• 한국지능시스템학회논문지
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• 제27권2호
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• pp.170-178
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• 2017

본 논문은 무인잠수정의 동특성을 고려하지 않아 실제로 항행이 불가능한 급격히 변화하는 경로를 계획하기도 하는 기존 $A^*$ 알고리즘 기반 경로계획의 단점을 개선하기 위하여, 무인잠수정의 동특성을 고려한 항행궤적에 기반한 개선된 경로계획 알고리즘을 제안한다. 기존의 $A^*$ 기반 알고리즘은 무인잠수정이 인접노드로 이동하는 경로를 직선으로 가정하여 이동비용을 계산하는 반면, 개선된 경로계획 알고리즘은 경로점 제어에 의하여 생성된 현실적 항행궤적을 노드 간의 이동경로로 설정하고 이동비용을 계산하여 최적의 경로를 계획한다. 모의실험에서 제안한 기법과 기존의 기법의 경로계획을 비교하여 본 논문의 논의가 타당함을 보인다.

• 한국항해항만학회:학술대회논문집
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• 한국항해항만학회 2006년도 International Symposium on GPS/GNSS Vol.2
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• pp.83-88
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• 2006

Many applications in the area of location-based services and personal navigation require nowadays the location determination of a user not only in outdoor environment but also indoor. To locate a person or object in a building, systems that use either infrared, ultrasonic or radio signals, and visible light for optical tracking have been developed. The use of WiFi for location determination has the advantage that no transmitters or receivers have to be installed in the building like in the case of infrared and ultrasonic based location systems. WiFi positioning technology adopts IEEE802.11x standard, by observing the radio signals from access points installed inside a building. These access points can be found nowadays in our daily environment, e.g. in many office buildings, public spaces and in urban areas. The principle of operation of location determination using WiFi signals is based on the measurement of the signal strengths to the surrounding available access points at a mobile terminal (e.g. PDA, notebook PC). An estimate of the location of the terminal is then obtained on the basis of these measurements and a signal propagation model inside the building. The signal propagation model can be obtained using simulations or with prior calibration measurements at known locations in an offline phase. The most common location determination approach is based on signal propagation patterns, namely WiFi fingerprinting. In this paper the underlying technology is briefly reviewed followed by an investigation of two WiFi positioning systems. Testing of the system is performed in two localization test beds, one at the Vienna University of Technology and the second at the Hong Kong Polytechnic University. First test showed that the trajectory of a moving user could be obtained with a standard deviation of about ${\pm}$ 3 m.

• 항공우주기술
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• 제7권1호
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• pp.229-235
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• 2008

지상국비행종단지령장비는 위성발사체(KSLV)발사 후 비행 중 일어날 수 있는 비상사태 (안전영역을 벗어나거나 지상에서 더 이상 추적이 불가능할 경우)에 대하여 지상통제장치에서 비행종단을 명령하여 비행을 강제로 종단시키는 역할을 한다. 본 글에서는 나로우주센터에서 위성발사체(KSLV) 발사를 위하여 설치 운용될 지상국비행종단지령장비의 설계에 관한 기본사항을 서술하고 있다. 국내 환경에 맞는 최적의 시스템 설계를 위하여 위성발사체의 비행궤적 및 특성을 고려한 운용개념을 먼저 정의하였고, 발사체에 탑재되는 수신부 특성을 고려하여 RF Link Budget 분석 및 송신시스템의 RF 요구 성능, 신뢰도 및 가용도 등을 분석하였다. 본 분석을 바탕으로 위성발사체(KSLV)에 비행종단명령을 안정적으로 생성, 처리하여 전송할 수 있는 각각의 장비를 설계하였다.

