• 융합보안논문지
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• 제8권4호
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• pp.161-166
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• 2008

본 논문은 3차원 모델 표면의 특징 곡률(Feature Curvature) 정보를 이용하여 3차원 거리정보 데이터(Range Image)를 자동으로 정합하는 효율적인 방법을 제안하고 그 성능을 분석하였다. 제안한 알고리즘은 3차원 데이터에 대한 거리정보의 물리적 특성인 가우스 곡률(Gaussian Curvature)을 이용하여 모델의 특징점을 검출하고, 공분산 행렬(Covariance Matrix)을 이용하여 각 데이터의 지역좌표계(Local Coordinate System) 사이의 변위를 계산한다. 3차원 형상 취득장치의 카메라 위치는 3차원 데이터와 투영된 2차원 영상과의 사영행렬(Projection Matrix) 관계식으로 계산한다. 결론부분에서는 실험결과를 기존 연구방법과 비교하여 제안된 방법이 더 빠르고 정확하게 정합하는 결과를 보임으로써 3차원 물체인식이나 모델링에 응용성을 제시하였다.

• Wind and Structures
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• 제18권1호
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• pp.37-56
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• 2014

The evaluation of pressure fields acting on slender structures under wind loads is currently performed in experimental aerodynamic tests. For wind-sensitive structures, in fact, the knowledge of global and local wind actions is crucial for design purpose. This paper considers a particular slender structure under wind excitation, representative of most common high-rise buildings, whose experimental wind field on in-scale model was measured in the CRIACIV boundary-layer wind tunnel (University of Florence) for several angles of attack of the wind. It is shown that an efficient reduced model to represent structural response can be obtained by coupling the classical structural modal projection with the so called blowing modes projection, obtained by decomposing the covariance or power spectral density (PSD) wind tensors. In particular, the elaboration of experimental data shows that the first few blowing modes can effectively represent the wind-field when eigenvectors of the PSD tensor are used, while a significantly larger number of blowing modes is required when the covariance wind tensor is used to decompose the wind field.

• International Journal of Aeronautical and Space Sciences
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• 제1권1호
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• pp.70-80
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• 2000

The attitude knowledge error model is formulated for specifically KOMPSAT attitude determination system using the Lefferts/Markley/Shuster method, and the attitude determination(AD) error analysis is performed so as to investgate the on-board attitude determination capability of KOrea Multi-Purpose SATellite(KOMPSAT) using the covariance analysis method. Analysis results show there is almost no initial value effect on Attitude Determination (AD) error and the sensor noise effects on AD error are drastically decreased as is predicted because of the inherent characteristic of Kalman filter structure. However, it shows that the earth radiance effect of IR-sensor(earth sensor) and the bias effects of both IR-sensor and fine sun sensor are the dominant factors degrading AD error and gyro rate bias estimate error in AD system. Analysis results show that the attitude determination errors of roll, pitch and yaw axes are 0.056, 0.092 and 0.093 degrees, respectively. These numbers are smaller than the required values for the normal mission of KOMPSAT. Also, the selected on-orbit data of KOMPSAT is presented to demonstrate the designed AD system.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 1993년도 한국자동제어학술회의논문집(국내학술편); Seoul National University, Seoul; 20-22 Oct. 1993
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• pp.64-69
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• 1993

In this paper we present the performance bounds of the optimal FIR filter in continuous time systems with modeling uncertainty. The performance measure bounds are calculated from the estimation error covariance bounds of the optimal FIR filter and the suboptimal FIR filter. Performance error bounds range are expressed by the upper bounds on the estimation error covariance difference between the real and nominal values in case of the systems with noise uncertainty or model uncertainty. The performance bounds of the systems are derived on the assumption that the system uncertainty and the estimation error covariance are imperfectly known a priori. The estimation error bounds of the optimal FIR filter is compared with those of the Kalman filter via a numerical example applied to the estimation of the motion of an aircraft carrier at sea, which shows the former has better performances than the latter.

• 한국음향학회지
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• 제11권1호
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• pp.67-79
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• 1992

적응방식이나 실시간 처리에 적합한 온라인 ARMA 계수추정을 위하여 공분산형 ARMA 고속 transversal 필터 알고리즘을 제안하였다. 제안된 알고리즘은 ARMA 모델의 경우 상관함수 행렬의 이동불변 특성이 각 블록 별로 만족함을 이용하여 ELS(Extended Least Squares)를 공분산형의 경우에 대해 고속 시갱신 알고리즘으로 구현한 것으로서, 알고리즘의 유도에는 사영연산자를 이용한 기하학적 접근방식을 사용하였다. 제안된 알고리즘은 13N+37 MADPR의 연산량을 필요로 하며, AR부분과 MA부분의 차수를 달리할 수 있다.

