• 제목/요약/키워드: line-of-sight

검색결과 735건 처리시간 0.032초

Spectroscopic Detection of Alfvenic Waves in the Chromosphere of Sunspot Regions

  • Chae, Jongchul;Cho, Kyuhyoun;Nakariakov, Valery M.;Cho, Kyung-Suk;Kwon, Ryun-Young
    • 천문학회보
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    • 제46권2호
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    • pp.47.1-47.1
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    • 2021
  • Transverse magnetohydrodynamic waves often called Alfvénic (or kink) waves have been often theoretically put forward to solve the outstanding problems of the solar corona like coronal heating, solar wind acceleration, and chemical abundance enhancement. Here we report the first spectroscopic detection of Alfvénic waves around a sunspot at chromospheric heights. By analyzing the spectra of the Hα line and Ca II 854.2 nm line, we determined line-of-sight velocity and temperature as functions of position and time. As a result, we identified transverse magnetohydrodynamic waves pervading the superpenumbral fibrils. These waves are characterized by the periods of 2.5 to 4.5 minutes, and the propagation direction parallel to the fibrils, the supersonic propagation speeds of 45 to 145 km s-1, and the close association with umbral oscillations and running penumbral waves in sunspots. Our results support the notion that the chromosphere around sunspots abounds with Alfvénic waves excited by the mode conversion of the upward-propagating slow magnetoacoustic waves.

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선박의 항로추종을 위한 LOS 가이던스 시스템의 제안 (A Proposal of an LOS Guidance System of a Ship for Path Following)

  • 김종화;이병결
    • 제어로봇시스템학회논문지
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    • 제11권4호
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    • pp.363-368
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    • 2005
  • This paper proposes an LOS(line-of-sight) guidance system of a ship for path following. From the viewpoint of a control configuration, guidance is a special type of compensation algorithm that is placed in front of the controller to accomplish navigational objects. A guidance system generates a reference trajectory for trajectory tracking or path control and decides the desired velocity, position and heading angle. A control system executes commands based on a reliable guidance law during navigation. An LOS vector from the vessel to a point on the path between two way-points in straight-line navigation or a point among turning circle in turning navigation is selected, and then a heading angle is calculated to converge the desired path based on the LOS vector. The LOS guidance law is defined for the straight-line and the turning circle, respectively. The effectiveness of the suggested LOS guidance system is assured through computer simulation.

해류중 직선 항행하는 선박의 LOS 가이던스 시스템의 제안과 유전 알고리즘을 이용한 최적화 (A Proposal of LOS Guidance System of a Ship in Straight-line Navigation under Ocean Currents and Its Optimization Using Genetic Algorithm)

  • 김종화;이병걸
    • Journal of Advanced Marine Engineering and Technology
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    • 제29권1호
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    • pp.124-131
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    • 2005
  • This paper suggests LOS(Line-Of-Sight) guidance system of a surface vessel in straight-line navigation under ocean currents An LOS vector from the vessel to a point on the path between two way-points is decided and a heading angle is calculated to converge to follow the desired path based on the LOS vector This guidance system is called LOS guidance system. The suggested LOS guidance law has parameters to be properly chosen according to navigational environment. Parameters of LOS guidance system are optimized to reduce propulsive energy and/or position error between desired Position and present position of a ship using genetic algorithm which is a strong optimization algorithm with adaptational random search The effectiveness of the suggested LOS guidance system is assured through computer simulations.

무인 비행선의 자동 경로 추종 시스템 개발 및 비행시험 (Design and Flight Test of Path Following System for an Unmanned Airship)

  • 정균명;성재민;김병수;제정형;이성근
    • 제어로봇시스템학회논문지
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    • 제16권5호
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    • pp.498-509
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    • 2010
  • In this paper, a waypoint guidance law Line Tracking algorithm is designed for testing an Unmanned Airship. In order to verify, we develop an autonomous flight control and test system of unmanned airship. The flight test system is composed FCC (Flight Control Computer), GCS (Ground Control System), Autopilot & Guidance program, GUI (Graphic User Interface) based analysis program, and Test Log Sheet for the management of flight test data. It contains flight test results of single-path & multi-path following, one point continuation turn, LOS guidance, and safe mode for emergency.

The extended narrow-line region kinematics of 3 Type-2 QSOs revealed by the VLTVIMOS IFU spectra

  • 조호진;우종학
    • 천문학회보
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    • 제37권2호
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    • pp.88.2-88.2
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    • 2012
  • We present kinematic properties of the narrow-line region in three type-2 QSOs at z~0.35, using 2-D spectra obtained with the VIMOS integral field unit spectrograph at the Very Large Telescope. One of the objects shows a line-of-sight velocity shift of the [OIII] and $H{\beta}$ lines up to 40km/s on a 15 kpc scale, which can be interpreted as either outflow or rotation. The outflow scenario is supported by the presence of blue wings and a radio structure showing lobes in the same direction. Another object features double-peaked emission lines which can be decomposed into two velocity components. Its Hubble Space Telescope image shows two nuclei separated by ~0.2"(~1kpc), implying this may be a binary AGN.

