• 제목/요약/키워드: Optical Tracking

검색결과 472건 처리시간 0.024초

광-ETherCAT 네트워크 기반 PMSM의 벡터제어 구현 (An Implementation of Vector Control of AC Servo Motor based on Optical-EtherCAT Network)

  • 김용진;김광헌;배영철
    • 한국전자통신학회논문지
    • /
    • 제8권4호
    • /
    • pp.583-588
    • /
    • 2013
  • 본 논문에서는 로봇에서 다축 모션 제어를 쉽게 할 수 있는 AC 서보 드라이버의 성능 검증을 위하여 벡터 전류 제어 구현 기법을 제안한다. 이를 위해 먼저 PMSM을 구동을 위한 드라이버를 개발한 후 이 드라이버가 정상적으로 동작하는지를 벡터 전류로 확인하였다. 벡터 제어는 무부하에서 전류 벡터 제어를 실행하여 지령 전류에 따른 추종 전류를 비교하였다. 검증 결과 만족할 만한 결과를 얻었음을 확인하였다.

200kW 탑형 태양열발전시스템에서 사용되는 Heliostat의 집열특성 분석 (Analysis of Energy Concentration Characteristics of Heliostat used in 200kW Tower Type Solar Thermal Power Plant)

  • 박영칠
    • 한국태양에너지학회 논문집
    • /
    • 제31권3호
    • /
    • pp.80-88
    • /
    • 2011
  • Heliostat in the tower type solar thermal power plant is a sun tracking mirror system to reflect the solar energy to the receiver and the optical performance of it affects to the efficiency of whole power plant most significantly. Thus a solid understanding of heliostat's energy concentration characteristics is the most important step in designing of the heliostat field and the whole power plant. The work presented here is the analysis of energy concentration characteristics of heliostat used in 200kW solar thermal power plant, where the receiver located at 43m high in tower has $2{\times}2$m rectangular shape. The heliostat reflective surface is formed by 4 of $1{\times}1$m flat plate mirror facet and the mirror facet is mounted on the spherical frame. The direct normal incident radiation models in vernal equinox, summer solstice, autumnal equinox and winter solstice are first derived from the actually measured data. Then the intercept ratio, heat flux distribution and total energy collected at the receiver for the heliostats located in the various places of the heliostat field are investigated. Finally the effect of mirror facet installation error on the optical performance of the heliostat is analyzed.

4 축 광픽업 액추에이터의 개발 (Development of a 4-axis optical pickup actuator)

  • 김재은;이경택;홍삼열;고의석;서정교;최인호;민병훈
    • 한국소음진동공학회:학술대회논문집
    • /
    • 한국소음진동공학회 2008년도 춘계학술대회논문집
    • /
    • pp.856-860
    • /
    • 2008
  • Wire-suspensions in the conventional actuators mechanically support the moving part and guarantee the accuracy of the actuator without tangential tilt actuation. However, such a suspension configuration has considerable stiffness in the tangential tilt direction with two additional wire beams for the tangential tilt. Thus, we performed a design sensitivity analysis for the wire-suspension stiffness of 4-axis actuator and controlled the main parameters such as distance among wire-suspensions and wire-suspension length to allow tangential tilt flexibility. The elasticity of frame PCB that supports the moving part by wire-suspensions was also exploited to improve the flexibility of wire-suspension in the tangential tilt direction. A novel suspension structure was devised by establishing eight wire-suspensions at both sides of the moving part for electrical connection to coils. The magnetic circuit according to the proposed 4-axis actuator using multi-polar magnet and coils was also suggested for the generation of electromagnetic forces in the focusing, tracking, radial and tangential tilt directions.