• 한국음향학회지
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• 제15권1호
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• pp.34-39
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• 1996

표적 상태추정은 소나 신호처리의 중요한 문제이다. 본 연구에서는 모노펄스 소나의 표적정보를 이용한 표적 상태추정에 공분산 해석기법을 적용하여 상태추정 성능을 향상시켰다. 앞서 개발된 MOST신호 합성기법으로 모의 표적신호를 발생시켜 신호대 잡음비의 변화에 따른 조건에서 제시된 기법의 성능을 평가하였다.

• Structural Engineering and Mechanics
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• 제56권5호
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• pp.767-785
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• 2015

The stochastic finite element method is employed to obtain a stochastic dynamic model of angled beams subjected to impact loads when uncertain material properties are described by random fields. Using the perturbation technique in conjunction with a precise time integration method, a random analysis approach is developed for efficient analysis of random elastic waves. Formulas for the mean, variance and covariance of displacement, strain and stress are introduced. Statistics of displacement and stress waves is analyzed and effects of bend angle and material stochasticity on wave propagation are studied. It is found that the elastic wave correlation in the angled section is the most significant. The mean, variance and covariance of the stress wave amplitude decrease with an increase in bend angle. The standard deviation of the beam material density plays an important role in longitudinal displacement wave covariance.

• Transactions on Electrical and Electronic Materials
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• 제17권1호
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• pp.13-17
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• 2016

The ampere-hour integral method and the open circuit voltage method are integrated via the extended Kalman filter method so as to overcome insufficiencies of the ampere-hour integral method and the open circuit voltage method for estimating battery SOC. The process noise covariance and the measurement noise covariance of the extended Kalman filter method are simplified based on the Thevenin equivalent circuit model, with a proposed simplified SOC estimating method. Verification of DST experiments indicated that the battery SOC estimating method is simple and feasible, and the estimated SOC error is no larger than 2%.

• 응용통계연구
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• 제5권2호
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• pp.283-292
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• 1992

개인용 컴퓨터의 보급이 급격히 늘어남에 따라 자료의 통계분석에 개인용 컴퓨터가 많이 이용되고 있다. 컴퓨터의 하드웨어가 하루가 다르게 발전하고 있음으로 웬만큼 많은 양의 자료를 분석하는 데에는 컴퓨터의 기억용량이나 처리속도등이 문제되지는 않는다. 자료가 축차적(sequentially)으로 주어질 때 어떤 통계량을 계산하기 위하여 매번 전체 자료를 다시 읽어야 한다면 이는 번거로운 작업이 될 것이며 기억용량의 낭비임에 틀림없다. 이러한 문제점을 S/W 적인 입장에서 해결하고자 하는 노력이 바로 갱신 알고리즘(Updating Algorithm)이다. 이 연구에서는 몇가지 통계량에 대한 갱신 알고리즘들을 알아보고 그들의 특성을 밝힘으로써 소형 및 개인용 컴퓨터를 이용하여서도 많은 양의 자료분석이 가능하도록 하고자 한다.

• 제어로봇시스템학회논문지
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• 제12권2호
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• pp.93-100
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• 2006

In this paper, a new-type Extended Kalman Filter (EKF) is proposed as a robust nonlinear filter for a stochastic nonlinear system. The original EKF is widely used for various nonlinear system applications. But it is fragile to its estimation errors because they give rise to linearization errors that affect the system mode1 as the modeling errors. The linearization errors are nonlinear functions of the estimation errors therefore it is very difficult to obtain the accurate error covariance of the EKF using the linear form. The inaccurately estimated error covariance hinders the EKF from being a sub-optimal estimator. The proposed filter tries to obtain the upper bound of the error covariance tolerating the uncertainty of the error covariance instead of trying to obtain the accurate one. It treats the linearization errors as uncertain modeling errors that can be handled by the robust linear filtering. In order to be more robust to the estimation errors than the original EKF, the proposed filter minimizes the upper bound like the robust linear filter that is applied to the linear model with uncertainty. The in-flight alignment problem of the inertial navigation system with GPS position measurements is a good example that the proposed robust filter is applicable to. The simulation results show the efficiency of the proposed filter in the robustness to initial estimation errors of the filter.