• Title/Summary/Keyword: Precision Correction

검색결과 322건 처리시간 0.029초

수중탐상로봇시스템의 오차분석 및 보정 (Calibration of an underwater robotic inspection system)

  • 장종훈;김재열;김재희
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 2000년도 제15차 학술회의논문집
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    • pp.378-378
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    • 2000
  • The permissible positioning error of the transducer used in reactor inspection must be within 10 mm. To implement the required precision it is necessary to manufacture all components affecting the positioning mechanism correctly and precisely. In addition, it is also necessary to handle error factors accurately. This paper describes the activities of the findings and corrections of the errors which were occurred in experiments. Those activities are; i) Categorization of error factors, ii) Cause analysis of errors, iii) Correction of errors founded in experiments by the analysis of laser induction type and by the validation of real measurement of horizontal, vertical baselines.

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Experimental technique for efficiency transfer along different geometries and volumes

  • Haddad, Kh;AL-Homyed, A.
    • Nuclear Engineering and Technology
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    • 제53권2호
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    • pp.695-698
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    • 2021
  • Efficiency calibration is a fundamental procedure in gamma spectrometric measurement. Experimental technique for efficiency calibration transfer in gamma spectrometer along different geometries and volumes has been developed and validated in this work. The developed technique offers simple and easy procedures to overcome several problems encountered in efficiency calibration of gamma spectrometer such as rate-related correction and different sample volumes. The validation shows that application of the developed technique has a precision of 95%.

대기 중 오염물질의 시료채취시 관측오차 저감방법에 대한 연구 : 6구형 매니폴더를 장착한 MFC system의 개발과 평가 (Methodological Approaches to Reduce Uncertainties Associated with Air Sampling : Development and Assessment of a Six-port Manifold MFC System)

  • 김기현;오상인;최여진;김민영;최규훈
    • 한국대기환경학회지
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    • 제19권4호
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    • pp.377-386
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    • 2003
  • In order to develop a confident sampling technique, we designed and constructed a 6-port manifold MFC sampling system for collecting gaseous pollutants in air. Using this instrumentation, we tested the performance criteria of MFC system in terms of: (1) flow rate; (2) MFC-to-MFC variability; (3) tube-to-tube variability; and (4) time. It was interesting to find that the later two factors did not show any significant variations, while the former two show substantially large variations. However, as most of those variabilities are consistent enough to form systematic patterns, we were able to explain the occurrence patterns of all those MFC biases in terms of those four major variables. The overall results of our experiment suggest that one needs to use correction factor for each MFC unit under a given flow rate to maintain optimal accuracy and precision for sampling of those pollutants.

다중채널 직접구동 엑츄에이터의 구동전류 동일화 루프 설계 (Current Equation Loop Design of Muti-channel Direct Drive Valve Actuation)

  • 남윤수
    • 한국정밀공학회지
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    • 제17권10호
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    • pp.162-169
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    • 2000
  • A Direct Drive Valve(DDV) hydraulic actuation system which is commonly used as an aircraft's control surface driving actuator has multi-loop control structure to ensure its safety operation. However, because of not perfect matching of one self channel characteristics with the others, the servo valve driving current of each channel can be widely different. Therefore, the long-time use of DDV actuator without any correction of these channel current offsets will cause the problem of performance or life expectancy degradation due to unwanted heats in the linear motor. A current equalization loop structure which can minimizes current offsets between channels is introduced and designed. The performance of the current equalization loop is investigated and verified through the analytic and experimental ways.

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Effect of Rolling Speed on the Exit Cross Sectional Shape in Rod Rolling Process

  • Lee, Young-Seog
    • International Journal of Precision Engineering and Manufacturing
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    • 제8권1호
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    • pp.27-31
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    • 2007
  • A rolling speed dependent spread model is proposed for predicting the exit cross sectional shape in oval-round (or round-oval) pass rod rolling process when the rolling speed is very high. The effect of rolling speed on the exit cross sectional shape is measured by performing a four-pass continuous high speed (${\sim}80m/s$) rod rolling test and is described in terms of the spread correction parameter. The validity of the model is examined by applying it to rod rolling process at POSCO No.3 Rod Mill. The cross sectional shapes of workpiece predicted by the proposed model coupled with the surface profile prediction $method^{6}$ are in good agreement with those obtained experimentally.

