• 한국초등수학교육학회지
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• 제19권3호
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• pp.267-287
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• 2015

본 논문에서는 2009 개정 초등학교 수학과 교육과정에 따른 교과서에서 취급하는 어림재기 유형 및 전략을 분석하고, 그 결과를 바탕으로, 차후의 교육과정 및 교과서 개발을 위한 시사점으로 다음 네 가지를 제시한다. 첫째, 교육과정과 교과서에서 어림재기 관련 내용을 일치시키는 것이 필요하다. 2009 개정 교육과정에서는 길이, 들이, 무게, 각도의 어림재기만을 제시하고 있다. 그러나 교과서에서는 시간과 넓이의 어림재기도 취급하고 있다. 둘째, 교과서에서 어림재기 전략을 다양하게 안내할 필요가 있다. 지도서에서는 어림재기 전략으로 참조대상 사용하기 전략, 덩어리로 나누기 전략, 단위로 나누기 전략의 세 가지를 예시하고 있지만, 교과서에서는 그렇지 않다. 셋째, '어림하다'의 의미를 명확히 할 필요가 있다. 교과서에서 '어림하다'가 어림재기의 맥락으로만 사용되는 것이 아니다. 넷째, 교육과정에서 시간, 넓이, 부피의 어림재기의 취급 여부를 명확히 할 필요가 있다.

• 정보처리학회논문지D
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• 제16D권3호
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• pp.353-360
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• 2009

대부분의 정보시스템은 컴포넌트 기반으로 아웃소싱에 의해 개발되고 있으며, 개발된 소프트웨어들은 통합되어 유지보수 되고 있다. 그러나 유지보수의 생산성과 효율성 제고를 위한 기반 연구인 비용 측정지표 및 비용 추정 모델에 관한 연구가 부족하다. 본 연구는 컴포넌트 기반의 소프트웨어에 대한 유지보수의 비용에 대한 측정지표를 제안하고, 제안한 측정지표의 의한 컴포넌트 소프트웨어의 유지보수 비용 추정 모델을 연구한다. 컴포넌트 기반의 유지보수 비용 측정지표를 추정하기 위하여 기존에 제시된 지표들을 비교 정리하고, 정리된 측정지표가 컴포넌트 소프트웨어 유지보수 유형에 따라 어떻게 적용되는지를 분류하고 유형별 비용 측정지표를 제안한다. 또, 제안한 측정지표를 이용한 컴포넌트 소프트웨어 유지보수 유형에 따른 비용 추정 모델을 제안한다. 제안한 추정 모델의 사례연구를 실시하여 유효성을 검증한다.

• Smart Structures and Systems
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• 제15권2호
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• pp.489-503
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• 2015

Response estimation at unmeasured locations using the limited number of measurements is an attractive topic in the field of structural health monitoring (SHM). Because of increasing complexity and size of civil engineering structures, measuring all structural responses from the entire body is intractable for the SHM purpose; the response estimation can be an effective and practical alternative. This paper investigates a response estimation technique based on the Kalman state estimator to combine multi-sensor data under non-zero mean input excitations. The Kalman state estimator, constructed based on the finite element (FE) model of a structure, can efficiently fuse different types of data of acceleration, strain, and tilt responses, minimizing the intrinsic measurement noise. This study focuses on the effects of (a) FE model error and (b) combinations of multi-sensor data on the estimation accuracy in the case of non-zero mean input excitations. The FE model error is purposefully introduced for more realistic performance evaluation of the response estimation using the Kalman state estimator. In addition, four types of measurement combinations are explored in the response estimation: strain only, acceleration only, acceleration and strain, and acceleration and tilt. The performance of the response estimation approach is verified by numerical and experimental tests on a simply-supported beam, showing that it can successfully estimate strain responses at unmeasured locations with the highest performance in the combination of acceleration and tilt.

• 한국주거학회:학술대회논문집
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• 한국주거학회 2008년도 춘계학술발표대회 논문집
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• pp.386-392
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• 2008

The purpose of this study is to clarify playground types by characteristics of playground environment in child care facilities, to analyze the needs and estimation of users according to playground types. The subjects of this study were care-givers, who assist outdoor play activities of children and manage safety in playground, to estimate adequateness of playground's environment to children's outdoor plays and to report needs. The data were collected by field measurement survey for clarification playground environments in 21 child care facilities and structured-questionnaire for estimation and needs of 181 care-givers in them. The major results showed the following. 1) The playgrounds were clarified to five type according to number of child and size of playground. The five types include A-type as large-scale facility/small-size playground, B-type as small-scale facility/large-size playground, C-type as small-scale facility/small-size playground, D-type as middle-scale facility/large-size playground, and E-type as large-scale facility/large-size playground. 2) The adequateness of playground environment of D-type were estimate higher than others. C-type were estimated lower than other types in size and outdoor play areas organization of playground. 3) The care-givers in D-type and E-type wanted to install various play equipments, but the care-giver in C-type didn't wanted to install play equipment. 4) The various outdoor play areas were needed in D-type.

• 전력전자학회:학술대회논문집
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• 전력전자학회 2016년도 추계학술대회 논문집
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• pp.59-60
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• 2016

Flooded lead acid batteries are still very popular in the industry because of their low cost as compared to their counterparts. State of Charge (SOC) estimation is of great importance for a flooded lead acid battery to ensure its safe working and to prevent it from over-charging or over-discharging. Different types of Kalman Filters are widely used for SOC estimation of batteries. The values of process and measurement noise covariance of a filter are usually calculated by trial and error method and taken as constant throughout the estimation process. While in practical cases, these values can vary as well depending upon the dynamics of the system. Therefore an Adaptive Unscented Kalman Filter (AUKF) is introduced in which the values of the process and measurement noise covariance are updated in each iteration based on the residual system error. A comparison of traditional and Adaptive Unscented Kalman Filter is presented in the paper. The results show that SOC estimation error by the proposed method is further reduced by 3 % as compared to traditional Unscented Kalman Filter.

