• 제목/요약/키워드: Position determination

검색결과 555건 처리시간 0.053초

6면 프리즘 렌즈가 장착된 Lensmeter에서 시험 렌즈의 편심 위치 계산 (Determination of the Decenter Position of a Test Lens in a Six-Sided Prism Lens Lensmeter)

  • ;박종대;조창호;김현규
    • 자연과학논문집
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    • 제16권1호
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    • pp.31-37
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    • 2005
  • 6면 프리즘 렌즈가 장착된 렌즈메터에서 상점의 위치로부터 시험렌즈의 편심의 위치를 알아 낼 수 있는 알고리즘을 개발하였다. 6개의 프리즘에 의해 형성되는 6개의 상점은 시험렌즈의 편심의 극좌표에 의해 변하게 되며, 비틀린 광선 추적으로 계산할 수 있다. 광학 설계 프로그램인 Code V를 사용하여 렌즈메터 광학계를 분석하고, 시험렌즈의 위치에 따른 상점의 위치 변화를 함수로 나타내서 역으로 상점의 위치로부터 시험렌즈의 편심의 위치를 알아낼 수 있는 방법을 개발하였다.

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정지궤도위성의 광학 관측데이터를 이용한 KARISMA의 정밀궤도결정 결과 분석 (Analysis of Precise Orbit Determination of the KARISMA Using Optical Tracking Data of a Geostationary Satellite)

  • 조동현;김해동;이상철
    • 한국항공우주학회지
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    • 제42권8호
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    • pp.661-673
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    • 2014
  • 본 논문에서는 한국항공우주연구원에서 개발한 우주파편 충돌위험 종합관리 시스템(KARISMA, KARI Collision Risk Management System)의 궤도결정 기능을 이용하여, 정지궤도위성의 광학 관측데이터에 기반한 정밀궤도결정을 수행하였다. 광학 관측데이터로는 정지궤도 위성 ARTEMIS에 대한 유럽우주기구(ESA, European Space Agency)의 실제 광학 관측데이터를 사용하였다. 동일한 관측데이터에 대해 유럽우주기구의 정밀궤도결정 시스템을 통해 얻은 궤도결정 결과와 비교했을 때 약 420 m 정도의 평균 위치오차가 있음을 확인하였다. 또한, 4일간의 광학 관측데이터를 바탕으로 얻은 궤도결정 결과를 이용하여 궤도예측을 수행하였으며, 유럽우주기구의 궤도결정 결과와 비교했을 때 3일 동안 대략 500~600 m 수준의 위치오차를 보였다. 이러한 결과들에 기반하여 KARISMA의 궤도결정 성능이 우주파편 충돌위험 분석을 위해 사용가능한 수준임을 확인할 수 있었다.

Batch Unscented Transformation for Satellite Orbit Determination Using A Satellite Laser Ranging (SLR)

  • Seo, Kyoung-Seok;Park, Sang-Young;Park, Eun-Seo;Kim, Young-Rok;Choi, Kyu-Hong
    • 한국우주과학회:학술대회논문집(한국우주과학회보)
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    • 한국우주과학회 2008년도 한국우주과학회보 제17권2호
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    • pp.34.2-34.2
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    • 2008
  • The batch least square filter is widely used for ground estimations. However, in orbit determination (OD) under inaccurate initial conditions and few measurement data the performance by the batch least square filter can lead an unstable results. To complement weak part of the batch filter, the batch unscented transformation without any linearization process is developed by ACL (Astrodynamics and Control Laboratory) in YONSEI University. In this paper, the batch unscented transformation is introduced and applied to satellite orbit determination using Satellite Laser Ranging (SLR) data. Only range of the satellite measured from ground tracking stations is used for measurement data. The results of simulation test are compared with those of the weighted batch least square filter for various initial states errors (position and velocity). Simulation results show that the batch unscented transformation is comparable or slightly superior to batch least square filter in the orbit determination.

