• 제목/요약/키워드: Accuracy averaging effect

검색결과 17건 처리시간 0.023초

시계열 데이터의 프라이버시 보호 클러스터링에서 노이즈 평준화 효과 (Noise Averaging Effect on Privacy-Preserving Clustering of Time-Series Data)

  • 문양세;김혜숙
    • 한국정보과학회논문지:컴퓨팅의 실제 및 레터
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    • 제16권3호
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    • pp.356-360
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    • 2010
  • 최근, 개인 데이터의 프라이버시 보호에 대한 문제가 대두됨에 따라 대용량 데이터를 대상으로 하는 데이터 마이닝 분야에서도 프라이버시 보호 문제에 대한 활발한 연구가 진행되고 있다. 데이터 마이닝에서의 프라이버시 보호 문제는 정보제공자에 의해 제공된 정보 중 민감한 개인 정보의 노출이 없이도 가능한 정확한 마이닝 결과를 얻는 것이다. 데이터 마이닝의 프라이버시 보호 기법에서는 데이터의 보호뿐만 아니라 결과의 정확도 또한 중요한 요인이다. 이에 따라, 본 논문에서는 시계열 데이터 클러스터링을 기반으로 랜덤 데이터 교란 기법에서 결과의 정확도를 높이는 기법으로 노이즈 평준화 개념을 제시한다. 기존의 랜덤 데이터 교란 기법은 데이터의 프라이버시는 잘 보호하지만 시계열간의 거리-순서가 보존되지 않아 결과의 정확도가 크게 떨어지는 문제점을 가진다. 이를 위해, 본 논문에서는 PAA를 기반으로 하는 노이즈 평준화 개념을 제시하고, 구체적인 예를 통해, 제안한 노이즈 평준화 개념이 랜덤 데이터 교란 기법에서 클러스터링 결과의 정확도를 높일 수 있음을 체계적으로 설명한다.

FEM을 이용한 유정압테이블의 운동정밀도 해서(1. 단면지지형 테이블의 해석 및 실험적 검증) (Finite Element Analysis on the Motion Accuracy of Hydrostatic Table(1.st. Analysis and Experimental Verification on Single-side Table))

  • 박천홍;정재훈;이후상;김수태
    • 한국정밀공학회지
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    • 제17권12호
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    • pp.137-144
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    • 2000
  • In order to achieve systematical method for improving motion accuracy of hydrostatic table, an algorithm using finite element method is proposed in this paper. Quantification of averaging effect of oil film on motion error is performed theoretically by analysis on the relationship between spacial frequency of rail form error and motion error of table. Influences of film stiffness and pocket size on the motion error of table are also analyzed theoretically. Validity of the algorithm is verified experimentally from the test on the motion error of table with three types of rail which have different form profile. Experimental results show that the algorithm is very effective to analyze theoretically the motion error of hydrostatic table.

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직선베어링 안내면의 운동오차 해석 (Analysis of the Motion Errors in Linear Motion Guide)

  • 김경호;박천홍;이후상;김승우
    • 한국정밀공학회지
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    • 제19권5호
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    • pp.139-148
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    • 2002
  • Motion errors of linear motion guideway are analyzed theoretically in this paper. For the analysis, an new algorithm predicting motion errors of bearing and guideway is proposed using the Hertz's elastic deformation theory. Accuracy averaging effect can be calculated quantitatively by analyzing relationship between motion errors of guideway and spatial frequency of rail form error. Influences of design parameters on the motion errors including the number of balls, preload, ball diameter, bearing length and the number of bearings are analyzed. As it is difficult to measure the rail form error, experimental results are compared with results analyzed by the equivalent analysis method which evaluate the motion errors of guideway using the measured errors of bearing. From the experimental results, it is confirmed that the proposed analysis method it effective lo analyze the motion errors of linear motion bearing and guideway.

FEM을 이용한 유정압테이블의 운동정밀도 해석 (Finite Element Analysis on the Motion Error of Hydrostatic Table)

  • 박천홍;정재훈;이후상;김수태
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 2000년도 춘계학술대회 논문집
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    • pp.658-662
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    • 2000
  • In order to achieve systematical method for improving motion accuracy of hydrostatic table, an algorithm using finite element method is proposed in this paper. Quantification of averaging effect of oil film on motion error is performed theoretically by analysis on the relationship between spacial frequency of rail form error and motion error of table. Influences of film stiffness and pocket size on the motion error of table are also analyzed theoretically Validity of the algorithm is verified experimentally from the test on the motion error of table with three types of rail which have different form profile. Experimental results show that the algorithm is very effective to analyze theoretically the motion error of hydrostatic table.

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Three-Dimensional Photon Counting Imaging with Enhanced Visual Quality

  • Lee, Jaehoon;Lee, Min-Chul;Cho, Myungjin
    • Journal of information and communication convergence engineering
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    • 제19권3호
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    • pp.180-187
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    • 2021
  • In this paper, we present a computational volumetric reconstruction method for three-dimensional (3D) photon counting imaging with enhanced visual quality when low-resolution elemental images are used under photon-starved conditions. In conventional photon counting imaging with low-resolution elemental images, it may be difficult to estimate the 3D scene correctly because of a lack of scene information. In addition, the reconstructed 3D images may be blurred because volumetric computational reconstruction has an averaging effect. In contrast, with our method, the pixels of the elemental image rearrangement technique and a Bayesian approach are used as the reconstruction and estimation methods, respectively. Therefore, our method can enhance the visual quality and estimation accuracy of the reconstructed 3D images because it does not have an averaging effect and uses prior information about the 3D scene. To validate our technique, we performed optical experiments and demonstrated the reconstruction results.