• Nuclear Engineering and Technology
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• 제53권9호
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• pp.3026-3034
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• 2021

Multi-target X-ray tube is a new type X-ray source, and can be applied in many fields such as sensitive X-ray fluorescence analysis and medical imaging. In this work, we report an electric field modulation multi-target X-ray tube, which contains four targets (Cr, Ni, Au, Mo) coated on a Beryllium (Be) window. A four-valve electric field deflector was developed to deflect the electron beam to bombard the corresponding targets. Particle dynamics analysis software was employed to simulate the particle tracking of electron beam. The results show that the 30 keV electron beam could get a 6.7 mm displacement on the target plane by 10⁵ V/m electric field. The focus areas are about 2 mm × 5 mm and 4 mm × 2.5 mm after deflection in two directions. Thermal behavior calculated by ANSYS shows that the designed target assembly could withstand a 10 W continuous power. The optimum target thicknesses and emission spectra were obtained by Geant4 when the thickness of Be window was 300 mm and the electron beam incident angle was 0.141 rad. The results indicate that this multi-target X-ray tube could provide different X-ray sources effectively.

• 한국전자파학회논문지
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• 제29권11호
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• pp.898-905
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• 2018

본 논문에서는 대지, 대공 표적을 포착 추적할 수 있는 적외선 및 가시광 센서가 탑재된 이종센서 영상탐색기의 종합 성능시험을 위해 구축한 HILS(Hardware In-the-Loop Simulation) 시스템 내에 적외선 표적원을 제안한다. 이 통합시스템은 다양한 종류의 표적과 시나리오 기반 이동 표적의 궤적을 모사하기 위해 열원 및 광원을 출력하는 100개의 모듈로 구성하였다. 또한 표적에 대한 위치, 속도, 방향, 배경 클러터와 재밍 환경 등을 모사할 수 있다. 이종센서 영상탐색기의 시험평가를 위해 구축된 HILS 시스템의 전체 시스템 구성과 적외선 표적원의 설계 및 측정 결과를 제시한다. 향후에, 구축된 HILS 시스템에서 모의비행 시나리오 기반으로 동적 실시간 포착 추적에 대한 단일 또는 이종센서가 탑재된 이종센서 영상탐색기의 성능을 시험할 예정이다.

• 수산해양기술연구
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• 제55권2호
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• pp.129-137
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• 2019

This study was conducted to investigate the effects of underwater noise caused by pile driving during marine construction on fish. In this study, the three gray rockfish were released about 1 km away from the construction site of wind power generation on July 18, 2018 and traced using two acoustic telemetry techniques. The behavior of the fish was analyzed by calculating the moving distance, swimming speed and direction of the gray rockfish. In the results of the acoustic tracking using the ship, the rockfish moved about 2.11 km for about two hours at a speed of $0.28{\pm}0.14m/s$ (0.94 TL/s). The bottom depth of the trajectory of the rockfish was $1.0{\pm}0.6m$ on average. There was a significant directionality in swimming direction of the gray rockfish, and there was no significant correlation between the swimming direction and tidal current direction. Moving distance during 5 minutes (5MD) during pile driving and finishing operations between rock surface and bedrock were 0.94-0.96 times (76.0-77.0 m) and 1.81-2.73 times (146.0-219.5 m), respectively, compared with no pile driving. This study is expected to be used as a basic data of fish behavior research on underwater noise.

• 한국항공우주학회지
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• 제50권12호
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• pp.867-875
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• 2022

본 논문에서는 달착륙선이 국내 개발된 발사체 상단에 탑재되어 지구 저궤도에 투입되고, 이후 달 전이 궤도 투입 기동을 통해 달에 착륙할 경우에 대한 예비 임무 분석을 수행하였다. 각각의 장단점이 있는 직접 착륙 방식 및 간접 착륙 방식을 모두 적용해보았으며, 2030년 음력 10월에 발사할 경우 발사 일에 따른 전이 궤도 특성을 분석하였다. 여기에 미국의 달착륙선 Surveyor-1과 같이 일식 조건, 태양 고도각 조건 및 추적 가능 시간대를 만족시키는 발사 일을 분석해 보았다. 직접 착륙 방식의 경우는 음력 10월중 4일, 간접 착륙 방식의 경우는 3일에 발사할 경우 근지점 이각과 일식 조건에 있어서 가장 적합한 발사일로 분석되었다.