척추측만증 유한 요소 모델 자동 생성 프로그램 개발 (Development of a program for Scoliosis FE Model Automatic Generation)

  • 유한규;김영은
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 2004년도 추계학술대회 논문집
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    • pp.1154-1159
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    • 2004
  • Unexpected postoperative changes, such as growth in rib hump, has been occasionally reported after corrective surgery for scoliosis. However there has been experimental data for explanation of these changes, nor the suggestion of optimal correction method. This numerical study was designed to investigate the main correlating elements in operative kinematics with post-operative changes of vertebral rotation and rib cage deformation in the corrective surgery of scoliosis. To develop a scoliotic spine model automatically, a special program for converting normal spine model to scoliotic spine model was developed. A mathematical finite element model of normal spine including rib cage, sternum, both clavicles, and pelvis was developed with anatomical details. The skeletal deformity of scoliosis was reconstructed, by mapping the X-ray images of a scoliosis into this three dimensional normal spine and rib cage model. The geometric mapping was performed by translating and rotating the spinal colume with the amount analyzed from the digitized 12 built-in coordinate axes in each vertebral image. By utilizing this program, problems generated in mapping procedure such as facet joint overlapping, vertebral body deformity could be automatically resolved.

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광위상 간섭을 이용한 기계 이송축의 운동오차 측정 및 실시간 보상

  • 이형석;김승우
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 1993년도 춘계학술대회 논문집
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    • pp.204-207
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    • 1993
  • 현대는 급속히 발전하는 공업을 바탕으로 생산품의 고기능화, 고정도화, 고속화를 추구하고있다. 그중에서도 고정도화에 대항 요구는 초정밀 가공 분야의 경우 2000년대 초에는 수 nm 수준까지 도달할 것으로 예측된다. 현재 각 선진국에서는, 초정밀도의 형상 정밀도를 요구하는 대형 광학 부품들의 가공에대한 연구가 진행중이며, 이와 같은 연구에서 요구되는 가공 정밀도가 조만간 가공기의 강성한계에 도달할 것이다. 이와함께 초정밀 가공에 있어서, 이송 테이블의 운동오차는 심각한 문제로 대두되고 있으므로, 테이블의 운동오차의측정 및 실시간 보상에 대한 연구의 의미가 있을 것으로 생각된다. 본 연 구는 기계 이송 테이블의 기하학적 운동오차의 실시간보상(real-time correction)에 관한 것이다.

Autonomous Sensor Center Position Calibration with Linear Laser-Vision Sensor

  • Jeong, Jeong-Woo;Kang, Hee-Jun
    • International Journal of Precision Engineering and Manufacturing
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    • 제4권1호
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    • pp.43-48
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    • 2003
  • A linear laser-vision sensor called ‘Perception TriCam Contour' is mounted on an industrial robot and often used for various application of the robot such as the position correction and the inspection of a part. In this paper, a sensor center position calibration is presented for the most accurate use of the robot-Perceptron system. The obtained algorithm is suitable for on-site calibration in an industrial application environment. The calibration algorithm requires the joint sensor readings, and the Perceptron sensor measurements on a specially devised jig which is essential for this calibration process. The algorithm is implemented on the Hyundai 7602 AP robot, and Perceptron's measurement accuracy is increased up to less than 1.4mm.

준천정 위성 궤도 특성 및 항법정보 연구 (Study of Quasi Zenith Satellite Orbit and Navigation Messages)

  • 김정래
    • 한국항공운항학회지
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    • 제15권1호
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    • pp.11-17
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    • 2007
  • One of the key elements for developing GNSS (Global Navigation Satellite Systems) is the comprehensive analysis of GNSS satellite orbit including the capabilities to generate precision navigation message. The orbit characteristics of Japan's own GNSS system, called QZSS (Quasi Zenith Satellite System) is analyzed and its navigation message, which includes orbit elements and correction terms, is investigated. QZSS-type orbit simulations were performed using a precision orbit integrator in order to analyze the effect of perturbation forces, e.g. gravity, Moon, Sun, etc., on the orbit variation. A preliminary algorithm for creating orbit element corrections was developed and its accuracy is evaluated with the simulation data.

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