  • PDF

DESIGN CONCEPT FOR THE RETROFIT KAO 1M ROBOTIC TELESCOPE

  • Han, Won-Yong;Mack, Peter;Park, Jang-Hyun;Jin, Ho;Lee, Woo-Baik;Lee, Chung-Uk
    • Journal of Astronomy and Space Sciences
    • /
    • 제17권2호
    • /
    • pp.211-220
    • /
    • 2000
  • Korea Astronomy Observatory(KAO) is working to retrofit its 1m robotic telescope in collaboration with a company (ACE, Astronomical Consultants & Equipment). The telescope system is being totally refurbished to make a fully automatic telescope which can operate in both interactive and fully autonomous robotic modes. Progress has been made in design and manufacturing of the telescope mount, mechanics, and optical performance system tests are being made for re-configured primary and secondary mirrors. The optical system is designed to collect 80% incident light within 0.5 arcsec with f/7.5 Ritchey-Chretien design. The telescope mount is an equatorial fork with a friction drive system. The design allows fully programmable tracking speeds with typical range of 15 arcsec/sec with accuracy of $\pm5$ arcsec/hour. The mount system has integral pointing model software to correct for refraction, and all mechanical errors and misalignments. The pointing model will permit positioning to better than 30 arcsec RMS within $75^{\circ}$ from zenith and 45 arcsec RMS elsewhere on the sky. The software is designed for interactive, remote and robotic modes of operation. In interactive and remote mode the user can manually enter coordinates or retrieve them from a computer file. In robotic mode the telescope controller downloads the coordinates in the order determined by the scheduler. The telescope will be equipped with a CCD camera and will be accessible via the internet.

  • PDF

무인 항공기 촬영 동영상을 위한 실시간 안정화 기법 (Real-time Stabilization Method for Video acquired by Unmanned Aerial Vehicle)

  • 조현태;배효철;김민욱;윤경로
    • 반도체디스플레이기술학회지
    • /
    • 제13권1호
    • /
    • pp.27-33
    • /
    • 2014
  • Video from unmanned aerial vehicle (UAV) is influenced by natural environments due to the light-weight UAV, specifically by winds. Thus UAV's shaking movements make the video shaking. Objective of this paper is making a stabilized video by removing shakiness of video acquired by UAV. Stabilizer estimates camera's motion from calculation of optical flow between two successive frames. Estimated camera's movements have intended movements as well as unintended movements of shaking. Unintended movements are eliminated by smoothing process. Experimental results showed that our proposed method performs almost as good as the other off-line based stabilizer. However estimation of camera's movements, i.e., calculation of optical flow, becomes a bottleneck to the real-time stabilization. To solve this problem, we make parallel stabilizer making average 30 frames per second of stabilized video. Our proposed method can be used for the video acquired by UAV and also for the shaking video from non-professional users. The proposed method can also be used in any other fields which require object tracking, or accurate image analysis/representation.

광 저장장치용 리니어 보이스 코일 모터의 고속, 고정밀 위치제어 (High Speed and High Precision Control of Linear Voice Coil Motor for Optical Disc)

  • 김세웅;전홍걸;박노철;양현석;박영필
    • 한국소음진동공학회:학술대회논문집
    • /
    • 한국소음진동공학회 2000년도 추계학술대회논문집
    • /
    • pp.754-758
    • /
    • 2000
  • In recent years, the LDM(Linear DC Motor) is widely used, because it has more merits than other rotary motors. First, if system requires linear motion, LDM realizes direct linear motion as rotary motor does not. Second, system is simple and easy to control, and so on. In optical disc drive, a tracking system consists of two parts. One is fine actuating and the other is coarse actuating. For coarse actuating VCM(Voice Coil Motor) actuator is used as a basic drive mechanism. In this paper, MC(Moving Coil) type LDM is designed, manufactured and controlled. System is composed of mechanical-electromagnetic component, therefore mechanical loss and electromagnetic loss exist. The dominent mechanical loss is friction which results from sliding between guide shaft and hole. Therefore, this paper shows the friction compensation control. High speed and accurate position is not gained only PID control, therefore other control method is applied to the system.

  • PDF

200kW 탑형 태양열발전시스템을 위한 Heliostat 반사면 구조 설계 (Design of Structure of Heliostat Reflective Surface for 200kW Tower Type Solar Thermal Power Plant)

  • 박영칠
    • 한국태양에너지학회 논문집
    • /
    • 제31권2호
    • /
    • pp.53-62
    • /
    • 2011
  • Heliostat in the tower type solar thermal power plant is a sun tracking mirror system to reflect the solar energy to the receiver and the optical performance of it affects to the efficiency of whole power plant most significantly. Thus a proper design of structure of the heliostat reflective surface could be the most important step in the construction of such power plant. The work presented here is a design of structure of optical surface of heliostat, which will be used in 200kW solar thermal power plant. The receiver located at 43(m) high from ground in tower has $2{\times}2$(m) rectangular shape. We first developed the software tool to simulate the energy concentration characteristics of heliostat using the ray tracing technique. Then, the shape of heliostat reflective surface is designed with the consideration of heliostat's energy concentration characteristics, production cost and productivity. The designed heliostat's reflective surface has a structure formed by canting four of $1{\times}1$(m) rectangular flat plate mirror facet and the center of each mirror facet is located on the spherical surface, where the spherical surface is formulated by the mirror facet mounting frame.