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Rapid Formation and Disappearance of a Filament Barb

  • Joshi, Anand D.
    • 천문학회보
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    • 제38권2호
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    • pp.86.1-86.1
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    • 2013
  • Observations of a filament showing an activated barb recorded from the at the Dutch Open Telescope (DOT) on 2010 August 20 are presented. The filament developed a barb in 10 minutes, which disappeared within the next 35 minutes. Such a rapid formation and disappearance of a filament barb is unusual, and has been seldom reported. Line-of-sight velocity maps were constructed from images in seven line positions along the H-alpha line. We observe flows in the filament spine towards the barb location prior to its formation, and flows in the barb towards the spine during its disappearance. Photospheric magnetograms from Helioseismic Magnetic Imager on board the Solar Dynamics Observatory were used to determine the changes in magnetic flux in the region surrounding the barb location. The variation of magnetic flux in this duration support the view that barbs are rooted in minor magnetic polarity.

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SPOT 4 영상의 기하보정을 위한 시선 벡터 조정 모델 (Line-of-Sight (LOS) Vector Adjustment Model for Restitution of SPOT 4 Imagery)

  • 정형섭
    • 한국측량학회지
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    • 제28권2호
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    • pp.247-254
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    • 2010
  • SPOT 4 위성영상의 기하 왜곡을 보정하기 위하여 새로운 접근방법을 연구하였다. 우주공간에서 위성과 지구의 관계를 정립함으로서 새로운 조건 방정식을 유도하였다. 초기 위성에 대한 정보가 어떤 일정한 변화에 의해 왜곡이 있다고 가정하고, LOS(Line-Of-Sight) 벡터를 변화시켜 위성영상의 기하를 보정하는 LOS 벡터 조정 모델을 연구하였다. 본 모델을 증명하기 위하여 관측각이 큰 SPOT 4 위성영상을 대상으로 실험하였다. 또한, 정확한 실험을 위하여 GPS로부터 측량한 10개의 지상기준점(GCPs)과 25개의 검사점(check points)을 사용하였다. SPOT 4 위성영상에 주어진 초기 위성정보(위성 위치, 속도, 자세, 관측각 등)를 그대로 이용하여 계산한 위성영상 기하는 총 35개의 지상기준점과 검사점에 대하여 거의 일정한 변화량을 지녔으며, 이를 통해 SPOT 4 위성영상에 시선벡터조정모델을 적용할 수 있음을 확인하였다. 시선벡터조정모델을 적용하여 영상에 고르게 분포하는 지상기준점을 2점에서 10점까지 변화시키면서 검사점의 오차를 계산하였고, 25개 검사점 오차는 모두 1픽셀 미만이었다. 새로운 접근 방법인 이 모델은 2점 이상의 지상기준점을 이용하여 SPOT 4 영상 기하를 효과적으로 보정하였으며, 또한 SPOT 영상과 촬영방식이 동일한 고해상 위성영상에 대해서도 좋은 결과를 얻을 것으로 기대한다.

UHF 대역 장거리 항공 통신 시험의 전파 손실 분석 (Analysis of UHF-Band Propagation Loss in Long-distance Air-to-Ground Communication Tests)

  • 장민수;김규환;김재환;이재문;황찬호
    • 한국산학기술학회논문지
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    • 제19권8호
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    • pp.55-63
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    • 2018
  • 본 논문에서는 지상 수신기와 항공기 탑재 송신기 간의 장거리 통신시험을 통해 UHF 대역의 전파 수신세기를 측정하고 그 결과를 분석하였다. 지상 수신기는 제주도 해발 1,100m 지점에 위치시키고 항공 탑재 송신기는 지상 수신기로부터 150km에서 220km 거리를 3.5km 이상의 고도로 비행하며 시험을 수행하였다. 이 경우 지상 수신기와 항공 송신기는 가시선(LOS ; Line of Sight)이 확보되는 환경이므로 자유공간손실(FSL ; Free Space Loss)을 토대로 결과를 예측하고 분석을 하는 경우가 일반적이다. 하지만 본 시험의 경우 지상 수신기와 항공 송신기 사이에 해수면이 존재하고, 장거리 통신 환경으로 인하여 반사면에 대한 입사각이 매우 작은 조건으로 직접 파의 자유공간손실 만으로는 정확한 예측 및 분석이 불가능하다. 따라서 주변에 장애물이 없고 두 안테나 사이 가시선이 확보되는 조건을 고려하여 평면 반사 모델과 구면 대지 반사 모델을 토대로 경로 손실을 예측하고 실제 시험결과와 비교하였다. 비교 결과, 구면 대지 반사모델에서 예측한 전파경로 손실 값과 실제 측정결과가 매우 유사한 특성을 보였다.

칼만필터링을 사용한 목표물 추적시스템의 설계 (Design of Target Tracking System using Kalman Filtering)

  • 김종화;이만형
    • 대한전기학회논문지
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    • 제37권9호
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    • pp.636-645
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    • 1988
  • A new filter algorithm is suggested improving structurally the conventional extended Kalman filter of which the performance is dependent on the selection of the reference axes, by use of line-of-sight axes and gain rotation technique. The implementation method using microcomputer which implements tracking Kalman filter is introduced in terms of hardware and software. Then, through the simulation the performance of suggested filter is compared with that of conventional extended Kalman filter and the possibility of the real time tracking of moving target is investigated.

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A METHOD FOR DETERMINING MAGNETIC HELICITY OF SOLAR ACTIVE REGIONS FROM SOHO/MDI MAGNETO GRAMS

  • CHAE JONGCHUL;JEONG HYEWON
    • 천문학회지
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    • 제38권2호
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    • pp.295-298
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    • 2005
  • Recently a big progress has been made on the measurements of magnetic helicity of solar active regions based on photospheric magnetograms . In this paper, we present the details of Chae's method of determining the rate of helicity transfer using line-of-sight magnetograms such as taken by SORO /MDI. The method is specifically applied to full-disk magnetograms that are routinely taken at 96-minute cadence.