• 제목/요약/키워드: Measurement error model

검색결과 809건 처리시간 0.136초

스플릿트샤프트 장치를 이용한 립실의 접촉력측정 (Radial Contact Force Measurement of Lip Seals with a Split Shaft Device)

  • Kim, Wan-Doo
    • 한국윤활학회:학술대회논문집
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    • 한국윤활학회 1996년도 제24회 추계학술대회
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    • pp.158-162
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    • 1996
  • A split shaft device is commonly used to measure the radial force of lip seals. The radial force measured with this device includes some inevitable error. This error is caused by the fact that the split shafts cannot maintain a perfect circle when the interference becomes larger or smaller than some initial interference. In this study, a theoretical model for the calculation of the radial contact force has been carried out, and an explicit equation for the measurement error as a function of the initial interference and the interference to be measured has been obtained. The error when the interference is small is not dependent upon the material properties and the shape of the lip seal, but rather upon the amplitude of the initial interference and the interference to be measured. When the interference is larger or smaller than the initial interference, the measured contact force is always underestimated or overestimated.

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NCPX 계측 방법에 따른 속도별 소음 데시벨 예측 모델 개발에 대한 연구 (A Study on Development of a Prediction Model for the Sound Pressure Level Related to Vehicle Velocity by Measuring NCPX Measurement)

  • 김도완;안덕순;문성호
    • 한국도로학회논문집
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    • 제15권4호
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    • pp.21-29
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    • 2013
  • PURPOSES : The objective of this study is to provide for the overall SPL (Sound Pressure Level) prediction model by using the NCPX (Noble Close Proximity) measurement method in terms of regression equations. METHODS: Many methods can be used to measure the traffic noise. However, NCPX measurement can powerfully measure the friction noise originated somewhere between tire and pavement by attaching the microphone at the proximity location of tire. The overall SPL(Sound Pressure Level) calculated by NCPX method depends on the vehicle speed, and the basic equation form of the prediction model for overall SPL was used, according to the previous studies (Bloemhof, 1986; Cho and Mun, 2008a; Cho and Mun, 2008b; Cho and Mun, 2008c). RESULTS : After developing the prediction model, the prediction model was verified by the correlation analysis and RMSE (Root Mean Squared Error). Furthermore, the correlation was resulted in good agreement. CONCLUSIONS: If the polynomial overall SPL prediction model can be used, the special cautions are required in terms of considering the interpolation points between vehicle speeds as well as overall SPLs.

무인자율수중운동체의 보정항법을 위한 축소된 오차 모델 (Reduced Error Model for Integrated Navigation of Unmanned Autonomous Underwater Vehicle)

  • 박용곤;강철우;이달호;박찬국
    • 제어로봇시스템학회논문지
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    • 제20권5호
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    • pp.584-591
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    • 2014
  • This paper presents a novel aided navigation method for AUV (Autonomous Underwater Vehicles). The navigation system for AUV includes several sensors such as IMU (Inertial Measurement Unit), DVL (Doppler Velocity Log) and depth sensor. In general, the $13^{th}$ order INS error model, which includes depth error, velocity error, attitude error, and the accelerometer and gyroscope biases as state variables is used with measurements from DVL and depth sensors. However, the model may degrade the estimation performance of the heading state. Therefore, the $11^{th}$ INS error model is proposed. Its validity is verified by using a degree of observability and analyzing steady state error. The performance of the proposed model is shown by the computer simulation. The results show that the performance of the reduced $11^{th}$ order error model is better than that of the conventional $13^{th}$ order error model.

초동 주시 측정 오차로 제어된 공대공 주시 토모그래피 사례연구 (A Case Study on the Cross-Well Travel-Time Tomography Regulated by the Error in the Measurement of the First Arrival Time)

  • 이두성
    • 지구물리와물리탐사
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    • 제12권3호
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    • pp.233-238
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    • 2009
  • 시추공 주시 토모그래피의 주요 요소 중 하나인 초동주시의 측정오차 정보를 사용한 주시 토모그래피 법을 제안하고, 이 역산 방법을 실제 시추공 탐사 자료에 적용하는 실험을 수행 하였다. 제안된 역산방법은 2단계 제어 처리 공정이다. 1) 성취하고자하는 속도 영상의 분해능에 기초하여 측정 주시의 허용 오차한계를 설정하고 측정오차가 오차한계 이상인 기록은 역산에서 제외한다. 2) 반복역산 과정에서 계산된 주시 차 중에서 해당기록의 측정오차 보다 작은 주시 차를 0(영) 처리함으로써 무의미한 수치가 누적되어 속도 개선에 기여함을 방지한다. 모든 기록을 사용한 속도영상과 제어역산으로 도출한 속도영상을 비교한 결과에 의하면, 제어 역산으로 도출한 속도영상에서 수치잡음이 상대적으로 적게 표출되었다. 그리고 Fermat 원리에 의하면, 이 영상이 보다 현실가능성이 높은 속도모델임을 확인하였다.