외부가압 공기 베어링 지지 스핀들 시스템에서 직각도 오차가 운전 정밀도에 미치는 영향 (An Effect on the Running Accuracy of the Perpendicularity Error in the Spindle System Supported with Externally-Pressurized Air Bearing)

  • 고정석;김경웅
    • Tribology and Lubricants
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    • 제15권3호
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    • pp.257-264
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    • 1999
  • Recently as electronics and semi-conductor industry develop, ultra-precision machine tools that use air-spindle with externally pressurized air bearing appear in need of ultra-precision products which demand high precision property. Effects of air compressibility absorbs the vibration of shaft, this is called averaging effect, however, the higher running accuracy is demanded by degrees, the more important factor is machining errors that affect running accuracy of shaft. Actually, it would be very important in the view points of running accuracy to understand effects of machining errors on the running accuracy of the spindle system quantitatively to design and manufacture precision spindle system in the aspect that efficiency in manufacturing spindle system and performance in operation. So fu, there are some researches on the effects that machining error affect running accuracy. However, because these researches deal with one bearing of spindle system, these results aren't enough to explain how much machining errors affect running accuracy in the typical spindle system overall. In this study, we investigate the effects of the perpendicularity error of bearing and shaft on running accuracy of spindle system that consists of journal and thrust bearing theoretically, and suggest design guideline about shape tolerances.

하이브리드 외부가압 공기베어링에서 노즐 위치에 따른 부하지지력 특성 (The development of the air-spindle for using to machining the die and mold)

  • 이득우;이종렬;황성철;이준석
    • 한국공작기계학회:학술대회논문집
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    • 한국공작기계학회 2000년도 추계학술대회논문집 - 한국공작기계학회
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    • pp.466-470
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    • 2000
  • Externally pressurized air journal bearing has been widely used in high-speed spindle system and precision machinery because of its characteristics such as substantially low frictional loss, low heat generation and averaging effect leading better running accuracy. But air journal bearing have a disadvantage of the low load capacity due to the low viscosity. In this paper, The air journal bearing design to overcome the defects of air bearing such as low stiffness and dimping coefficients was investigated theoretically.

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단일 스태거 PRI의 추정 및 능동 상쇄를 위한 예상 도착 시간 추정 기법 (Estimation Method of Single Stagger PRI and Future TOA for Active Cancellation)

  • 임성목;심동규;이충용
    • 전자공학회논문지
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    • 제51권3호
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    • pp.34-41
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    • 2014
  • 스태거 펄스 반복 주기 (pulse repetition interval, PRI)로 구성된 위협 레이더 신호에 대하여 실시간으로 PRI transform을 적용하여 스태거 PRI를 분석하고 측정 TOA와 추정된 PRI를 이용하여 능동 상쇄에 필요한 미래의 TOA (time of arrival)를 계산한다. 또한, 추정된 PRI와 TOA에 포함되어 있는 오차의 영향을 살펴보고 추정 PRI의 정확도를 향상시키는 기법과 TOA 오차의 영향을 감소시키기 위하여 TOA 평균화 기법을 제안한다. 마지막으로 TDOA와 최근 TOA를 이용하여 단순하게 예측된 미래 TOA와 제안된 방법을 통해 예측된 미래 TOA 간의 RMSE (root mean square error)를 비교하여 제안된 기법의 예측 정확도가 높음을 보인다.

원통형 커패시턴스 센서를 이용한 초정밀 공기 주축의 회전오차 측정

  • 김해일;박상신;한동철
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 1995년도 춘계학술대회 논문집
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    • pp.637-642
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    • 1995
  • For measuring the error motion of ultra-precision spindle, eliminating the geometric errors is a must. Unless it is achieved, geometric errors will be dominant in data. Here, the roundness error and alignment error between spindle and sensor are to be removed. That's because typical error range of such spindle is muchless than geometric one. A capacitive transducer of cylidricalshape was developed, which takes full advantage of the spatial-averaging effect by using large area compared tpo the geometric error. This idea was first proposed by Chapman and here it is modified for better performance with nomical gap of 50 .mu. m and with newly designed guards which encompass the respective sensor to rectify the electrical field distribution in good shape. The measurement system is made to get the orbit of Ultra-Precision Air Spindle which is supposed to have its runout under 1 .mu. m. The Calibration data of this sensor is presented and the spindle orbit from 2000rpm to 5500rpm is showed. It is quite reasonable to use this sensor in the range of 60 .mu. m with an accuracy of several tens of nm.

Frozen Orbits Construction for a Lunar Solar Sail

  • Khattab, Elamira Hend;Radwan, Mohamed;Rahoma, Walid Ali
    • Journal of Astronomy and Space Sciences
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    • 제37권1호
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    • pp.1-9
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    • 2020
  • Frozen orbit is an attractive option for orbital design owing to its characteristics (its argument of pericenter and eccentricity are kept constant on an average). Solar sails are attractive solutions for massive and expensive missions. However, the solar radiation pressure effect represents an additional force on the solar sail that may greatly affect its orbital behavior in the long run. Thus, this force must be included as a perturbation force in the dynamical model for more accuracy. This study shows the calculations of initial conditions for a lunar solar sail frozen orbit. The disturbing function of the problem was developed to include the lunar gravitational field that is characterized by uneven mass distribution, third body perturbation, and the effect of solar radiation. An averaging technique was used to reduce the dynamical problem to a long period system. Lagrange planetary equations were utilized to formulate the rate of change of the argument of pericenter and eccentricity. Using the reduced system, frozen orbits for the Moon sail orbiter were constructed. The resulting frozen orbits are shown by two 3Dsurface (semi-major, eccentricity, inclination) figures. To simplify the analysis, we showed inclination-eccentricity contours for different values of semi-major axis, argument of pericenter, and values of sail lightness number.