• 한국항공운항학회:학술대회논문집
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• 2015.11a
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• pp.191-197
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• 2015

본 논문에서는 공항 지상 감시 장비(ASDE: Airport Surface Detection Equipment) 데이터를 이용하여 항공기의 지상이동 운항모드를 추정하는 방법을 제안하였다. 제안된 방법에서는 항공기의 운항모드와 그에 따라 관측되는 속도 및 가속도를 확률 변수로 정의함으로써, 확률적 추정방법을 통해 운항모드를 추정하였다. 운항모드를 추정하기 위한 모형으로서는 은닉 마르코프 모형(HMM: Hidden Markov Model)을 사용하였으며 실제 ASDE 데이터를 통해 제안된 방법의 성능을 검증해 보았다.

• The Bulletin of The Korean Astronomical Society
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• v.37 no.2
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• pp.225.2-225.2
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• 2012

저궤도 관측용 다중 카메라를 통해 고해상도 위성을 제공할 수 있으며, 지도 제작이나 환경, 농업, 해양 지역 모니터링 등의 목적으로 사용될 수 있다. 특히 항공촬영 및 지구 관측을 통해 수치표고모델(DEM) 추출을 함으로써 촬영지역의 고도정보를 포함하는 입체영상을 얻는데 유용하다. 또한, 달 관측을 위한 관측위성에 장착할 경우 달 표면의 지형을 정밀하게 얻어내어 달표면 고도 지형 지도제작 및 향후 달 탐사선을 통한 달 탐사 시 탐사지역 선정에 필요한 정보를 제공할 수 있다. 다중 카메라를 포함한 탑재체 시스템은 크게 광학부와 카메라 전자부로 구성된다. 광학부에서는 입체촬영 및 줌인이 가능한 광학계를 제공하며, 카메라 전자부에서는 광학계를 통해 검출기로 입사되는 빛에너지를 전자신호로 변환하고, 이를 카메라 전자부 영상출력 형식으로 변환하게 된다. 특히, 다중카메라를 각각 제어하기 위한 정밀제어로직, 다양한 촬영 지원 모드, 다중카메라 영상자료 및 영상처리를 위한 추가적인 영상정보를 제공한다. 본 논문에서는 저궤도 관측용 다중 카메라를 이용한 다양한 활용에 따른 각 모드별 성능분석방법을 제안한다. 이를 위해 각 촬영조건에 따라 필요한 파라미터를 분석하고 실제 활용시 예상되는 성능을 분석해 본다. 또한 다중카메라를 통해 얻어진 영상을 처리하는데 필요한 처리 과정 및 처리된 영상을 활용하는 방법을 제시한다. 특히 다중 카메라 촬영을 통해 얻어진 영상데이터의 특성을 알아보고, 이를 보정 및 처리하기 위해 필요한 추가 적인 정보, 영상파라미터, 처리 단계 및 최종결과물을 검증하는 방법을 제시한다.

• Proceedings of the KIEE Conference
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• 2007.10c
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• pp.141-143
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• 2007

본 논문은 매입형 영구자석 동기전동기의 속도 센서리스의 제어 방법에 관한 것이다. 매입형 영구자석 동기전동기의 센서리스 구동을 위하여 적응 적분바이너리 관측기와 적응 슬라이딩 모드 관측기를 이용하였다. 두 관측기의 성능 비교를 위하여 매입형 영구자석 동기전동기의 고정자 전압방정식으로부터 각각 관측기를 구성하였고, 동일한 시스템에서의 실험을 통하여 관측기의 성능을 비교하였다.

• Journal of Satellite, Information and Communications
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• v.9 no.2
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• pp.74-79
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• 2014

Conventional ScanSAR mode has been adopted in Envisat or Radarsat and played an important role to acquire wide swath SAR images for environmental surveillance. However, it suffers from the undesirable scalloping effect caused by non-homogeneity of antenna pattern while the image resolution is sacrificed. In recent years, TOPS mode has been suggested and put into use to overcome the disadvantages of the conventional scanning mode. Although TOPS mode is able to produce wide-swath SAR image in a short time interval, it demands highly complicated system design knowledge. In this paper, we present the operation principle of TOPS mode and a full SAR simulation is performed to generate TOPS SAR raw data. Azimuth antenna pattern is modified during TOPS mode operation and it is shown that the undesired scalloping effect is suppressed in the generated SAR image.

