• Title/Summary/Keyword: Measuring Space

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Airflow Characteristic Experiments for the Upper Plenum Design of Clean Room (클린룸의 상부 플레넘 설계를 위한 유동특성 실험)

  • Oh, M.D.;Bae, G.N.;Kim, S.C.;Lee, C.S.
    • Korean Journal of Air-Conditioning and Refrigeration Engineering
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    • v.1 no.4
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    • pp.276-289
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    • 1989
  • The airflow characteristics in both the upper plenum and the clean space of clean room are investigated by measuring the pressure distribution of the upper plenum and the velocity profile in the clean space, at the various conditions of the supplied airflow rate, the volume of upper plenum and the air supply type. The performance of vertical air supply type and horizontal air supply type is analyzed in terms of the airflow uniformity which is frequently used in indicating the clean room performance, and the relations among the volume of upper plenum, the supplied airflow rate and the airflow uniformity are confirmed. The results of this experimental study can be applied to the designing of the upper plenum of clean room.

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DISCRETE TIME DYNAMIC MODEL FOR TELESCOPE AUTO-GUIDING SYSTEM (망원경의 자동추적장치를 위한 이산시간 동적모델 분석)

  • Lee, Joon-Hwa
    • Journal of Astronomy and Space Sciences
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    • v.24 no.4
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    • pp.431-450
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    • 2007
  • In the auto-guiding system for obtaining a long exposure astrophotography, CCD camera is usually used for measuring guide errors which are affected by optical dispersion and mechanical disturbances. In this paper, a discrete time dynamic model and a performance index are proposed for analysing the auto-guiding system. The optimal gain for proportional control is derived considering the optical dispersion and the disturbances. Some experiments are provided to illustrate that the optimal control gain is lower as the optical dispersion is higher.

Development of Tracking System for High Maneuvering Vehicle (고기동 비행체를 위한 추적시스템 개발)

  • Cho, Dong-Sik;Rha, Sung-Woong
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.36 no.4
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    • pp.399-406
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    • 2008
  • Tracking system is developed to receive both telemetry data and video data which are transmitted by radio frequency for the flight test of high manuvering vehicle. Tracking method of tracking system is the phase comparative monopulse that produce tracking data by measuring the phase difference of signal which is received by four patch antennas. The performance of tracking system is verified by flight test for RC helicopter and rocket.

Precision Measurement for Aircraft Alignment using Industrial Photogrammetry (산업사진측량을 이용한 항공기 얼라인먼트 정밀측정)

  • Jung, Sung-Heuk;Lee, Jae-Kee
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.33 no.6
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    • pp.57-63
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    • 2005
  • According to increasing of demand for high accurate and quick measuring technology, they became to interest in industrial photogrammetry that can satisfy with this needs. This study is examined O-2A aircraft to check the application of Industrial Photogrammetry technology. To measure the aircraft alignment, the check points marked on it were used without exact aircraft design data. And to check any deformation of its external original feature, Pro-spot system has been used.

PROTOTYPE DEVELOPMENT OF THE STAR SENSOR FOR THE KITSAT-3 (우리별 3호 STAR SENSOR 시험모델 개발)

  • 이현우;김병진;유상근;한원용
    • Journal of Astronomy and Space Sciences
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    • v.12 no.2
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    • pp.256-264
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    • 1995
  • This report presents the development procedure and the results of a prototype star sensor which can be used as one of the attitude sensors of the KITSAT-3. The star sensor is a major attitude sensor that can determine the 3-axis attitude information, by comparing between star corrdinates in the star catalog and the measured corrdinates. The 2 dimensional CCD camera is used for measuring the star corrdinates and the DSP(Digital Signal Processor) technology is applied to the image and signal processing. Using the prototype star sensor with thermoelectri cooling technique, we have succesfully obtained the star images around 4th magnitude at Sobaeksan Astronomy Observatory minimizing night sky effect.

