• Title/Summary/Keyword: Measuring Space

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Analysis of the Ease in Basic Bodice Pattern Using 3-D Measuring Instrument (3차원 계측장치를 이용한 길 원형의 여유량 분석)

  • Shim, Kue-Nam;Suh, Jung-Kwon;Lee, Won-Ja
    • Fashion & Textile Research Journal
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    • v.2 no.3
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    • pp.239-245
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    • 2000
  • The purpose of this study was for analysis of ease about basic bodice pattern, as the first step of the research process for the drawing method of basic bodice for women in their twenties. The five selected basic bodice were made and they were worn by FRP body The garment space of each bodice was measured by analysis of the garment space of each section in figure of polymerization of cross section by a 3-D measuring instrument. The research suggests that this compared analysis is an objective reference. This analysis not only of the area of cross section of garment space and ease but also of the girth of the body shape and wearing shape, using the PAD system and 3-D measuring instrument, can be helpful in making garment patterns.

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Developement of Measuring Units of Space Motion Accuracy in Machining Center (Machining Center의 공간정도 측정장치의 개발)

  • Kim, Young Seuk;Namgung, Suk
    • Journal of the Korean Society for Precision Engineering
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    • v.12 no.2
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    • pp.37-47
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    • 1995
  • In recent years, it has been variously developed for testing the accuracy of circular motion of NC machine tools, for example Telescoping Ball Bar Method by Bryan, Circular test Method by Knapp and $r^{-{\theta} }$ Method by Tsutsumi etc., but these methods are all 2-dimentional measuring methods on plane. These simple methods of circular motion accuracy test of NC machine tools have been studied by many reserchers as above, but it is not yet settled in the code of measuring methods of motion errors of NC machine tools, because of errors of measuring units and sensors, and also especially the difficulties of centering of measuring units and the spindle of machining center. In this paper, in use of 2 rotary encoders and 1 magnetic type linear scale with resolution of 0.5 .mu. m, it has become possible for measuring of 3 dimentional space motion accuracy.

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Test bed for autonomous controlled space robot (우주로봇 자율제어 테스트 베드)

  • 최종현;백윤수;박종오
    • 제어로봇시스템학회:학술대회논문집
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    • 1997.10a
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    • pp.1828-1831
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    • 1997
  • this paper, to represent the robot motion approximately in space, delas with algorithm for position recognition of space robot, target and obstacle with vision system in 2-D. And also there are algorithms for precise distance-measuring and calibration usign laser displacement system, and for trajectory selection for optimizing moving to object, and for robot locomtion with air-thrust valve. And the software synthesizing of these algorithms hleps operator to realize the situation certainly and perform the job without any difficulty.

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Coma Aberration Correction of Optical System by using a Robot Arm Type Coordinated Measuring Machine (로봇팔 타입 삼차원좌표측정기를 이용한 광학계의 비축수차 보정)

  • Chun, Ho Bin;Kim, Goeun;Song, In-Woong;Kang, Hyug-Mo;Rhee, Hyug-Gyo;Ghim, Young-Sik;Yang, Ho-Soon;Kwon, Jong Hoon
    • Journal of the Semiconductor & Display Technology
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    • v.15 no.3
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    • pp.62-66
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    • 2016
  • Optical system needs to be aligned before its undergoing process, is usually shows coma aberrations, which occurred due to imperfection in the lens or other components results in off-axis point sources, appearing to have a tail like a comet. There are some methods to correct coma aberration. In this paper, to correct coma aberration in optical system, using a robot arm type coordinate measuring machine(CMM). CMMs are widely used to measure the form of accuracy of parts and positioning accuracy of systems. Among them, robot arm type CMM has more advantages than the others, such as its mobility and measuring range. However, robot arm type CMM has lower accuracy than cantilever type CMM. To prove robot arm type CMM's accuracy, several factors were suggested in this paper and the final measuring results were compared to a commercial cantilever type CMM. Based on this accuracy, a typical optical system was successfully aligned by using our robot arm type CMM.

Optimization of BIM based Space Plan by Expert System (전문가시스템을 활용한 BIM기반 건축공간 면적계획 최적화 방안)

  • Kwon, Ocheol;Cho, Joowon
    • Korean Journal of Computational Design and Engineering
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    • v.21 no.2
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    • pp.99-110
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    • 2016
  • The quality of building space program is a key to measure how the building performance satisfies its owner and users. However assuring its efficiency requires reliable criteria that reflect high level experience knowledge in the field. This study suggests a plan to gauge the level of building space performance using expert knowledge, which has not been utilized well enough but should play a critical role. In order to setup an expert system measuring level of the space program, we firstly optimized the space areas to the best case in a knowledgebase and use them as criteria to judge the quality of the spaces extracted from BIM model. We found the experimental results show us a promising way of measuring a relative quality of the space programs.