Creation of 3D Maps for Satellite Communications to Support Ambulatory Rescue Operations

  • Nakajima, Isao;Nawaz, Muhammad Naeem;Juzoji, Hiroshi;Ta, Masuhisa
    • Journal of Multimedia Information System
    • /
    • 제6권1호
    • /
    • pp.23-30
    • /
    • 2019
  • A communications profile is a system that acquires information from communication links to an ambulance or other vehicle moving on a road and compiles a database based on this information. The equipment (six sets of HDTVs, fish-eye camera, satellite antenna with tracking system, and receiving power from the satellite beacon of the N-star) mounted on the roof of the vehicle, image data were obtained at Yokohama Japan. From these data, the polygon of the building was actually produced and has arranged on the map of the Geographical Survey Institute of a 50 m-mesh. The optical study (relationship between visibility rate and elevation angle) were performed on actual data taken by fish-eye lens, and simulated data by 3D-Map with polygons. There was no big difference. This 3D map system then predicts the communication links that will be available at a given location. For line-of-sight communication, optical analysis allows approximation if the frequency is sufficiently high. For non-line-of-sight communication, previously obtained electric power data can be used as reference information for approximation in certain cases when combined with predicted values calculated based on a 3D map. 3D maps are more effective than 2D maps for landing emergency medical helicopters on public roadways in the event of a disaster. Using advanced imaging technologies, we have produced a semi-automatic creation of a high-precision 3D map at Yokohama Yamashita Park and vicinity and assessed its effectiveness on telecommunications and ambulatory merits.

The medium-band observation of the neutrino source, TXS 0506+056

  • Hwang, Sungyong;Im, Myungshin;Taak, Yoonchan;Paek, Insu;Choi, Changsu;Shin, Suhyun;Ji, Tae-Geun
    • 천문학회보
    • /
    • 제44권1호
    • /
    • pp.73.4-73.4
    • /
    • 2019
  • The TXS0506+056 is a blazar and counterpart of the neutrino event IceCube-170922A. It is the first time that the neutrino event and flaring event in electromagnetic wave (EM) coincided. We observed TXS0506+056 with medium-bands in optical using 0.25m and 2.1m telescope at McDonald observatory about a month after the neutrino event. We tracked the variability of SED of the target for three weeks, and our observation showed no abrupt variability in optical range during this period. We concluded that a month after the neutrino event, the TXS0506+056 became less active and shows no feature of the energetic event. We also concluded that the medium-bands are well suited for tracking SEDs of objects. Our result demonstrates the potential of the wide-field 0.25m telescope (5.5 deg^2) for finding transient objects and track the variability of sources like AGNs.

  • PDF

3 m급 광학영상 촬영을 위한 6U 초소형위성 시스템 개념설계 (Conceptual Design of 6U Micro-Satellite System for Optical Images of 3 m GSD)

  • 김극남;박상영;김기환;박승한;송영범;송성찬
    • 항공우주시스템공학회지
    • /
    • 제16권3호
    • /
    • pp.105-114
    • /
    • 2022
  • 본 연구는 저궤도에서 3 m급 광학 영상을 획득하기 위한 6U 초소형위성 시스템의 개념설계를 제안한다. 3 m급 광학 영상을 촬영하기 위한 광학계를 설계하고 최적화한다. 광학계는 구경 Ø78 mm, 길이 250 mm의 공간 내, 유효 초점거리 1400 mm를 가진다. 이를 탑재할 수 있는 6U 초소형위성의 시스템에 대한 요구조건과 제한조건을 도출한다. 이러한 조건들을 만족하는 자세 및 궤도제어계, 추진계, 명령 및 데이터처리계, 전력계, 통신계, 구조 및 메커니즘계, 열제어계를 설계한다. 설계된 광학 탑재체와 COTS 부품으로 구성된 본체의 서브시스템을 통합하여 6U 초소형위성의 시스템을 완성한다. 전체 시스템의 질량, 전력, 통신에 대한 버짓 분석을 통해 설계규격을 확인한다. 저궤도에서 광학 영상을 획득하기 위한 6U 초소형위성의 운용 개념을 제시한다. 이러한 초소형위성을 대량으로 생산하여 위성군을 구축한다면 감시·정찰 임무나 재난·재해 관리에 활용할 수 있다.