• 제어로봇시스템학회논문지
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• 제20권2호
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• pp.218-222
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• 2014

In this paper, we introduce an autonomous calibration method for a 2D laser displacement sensor (e.g. laser vision sensor and laser range finder) by matching a single point on a flat structure. Many arc welding robots install a 2D laser displacement sensor to expand their application by recognizing their environment (e.g. base metal and seam). In such systems, sensing data should be transformed to the robot's coordinates, and the geometric relation (i.e. rotation and translation) between the robot's coordinates and sensor coordinates should be known for the transformation. Calibration means the inference process of geometric relation between the sensor and robot. Generally, the matching of more than 3 points is required to infer the geometric relation. However, we introduce a novel method to calibrate using only 1 point matching and use a specific flat structure (i.e. circular hole) which enables us to find the geometric relation with a single point matching. We make the rotation component of the calibration results as a constant to use only a single point by moving a robot to a specific pose. The flat structure can be installed easily in a manufacturing site, because the structure does not have a volume (i.e. almost 2D structure). The calibration process is fully autonomous and does not need any manual operation. A robot which installed the sensor moves to the specific pose by sensing features of the circular hole such as length of chord and center position of the chord. We show the precision of the proposed method by performing repetitive experiments in various situations. Furthermore, we applied the result of the proposed method to sensor based seam tracking with a robot, and report the difference of the robot's TCP (Tool Center Point) trajectory. This experiment shows that the proposed method ensures precision.

• 한국항공우주학회지
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• 제40권1호
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• pp.23-34
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• 2012

우주 발사체는 치밀한 비행 계획에 따라 사전에 결정된 경로를 비행하도록 설계된다. 그러나 비정상으로 추력이 종료되거나 계획된 비행경로를 이탈한 경우, 또는 자유 낙하 중인 대기권 재진입 발사체에 대한 추적 과정에서 추적 센서의 측정이 불가하게 된 경우 등에는 별도의 추적 장비를 이용한 추적 또는 신속한 낙하지점 추정이 필요하다. 본 논문에서는 클러터 환경에서 무추력 탄도 비행 중인 발사체에 대한 위치 정보를 획득하고 트랙을 생성 및 유지하기 위하여 Integrated Track Splitting(ITS) 알고리듬과 Extended Kalman Filter(EKF)를 결합한 ITS-EKF 알고리듬 적용을 제안한다. 따라서 대기권 재진입 발사체에 대하여 ITS-EKF 알고리듬을 적용한 시뮬레이션을 통해 추적 성능 확인 및 지상 낙하지점을 추정한다. ITS-EKF 알고리듬 적용 결과의 적절성을 확인하기 위하여 ITS와 Particle Filter를 결합한 ITS-PF 알고리듬을 적용하여 구한 추적 성능 및 낙하지점 분포 결과와 비교하여 제시된 알고리듬이 효과적인 실시간 On-line 낙하지점 추정에 사용이 가능함을 확인한다.

• Journal of Astronomy and Space Sciences
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• 제33권2호
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• pp.127-135
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• 2016

Inactive space objects are usually rotating and tumbling as a result of internal or external forces. KOREASAT 1 has been inactive since 2005, and its drift trajectory has been monitored with the optical wide-field patrol network (OWL-Net). However, a quantitative analysis of KOREASAT 1 in regard to the attitude evolution has never been performed. Here, two optical tracking systems were used to acquire raw measurements to analyze the rotation period of two inactive satellites. During the optical campaign in 2013, KOREASAT 1 was observed by a 0.6 m class optical telescope operated by the Korea Astronomy and Space Science Institute (KASI). The rotation period of KOREASAT 1 was analyzed with the light curves from the photometry results. The rotation periods of the low Earth orbit (LEO) satellite ASTRO-H after break-up were detected by OWL-Net on April 7, 2016. We analyzed the magnitude variation of each satellite by differential photometry and made comparisons with the star catalog. The illumination effect caused by the phase angle between the Sun and the target satellite was corrected with the system tool kit (STK) and two line element (TLE) technique. Finally, we determined the rotation period of two inactive satellites on LEO and geostationary Earth orbit (GEO) with light curves from the photometry. The main rotation periods were determined to be 5.2 sec for ASTRO-H and 74 sec for KOREASAT 1.