• Title/Summary/Keyword: 자동시준

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Automatic Alignment of a Collimating Mirror by Using Phase Image Correlatio (위상 이미지 상관기법을 이용한 시준거울의 자동정렬)

  • Kim, Hyun-Suk;Tserendolgor, D.;Kim, Dae-Suk;Lee, Hyung-Chul;Kim, Soo-Hyun
    • Korean Journal of Optics and Photonics
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    • v.22 no.1
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    • pp.30-34
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    • 2011
  • A novel alignment method that can be used for aligning the collimating mirror employed in a monochromator is described. In most of the spectrometer industry, the alignment of optical components such as a focusing mirror, a grating and a collimating mirror has been performed manually so far. In this paper, we use a matchedfilter based image correlation technique for measuring the accurate image position which is used for aligning the collimating mirror. The experimental results show that with the proposed scheme automatic alignment can be completed within 10 seconds.

Study on Measurement Accuracy by Auto-Collimation using Theodolite (데오드라이트를 이용한 자동 시준에 의한 측정 정확도에 관한 연구)

  • Lee Byoung-Gi;Kwon Jae-Wook;Yoon Yong-Sik
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 2005.06a
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    • pp.1793-1796
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    • 2005
  • The auto-collimation by using theodolite has been accomplished for the straight measurement and the horizontality adjustment. But according to the procedure of auto-collimation or composition of the measurement equipment, an error of the measurement can be occurred. Therefore, this paper accomplished the research for enhancement of measurement accuracy according to measurement procedure of auto-collimation. For that, it has been compared the study of the combination of several precise measurement equipment with using of several theodolite.

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A Study of Spacecraft Alignment Measurement with Theodolite (데오도라이트를 이용한 위성체 얼라인먼트 측정에 관한 연구)

  • Yun,Yong-Sik;Park,Hong-Cheol;Son,Yeong-Seon;Choe,Jong-Yeon
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.31 no.10
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    • pp.105-111
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    • 2003
  • A measurement of spacecraft alignment is an important process of spacecraft assembly, integration and test. Because, it is necessary that a operator of a ground station controls the precise positions of on-orbit spacecraft by using the alignment data of attitude orbit control sensors(AOCS) on spacecraft. And, an accuracy of spacecraft alignment requirement is about $0.1^{\circ}{\sim}0.7^{\circ}$. A spacecraft alignment is measured by autocollimation of theodolite. This paper describes the measurement principle and method of spacecraft alignment. The result shows that all the AOCS on the spacecraft are aligned within the tolerance required through the alignment measurement.

Collimation testing of a white light beam and measurement of chromatic aberration of a lens by using vernier Moire fringe patterns (버니어 무아레 무늬를 이용한 백색광의 시준 검사 및 렌즈의 색수차 측정)

  • 송종섭
    • Korean Journal of Optics and Photonics
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    • v.11 no.4
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    • pp.232-238
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    • 2000
  • The new collimation testing technique of a white light beam using vernier Moire fringes of two line or circular gratings with different pitches is presented. We can visually measure the defocusing ($\Deltaf$), the divergence angle ($\theta$), and the longitudinal chromatic aberration $(L_{ch})$ of a collimating lens by using the technique. For example, we obtained $\Deltaf$= 21.9 mm and $\theta=0.0038^{\circ}$ for a testing lens with the focallengthf = 120.0 mm and F-number of F/2.4. The longitudinal chromatic aberration $L_{ch}$ of another testing lens withf = 65.0 mm, F/1.6, and the Abbe number V = 64.1 for the incident wavelengths of $\lambda_1=480 nm and \lambda_2=640 nm$ is easily measured by same technique. It is found that the measured value $L_{ch}=1.59mm(\pm0.01mm)$ is well agreed with $L_{ch}=1.58mm(\pm0.01mm)$ obtained by the autofocus method.

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Improvement of Positioning Accuracy using Site Calibration and Monitoring System of GPS (GPS의 현장 Calibration과 Monitoring System을 이용한 위치결정 정확도 향상)

  • Ahn Won-Tae;Moon Young-Hyun;Choi Seok-Keun;Lee Jae-Kee
    • Proceedings of the Korean Society of Surveying, Geodesy, Photogrammetry, and Cartography Conference
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    • 2006.04a
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    • pp.21-26
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    • 2006
  • 기존 해상구조물의 위치결정은 조류나 바람, 안개, 비, 눈, 일조시간 등의 기상조건으로 인한 장해요인과 지상 기준점 좌표값을 쉽게 이용하기가 곤란하기 때문에 정확한 위치결정을 할 수 있는 기법이 필요하다. 기존의 측량방법은 해상의 가설측량대 설치 및 철거에 따른 시간과 예산이 소요되고, 기상조건에 따라 시준이 불가능하여 작업 중단과 공기가 지연되며, 시준오차와 자료 오기오차 등이 발생하는 문제점을 가지고 있다. 본 연구에서는 GPS측량방법을 이용하여 현장 Calibration을 수행하여 위치정확도를 향상시키고, 해상에서의 기상조건에 따른 문제점과 상시 Monitoring에 의한 자동제어시스템을 개발함으로써 측량 정확도 향상과 해상구조물 공사기간 단축, 공사비 절감 등의 효과를 가져 올 수 있도록 하였다.