Computation of Ease-Rate in Basic Bodice Pattern by Analysis of Multiple Cross Section, Using 3-D Measuring Instrument (착의 단면 중합도 분석에 의한 길 원형의 여유률 산출 - 3차원 형상 계측기에 의한 -)

  • Shim, Kue-Nam;Kim, Jin-Sun;Lee, Womn-Ja
    • Fashion & Textile Research Journal
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    • v.2 no.4
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    • pp.360-365
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    • 2000
  • This research is the trial for the computation of the ease-rate for the bodice pattern. The result of the analysis about the cross section figures of garment space by using a 3-D measuring instrument is that: The garment space of each bodice by each body size is definite. In the figure of cross section of the basic lines, an area of cross section of garment space and length of cross section of garment space are not increased in proportion to an area of cross section of the body. The ease rate is the same no matter that flat-rate of the body is same or different. The ease-rate is computed by length of cross section of garment space that is in proportion to the radius of the body.

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Conceptual Design and Demonstration of Space Scale for Measuring Mass in Microgravity Environment

  • Kim, Youn-Kyu;Lee, Joo-Hee;Choi, Gi-Hyuk;Choi, Ik-Hyeon
    • Journal of Astronomy and Space Sciences
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    • v.32 no.4
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    • pp.419-425
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    • 2015
  • In this study, a new idea for developing a space scale for measuring mass in a microgravity environment was proposed by using the inertial force properties of an object to measure its mass. The space scale detected the momentum change of the specimen and reference masses by using a load-cell sensor as the force transducer based on Newton's laws of motion. In addition, the space scale calculated the specimen mass by comparing the inertial forces of the specimen and reference masses in the same acceleration field. By using this concept, a space scale with a capacity of 3 kg based on the law of momentum conservation was implemented and demonstrated under microgravity conditions onboard International Space Station (ISS) with an accuracy of ${\pm}1g$. By the performance analysis on the space scale, it was verified that an instrument with a compact size could be implemented and be quickly measured with a reasonable accuracy under microgravity conditions.

Apophis Rendezvous Mission: II. Payloads and Operation Scenario

  • Jeong, Minsup;Choi, Young-Jun;Moon, Hong-Kyu;Kim, Myung-Jin;Choi, Jin;Moon, Bongkon;JeongAhn, Youngmin;Lee, Hee-Jae;Baek, Seul-Min;Yang, Hongu;Ishiguro, Masateru
    • The Bulletin of The Korean Astronomical Society
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    • v.46 no.1
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    • pp.44.1-44.1
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    • 2021
  • We plan to visit the Apophis, a Potentially Hazardous Asteroid (PHA). Apophis will have an extremely close encounter with the Earth on April, 2029. At the closest position, Apophis approaches 0.1 lunar distances from the Earth. The science goals are 1) mapping the surface of the asteroid before and after the encounter, 2) measuring surface roughness before and after the encounter, and 3) measuring interplanetary space environments such as magnetic field and dust particles. For the science goal, we are planning to employ five instruments for this mission, which are Polarimetric Asteroid Camera (PolACam), Asteroid Terrain Mapping Camera (MapCam), Laser Altimeter, Dust Particle Detector (DPDetector), Magnetometer (Mag). In this presentation, we plan to give a talk on the instruments.

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Improved kinematic mount design for bar type reference mirror for profilometric measurement large optical surface

  • Jung, Kil-Jae;Yang, Ho-Soon;Rhee, Hyug-Gyo;Jyun, Byoung-Hyug;Lee, Yun-Woo;Kim, Sug-Whan
    • Bulletin of the Korean Space Science Society
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    • 2010.04a
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    • pp.25.3-25.3
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    • 2010
  • Our previous study used a bar-type reference mirror to measure the relative distance to the target surface. The target measurement accuracy was required to $1{\mu}m$ PV for aspheric optical surface up to 1m in diameter. Earlier system suffers from the reference surface deformation when the measuring part moves. In order to reduce the deformation, measuring part and the reference part separated from each order in the new design. This system utilizes a kinematic support assembly using invar flexure to minimize the reference surface deformation under gravity and vibration. The surface deformation requirement of reference mirror is defined as of $0.2{\mu}m$ under gravity and 40Hz vibration. The finite element results, shows reference mirror deformation of $0.164{\mu}m$. The first resonance mode was computed to analysis 46.05Hz for reference part and 43.44Hz for measuring part. Thesis satisfies the frequency requirement.

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