solution for problems with many local solutions. Also it was found that MMA is a very effective approximate method using the original function and its 1st derivatives.