소형 선박용 관성측정장치 개발을 위한 MEMS 기반 관성 센서의 평가와 선정 (Evaluation and Selection of MEMS-Based Inertial Sensor to Implement Inertial Measurement Unit for a Small-Sized Vessel)

  • 임정빈
    • 한국항해항만학회지
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    • 제35권10호
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    • pp.785-791
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    • 2011
  • 본 논문에서는 소형 선박용 관성측정장치(Inertial Measurement Unit, IMU) 개발에 적합한 MEMS(Micro-Electro Mechanical System) 기반의 관성 센서 평가와 선정에 관하여 기술했다. 먼저, 오일러 공식에 기초한 관성 센서의 오차 모델과 잡음 모델을 정의하고, 앨런 분산(Allan Variance) 기법과 몬테카르로(Monte Carlo) 시뮬레이션 기법을 도입하여 관성 센서를 평가하였다. ADIS16405, SAR10Z, SAR100Grade100, LIS344ALH, ADXL103 등 다섯 가지 관성 센서에 대한 평가결과, ADIS16405의 자이로와 가속도계를 조합한 경우 오차가 가장 작게 나타났는데, 600 초 경과시 속도 오차의 표준편차가 약 160 m/s, 위치 오차의 표준편차가 약 35 km로 나타났다. 평가를 통해 ADIS16405 관성 센서가 IMU 구축에 최적임을 알았고, 이러한 오차 감소 방법에 대해서 참고문헌을 조사하여 검토하였다.

이차 변수 오차 모형의 예측분석 (Prediction Analysis of the Quadratic Errors-in-Variables Model)

  • 변재현;이승훈
    • 품질경영학회지
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    • 제21권1호
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    • pp.152-160
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    • 1993
  • In developing a quadratic regression relationship, independent variable is frequently measured with error. In this paper the integrated mean square error of prediction is developed for a quadratic functional relationship model as a measure of the effect of measurement error of the independent variable on the predicted values. The amount of the effect of error is presented and illustrated with an example.

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INS/GPS 결합 칼만필터의 측정치 스무딩 및 예측 (Smoothing and Prediction of Measurement in INS/GPS Integrated Kalman Filter)

  • 이태규;김광진;제창해
    • 제어로봇시스템학회논문지
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    • 제7권11호
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    • pp.944-952
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    • 2001
  • Inertial navigation system(INS) errors increase with time due to inertial sensor errors, and therefore it is desired to combine INS with external aids such as GPS. However GPS informations have a randomly abrupt jump due to a sudden corruption of the received satellite signals and environment, and moreover GPS can\`t provide navigation solutions. In this paper, smoothing and prediction schemes are proposed for GPS`s jump or unavailable GPS. The smoothing algorithm which is designed as a scalar adaptive filter, smooths abrupt jump. The prediction algorithm which is proved by Schuler error model of INS, estimates INS error in appropriate time. The outputs of proposed algorithm apply stable measurements to GPS aided INS Kalman filter. Simulations show that the proposed algorithm can effectively remove measurement jump and predict INS error.

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전달정렬의 측정치 시간지연 오차보상 기법 (Measurement Time-Delay Error Compensation for Transfer Alignment)

  • 임유철;송기원;유준
    • 제어로봇시스템학회논문지
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    • 제7권11호
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    • pp.953-957
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    • 2001
  • This paper is concerned with a transfer alignment method for the SDINS under ship motions. Major error sources of transfer alignment are data transfer time-delay, lever-arm velocity and ship body flexure. Specifically, to reduce alignment errors induced by measurement time-delay effects, the error compensation method through delay state augmentation is suggested. A linearized error model for the velocity and attitude matching transfer alignment system is first derived by linearizing the nonliner measurement equation with respect to its time delay and augmenting the delay state into the conventional linear state equations. And then it is shown via observability analysis and computer simulations that the delay state can be estimated and compensated during ship motions resulting in considerably less alignment errors.

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Measurement Time-Delay Error Compensation For Transfer Alignment

  • Lim, You-Chol;Song, Ki-Won;Joon Lyou
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 2000년도 제15차 학술회의논문집
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    • pp.486-486
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    • 2000
  • This paper is concerned with a transfer alignment method for the SDINS(StrapDown Inertial Navigation System) under ship motions. Major error sources of transfer alignment are data transfer time-delay, lever-arm velocity and ship body flexure. Specifically, to reduce alignment errors induced by measurement time-delay effects, the error compensation method through delay state augmentation is suggested. A linearized error model for the velocity and attitude matching transfer alignment system is first derived by linearizing the nonlinear measurement equation with respect to its time delay and augmenting the delay state into the conventional linear state equations. And then it is shown via observability analysis and computer simulations that the delay state can be estimated and compensated during ship motions resulting in considerably less alignment errors.

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Underwater Navigation of AUVs Using Uncorrelated Measurement Error Model of USBL

  • Lee, Pan-Mook;Park, Jin-Yeong;Baek, Hyuk;Kim, Sea-Moon;Jun, Bong-Huan;Kim, Ho-Sung;Lee, Phil-Yeob
    • 한국해양공학회지
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    • 제36권5호
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    • pp.340-352
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    • 2022
  • This article presents a modeling method for the uncorrelated measurement error of the ultra-short baseline (USBL) acoustic positioning system for aiding navigation of underwater vehicles. The Mahalanobis distance (MD) and principal component analysis are applied to decorrelate the errors of USBL measurements, which are correlated in the x- and y-directions and vary according to the relative direction and distance between a reference station and the underwater vehicles. The proposed method can decouple the radial-direction error and angular direction error from each USBL measurement, where the former and latter are independent and dependent, respectively, of the distance between the reference station and the vehicle. With the decorrelation of the USBL errors along the trajectory of the vehicles in every time step, the proposed method can reduce the threshold of the outlier decision level. To demonstrate the effectiveness of the proposed method, simulation studies were performed with motion data obtained from a field experiment involving an autonomous underwater vehicle and USBL signals generated numerically by matching the specifications of a specific USBL with the data of a global positioning system. The simulations indicated that the navigation system is more robust in rejecting outliers of the USBL measurements than conventional ones. In addition, it was shown that the erroneous estimation of the navigation system after a long USBL blackout can converge to the true states using the MD of the USBL measurements. The navigation systems using the uncorrelated error model of the USBL, therefore, can effectively eliminate USBL outliers without loss of uncontaminated signals.