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총의치 수직고경 설정에 대한 고찰 (Vertical Dimension in Complete Denture : A Literature Review & Clinical Procedures)

  • 정준용
    • 구강회복응용과학지
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    • 제18권3호
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    • pp.185-195
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    • 2002
  • Purpose This article describes the historic and clinical aspects of the determination of the vertical dimension of occlusion and the synoptic procedure of the determination of the vertical dimension of occlusion in complete denture. The determining procedure of the susceptible vertical dimension of occlusion is one of the most important steps in construction of complete denture and prosthodontic treatment. It is considered essential for the improvement and the recovery of facial esthetics and stomatognathic functions. Results Several methods have been suggested for measurement of the vertical dimension of occlusion in the construction of complete denture and the prosthodontic rehabilitation. These range from pre-extraction records to the use of physiologic rest position, swallowing, phonetics, esthetics and facial proportion, etc. But, there is no universally accepted or completely accurate method. There seems to be no significant advantages of one technique other than those of cost, time and equipment requirements, and seems to be in controversial in determining the vertical dimension. Conclusion The vertical dimension of occlusion should be determined and reinspected carefully by dentist for a successful prosthesis with several methods. The more investigations are necessary for more objective and scientific techniques in determining the vertical dimension of occlusion.

유한요소법에 의한 이종재료 접합면에 수직인 균열의 응력확대계수 결정 (Determination of Stress Intensity Factor for a Crack Perpendicular to Bimaterial Interface by Finite Element Method)

  • 임원균;김상철;이창수
    • 대한기계학회논문집
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    • 제17권10호
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    • pp.2398-2406
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    • 1993
  • Abdi's numerical method(ref.13) for representing a stress singularity by shifting the mid-side nodes of isoparametric elements is reviewed. A simple technique to obtain the optimal position of the mid-side nodes in quadratic isoparametric finite element is presented. From this technique we can directly obtain the position of the side-nodes adjacent to the crack tip. It is also observed that the present technique provides good accuracy for the expression of the opening displacement and the determination of the mid-side nodes for more wide range of material properties than that obtained by Abdicant the finite element method is applied to determine stress intensity factors for pressurized crack perpendicular to and terminating at the interface of two bonded dissimilar materials. A proper definition for stress intensity factors of a crack perpendicular to bimaterial interface is provided. It is based upon a near-tip displacement solutions on the crack surface for interface crack between two dissimilar materials. Numerical testing is carried out with the eight-node and six-node elements. The results obtained are compared with the previous solutions.

선박 내부 위치 측위를 위한 시스템 설계 (System Design for Location Determination Inside the Ship)

  • 박진관;정민아;윤석호;이성로
    • 한국통신학회논문지
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    • 제38C권2호
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    • pp.181-188
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    • 2013
  • 본 논문은 GPS 신호를 수신할 수 없는 대형선박의 내부에서 현재 위치를 정확하게 측정하기 위해서, GPS 신호를 대신하여 선박내부에 설치되어 있는 Wireless AP (Access Point)에서 발신되는 RSSI (Received signal strength indication)를 이용하였다. 선박내부에서 수신되는 RSSI 신호 중 신호세기가 가장 강한 3곳의 AP에서 발신되는 RSSI를 Friis 공식을 통해 거리로 환산 후, 삼각측량법을 통해 위치로 변환하였다. 그리고 AP에서 발신되는 신호에는 노이즈가 발생되기 때문에 신호세기가 불규칙하게 변함으로써 정확한 위치를 얻기 힘들다. 그래서 칼만필터를 통해 실시간으로 위치를 보정하고, 보정된 위치는 서버 DB에 저장된다.

소프트웨어 기반 Loran-C 신호 처리 (Software-Based Loran-C Signal Processing)

  • 임준혁;임성혁;김우현;지규인
    • 제어로봇시스템학회논문지
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    • 제16권2호
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    • pp.188-193
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    • 2010
  • With GPS being the primary navigation system, Loran use is in steep decline. However, according to the final report of vulnerability assessment of the transportation infrastructure relying on the global positioning system prepared by the John A. Volpe National Transportation Systems Center, there are current attempts to enhance and re-popularize Loran as a GPS backup system through the characteristic of the ground based low frequency navigation system. To advance the Loran system such as Loran-C modernization and eLoran development, research is definitely needed in the field of Loran-C receiver signal processing as well as Loran-C signal design and the technology of a receiver. We have developed a set of Matlab tools, which implement a software Loran-C receiver that performs the receiver's position determination through the following procedure. The procedure consists of receiving the Loran-C signal, cycle selection, calculation of the TDOA and range, and receiver's position determination through the Least Square Method. We experiences the effect of an incorrect cycle selection and various error factors (ECD, ASF, sky wave, CRI, etc.) from the result of the Loran-C signal processing. It is apparent that researches which focus on the elimination and mitigation of various error factors need to be investigated on a software Loran-C receiver. These aspects will be explored in further work through the method such as PLL and Kalman filtering.