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Application of the New Technology for an Efficient Cadastral Re-survey Project (지적재조사사업의 효율화를 위한 신 기술 적용 방안)

  • Hong, Sung-Eon
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.14 no.12
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    • pp.6196-6203
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    • 2013
  • This study examined cadastral surveying technology regulated under the "Special Law for the cadastral surveying", and analyzed the related surveying methods currently used. Based on the analysis, this study suggested the efficient application plan future cadastral surveying projects. The new technologies analyzed were GNSS, GPS RTK, Network RTK, GPS Augmentation System, and the mobile and auto sighting TS. As a result of the analysis, this study suggests that if a receiving technology is possible for the integrated receiving of GPS/GLONASS/Galileo systems, both the accuracy of location determination could be enhanced and stable data could be obtained. The Network RTK technology may solve the constraint receiving factors of satellite information in the long term if a GPS Augmentation System is used. Finally, mobile and auto sighting TS technologies can reduce the personnel factors, but can be applied after the offset problem is overcome.

A Study on Alignment Measurement and Compensation for Spacecraft Sensors (위성 탑재 센서의 정렬 측정 및 보정에 관한 연구)

  • Lee Byoung-Gi;Kim Young-Youn;Yoon Yong-Sik
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 2005.06a
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    • pp.537-540
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    • 2005
  • The attitude control, sensors and camera installed on the spacecraft should be located according to the system alignment requirement. The alignment measurement requirement accuracy for the sensors should be below $\pm$0.1. Therefore, Alignment Measurement System which is combined theodolite, Rotating table and digital inclinometer etc., should be used. As the measurement accuracy is required very precise, the appropriate measurement procedure and alignment angle measurement, calculation and shimming work should is accomplished. Consequently, this paper is accomplished the works to align the measurement requirement accuracy throughout alignment measurement and shimming work of installed module and sensor

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A Study on Spacecraft Alignment Measurement with Theodolite (데오도라이트를 이용한 위성체 얼라인먼트 측정에 관한 연구)

  • 윤용식;이동주
    • Transactions of the Korean Society of Machine Tool Engineers
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    • v.12 no.6
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    • pp.64-70
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    • 2003
  • A measurement of spacecraft alignment is an important process of spacecraft assembly, integration and test because it is necessary that a ground station controls the precise positions of on-orbit spacecraft by using the alignment data of attitude orbit control sensors(AOCS) on spacecraft. In addition, accuracy of spacecraft alignment requirement is about $0.1^{\circ}$~$0.7^{\circ}$. The spacecraft alignment is measured by autocollimation of theodolite. This paper describes the measurement principle and method of spacecraft alignment. The result shows that all of the AOCS on the spacecraft are aligned within the tolerance required through the alignment measurement.

Null alignment system of the optical beam director (광집속장치의 광학정렬을 위한 null 광학계)

  • 김연수;김현숙;김현규
    • Korean Journal of Optics and Photonics
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    • v.15 no.3
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    • pp.254-257
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    • 2004
  • A null optical system for monitoring the alignment of the optical beam director is proposed instead of the conventional autocollimator alignment system. A null optical system for the optical beam director of aperture 30 cm is designed and its performance is analysed.

Autofocusing Mechanism of a Triple-Magnification Infrared System (3중 배율 적외선 영상 장비의 자동 초점 조절 방안)

  • Jung, Hyojung;Jeong, Suseong;Yang, Yunseok;Lee, Yongchun;Han, Jeongsu
    • Korean Journal of Optics and Photonics
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    • v.31 no.6
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    • pp.314-320
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    • 2020
  • The optics used in an infrared imaging system has a strong refractive-index change according to temperature, so an autofocus control function is essential for a military infrared imaging system with a wide operating-temperature range. In this study, we design a triple-magnification infrared imaging system, and to compensate for the change in refractive index according to temperature we measure the change in the lens focus according to temperature. The autofocus control function was implemented by using the measured movement amount, and we could obtain an image with satisfactory resolution performance over a wide range of operating temperatures.