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Effectiveness Criteria for Methods of Identifying Ionospheric Earthquake Precursors by Parameters of a Sporadic E Layer and Regular F2 Layer

  • Korsunova, Lidiya P.;Hegai, Valery V.
    • Journal of Astronomy and Space Sciences
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    • v.32 no.2
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    • pp.137-140
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    • 2015
  • The results of the study of ionospheric variations in the summer months of 1998-2002 at an ionospheric station of vertical sounding "Petropavlovsk-Kamchatsky" are presented. Anomalous variations of virtual sporadic-E height (h'Es), Es blanketing frequency (fbEs), and the critical frequency of the ionospheric F2 layer (foF2) (which can be attributed to the possible earthquake precursors) are selected. The high efficiency of the selection of ionospheric earthquake precursors based on the several parameters of Es and F2 layers is shown. The empirical dependence, which reflects the connection between the lead-time of the earthquake moment, the distance to the epicenter from the observation point, and the magnitude of the earthquake are obtained. This empirical dependence is consistent with the results of the detection of earthquake precursors by measuring the physical parameters of the Earth's crust in the same region.

Real-time estimation of Temperature Distribution of a Ball Screw System Using Modal Analysis and Observer (모드해석과 관측기에 의한 볼스크류 온도분포의 실시간 예측)

  • 김태훈
    • Proceedings of the Korean Society of Machine Tool Engineers Conference
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    • 2000.04a
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    • pp.635-640
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    • 2000
  • Thermal deformation of machine tools can be evaluated from the analysis of the whole temperature field. However, it is extremely inefficient and impossible to acquire the whole temperature field by measuring temperatures of every point. So, a temperature estimator, which can estimate the whole temperature field from the temperatures of just a few points, is required. In this paper, 1-dimensional heat transfer problem is modeled with modal analysis and state space equations. and then state observer is designed to estimate the intensity of heat source and the whole temperature field in real-time. The reliability of this estimator is verified by making a comparison between solutions by the proposed method and the exact solutions of examples. The proposed method is applied to the estimation of temperature distribution in a ball screw system.

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Dehazing in HSI Color Space with Color Correction (HSI 색 공간 색상 보정을 이용한 안개 제거 알고리즘)

  • Um, Taeha;Kim, Wonha
    • Journal of Broadcast Engineering
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    • v.18 no.2
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    • pp.140-148
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    • 2013
  • The haze removal algorithm using median dark channel prior is an efficient and fast method with relatively accurate transmission estimation. However, conventional methods may produce color distortion since the method ignores the color mismatch between estimated airlight and actual airlight. In this paper, we propose a color correction with measuring color fidelity in the HSI color space. Experimental results show that the proposed algorithm gives better color correction scheme.

Effect of Swirl Injector with Variable Backhole on Acoustic Damping in Liquid Rocket Engine (액체로켓 스월인젝터의 음향학적 감쇠기능)

  • ;;;;;;Bazarov, V. G.
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.34 no.8
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    • pp.79-86
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    • 2006
  • Swirl injector with adjustable backhole length was analyzed to suppress high-frequency combustion instability in Liquid Rocket Engines. In order to analyze the effect of variable backhole injector as an acoustic absorber, backhole injector was regarded as a quarter-wave resonator. As a result of theoretical approaches and acoustic tests, backhole injector with adjustable length could decrease the unstable modes of combustion chamber. And the damping efficiency was estimated by measuring damping rates experimentally.

Imperfection Parameter Observer and Drift Compensation Controller Design of Hemispherical Resonator Gyros

  • Pi, Jaehwan;Bang, Hyochoong
    • International Journal of Aeronautical and Space Sciences
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    • v.14 no.4
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    • pp.379-386
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    • 2013
  • The hemispherical resonator gyroscope is a type of vibratory gyroscope, which can measure angle or angular rate, based on its operating mode. This paper deals with the case when the hemispherical resonator gyroscope is operated in angle measurement mode. In angle measurement mode, the resonator pattern angle precesses, with respect to the external rotation input, by the principle of the Coriolis effect, so that the external rotation can be estimated, by measuring the amount of precession angle. However, this pattern angle drifts, due to the manufacturing error of the resonator. Since the drift effect causes degradation of the angle estimation performance of the resonator, the corresponding drift compensation control should be performed, to enhance the estimation performance. In this paper, a mathematical model of the hemispherical resonator gyro is first introduced. By using the mathematical model, a nonlinear observer for imperfection parameter estimation, and the corresponding compensation controller are designed to operate hemispherical resonator gyros, as angle measurement sensors.