• East Asian mathematical journal
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• 제33권2호
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• pp.177-197
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• 2017

The purpose of this study is to investigate and analyze the understandings of elementary pre-service teachers about 'estimation' in the elementary mathematics. Together with this analysis, we identify elementary pre-service teacher's Mathematical Pedagogical Contents Knowledge(MPCK), especially focusing to Subject Matter Knowledge(SMK). In order to this goals, we investigate contents relating to 'estimation' from $1^{st}$ curriculum to 2009 revised curriculum and compare 'rounding up', 'rounding off', 'rounding' in the elementary mathematics textbooks. As results of investigations, 'estimation' has been teaching at the 'Measurement' domain from $3^{rd}$ curriculum, but contexts of measuring weaken from $7^{th}$ curriculum. 'Rounding up(off)' is defined three types in the textbooks from $1^{st}$ to 2009 revised curriculum. And we examine elementary pre-service teachers through the questions on these 'estimation' contents. On the analysis of pre-service teacher's understanding relating MPCK, four themes is summarized as followings; the understanding of '0' in the 'rounding up', the cognitive gap between 'rounding up' and 'rounding off', the difference of percentage of correct answers according to types of question in the 'rounding up', and the difference between the definition of 'rounding up' and the definition of 'rounding'.

• Journal of Astronomy and Space Sciences
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• 제26권1호
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• pp.31-46
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• 2009

An Unscented Kalman Filter (UKF) for estimation of the attitude and rate of a spacecraft using only magnetometer vector measurement is developed. The attitude dynamics used in the estimation is the nonlinear Euler's rotational equation which is augmented with the quaternion kinematics to construct a process model. The filter is designed for small satellite in low Earth orbit, so the disturbance torques include gravity-gradient torque, magnetic disturbance torque, and aerodynamic drag torque. The magnetometer measurements are simulated based on time-varying position of the spacecraft. The filter has been tested not only in the standby mode but also in the detumbling mode. Two types of actuators have been modeled and applied in the simulation. The PD controller is used for the two types of actuators (reaction wheels and thrusters) to detumble the spacecraft. The estimation error converged to within 5 deg for attitude and 0.1 deg/s for rate respectively when the two types of actuators were used. A joint state parameter estimation has been tested and the effect of the process noise covariance on the parameter estimation has been indicated. Also, Monte-Carlo simulations have been performed to test the capability of the filter to converge with the initial conditions sampled from a uniform distribution. Finally, the UKF performance has been compared to that of the EKF and it demonstrates that UKF slightly outperforms EKF. The developed algorithm can be applied to any type of small satellites that are actuated by magnetic torquers, reaction wheels or thrusters with a capability of magnetometer vector measurements for attitude and rate estimation.

• Journal of Radiation Protection and Research
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• 제31권1호
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• pp.17-23
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• 2006

본 연구의 목적은 바이오어쎄이 측정오차의 통계적 분포가 섭취량 추정값에 미치는 영향을 분석하여 오차의 분포를 선정하는데 필요한 기준을 제시하는데 있다. 이를 위하여 본 연구에서는 오차가 정규분포와 대수정규분포를 따른다고 가정한 경우에 대해 최대우도법을 사용하여 섭취량을 평가하였고 그 결과를 서로 비교해 보았다. 본 연구의 결과에 따르면, 검출한도보다 약간 높은 값을 갖는 폐 잔류량 측정결과의 경우 두 분포사이에서의 차는 거의 무시할 수 있을 정도로 작게 나타났다. 그러나 일일 소변 배설률에 대한 측정결과의 경우 오차가 대수정규분포를 따른다고 가정하였을 때의 결과가 정규분포를 따른다고 가정하였을 때의 결과보다 거의 10 % 정도 높게 평가되었다. 이러한 사실로 비추어 볼 때 불착도 요소가 계측통계 오차에 주로 기인되는 경우 오차의 분포가 섭취량 추정값에 거의 영향을 미치지 않는 것으로 사료되나, 불확도 요소에서 그 이외의 오차가 지배적인 경우에는 대수정규분포를 가정하여 섭취량을 추정하는 것이 바람직하다고 판단된다.

• 산업경영시스템학회지
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• 제23권58호
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• pp.113-118
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• 2000

Estimation of the process deviation is an important problem in statistical process control, especially in the control chart, process capability analysis or measurement system analysis. In this paper we suggest the use of the Gini's mean difference for the estimation of the c, the measure of the process deviation through a lots of simulations in various types of distributions. The Gini's mean difference uses the differences of all possible pairs of data. This point will improve the efficiency of estimation. In various classes of distributions, the Gini's mean difference shows good performance, in sense of bias of estimates or mean squared errors.

• 제어로봇시스템학회논문지
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• 제4권1호
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• pp.38-44
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• 1998

The modified maximum likelihood estimation method is used to estimate the nondimensional aerodynamic derivatives of a single turbo-prop aircraft at a specified flight condition for the best deduction of the dynamic characteristics. In wind axes the six degree of freedom equations are algebraically linearized so that the linear state equation contains aerodynamic derivatives in a state-space form and is used in the maximum likelihood method. The simulated data added with the measurement noise is used as a flight test data which is necessary to the estimation of nondimensional aerodynamic derivatives. It is obtained by implementing the 6-DOF nonlinear flight simulation. In the flight simulation, the effects of several control input types, control deflection amplitudes, and the turbulence intensities on the statistical convergence criteria are also examined and quantitative analysis of the results is discussed.