• Journal of Power System Engineering
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• v.10 no.4
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• pp.172-180
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• 2006

본 논문은 Dijkstra 알고리즘에 기초한 최단거리 경로계획을 하며 이 경로를 추적하기 위한 슬라이딩 모드 제어를 제시한다. 슬라이딩 모드 제어기는 동적매개변수 불확실성과 입력외란이 존재 시에도 강인 점근적으로 계획된 경로를 추적하도록 한다. 더불어 작업장 내의 이동로봇의 위치를 USB 카메라에 의해 감지하며, Pin-hole 카메라모델로 하여 카메라에 의해 관측되는 작업장 내의 이륜구동로봇의 위치좌표를 결정하였으며, 이 위치를 정확히 감지하기 위해 Tsai법을 사용하여 카메라 보정한다. 시뮬레이션 결과는 슬라이딩 모드 제어기의 성능을 검증하기 위해 보였다.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.1 no.2
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• pp.63-68
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• 2000

A passively mode-locked ring type fiber laser had been installed in order to get the short pulses The single and the double mode-locking were appeared, and the shortest pulse length of 65 fs was obtained with a 110 m long dispersion shifted fiber(DSF) in a local cavity of 139.8 m. Also high order harmonic modelocking of 17th and Q-switched high order harmonic modelocking were obtained.

• Journal of the Korea Institute of Information and Communication Engineering
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• v.17 no.1
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• pp.151-157
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• 2013

In this paper, a comparative analysis of PBTI induced device degradation in nanowire n-channel junctionless and inversion mode Multiple-Gate MOSFET(MuGFETs) has been performed. It has been observed that the threshold voltage is increased after PBTI stress and the threshold voltage variation of junctionless device is less significant than that of inversion mode device. However the degradation rate of junctionless device is less significant than that of inversion mode device. The activation energy of the device degradation is larger in inversion mode device than junctionless device. In order to analyze the more significant PBTI induced device degradation in inversion mode device than junctionless device, 3-dimensional device simulation has been performed. The electron concentration in inversion mode device is equal to the one in junctionless device but the electric field in inversion mode device is larger than junctionless device.

• Journal of Aerospace System Engineering
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• v.16 no.5
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• pp.49-56
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• 2022

S-STEP is a small SAR satellite mission that monitors time-limited emergency targets and military anomalies in areas of interest, achieving the average revisit in less than 30 minutes by deploying a constellation of 32 satellites in low orbit at an altitude of 510 km. The mission operation mode of S-STEP is divided into normal mode, observation mode, communication mode, and orbit maintenance mode. Further,, the attitude control mode is subdivides into initial detumbling, sun pointing, target pointing, ground station pointing, and thrust direction maintenance. Based on the preliminary mission operational scenario and the satellite's characteristics, this study analyzed the attitude control performance during initial detumbling and observation modes. It verifies that each mode's attitude control accuracy requirements within the time allotted by the scenario of the S-STEP achieved.

• The Sea:JOURNAL OF THE KOREAN SOCIETY OF OCEANOGRAPHY
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• v.17 no.2
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• pp.130-137
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• 2012

The underwater glider using conception of Lagrangian method, is a new observation platform to understand the properties of the ocean vertically. In 2011 March, KORDI made a first successful autonomous trip from Hupo to west coast of Uleungdo piloting Littoral Glider of Alaska Native Technology LLC. The journey considered many environmental variables and route vigilantly selected, the glider covered 177 km horizontally and took approximately 6 days (153 hours). Despite the existence of 1 kt eddy current, Sound velocity sampling was conducted from 5 meters and reaching maximum of 200 meters depth at each dive. It successfully collected sound velocity and temperature profile at every 5 seconds totaling up to 1408 profiles using SVT&P sensor. During the flight it was also a mission to check the diverse modes of the glider i.e. spiral, waypoints, heading, drift and hover could function without a defect in a given situation. These modes were thoroughly monitored and it could be considered that the glider handled it well during the flight. As a result of this test flight, it was evident that the given underwater glider could operate under 2kt current environment with users defined heading and depth, also with the payload up to 5 kg without changing internal buoyancy.

• Journal of the Korea Institute of Information and Communication Engineering
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• v.17 no.9
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• pp.2133-2138
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• 2013

In this paper, the variation of a steep subthreshold slope at elevated temperature in nanowire n-channel junctionless and inversion mode MuGFETs has been compared. It has been observed that the subthreshold slopes are increased with the increase of the operation temperature in junctionless and inversio-mode transistors. The variation of a subthreshold slope with operation temperature is more significant in junctionless transistor than inversion-mode transistor. The temperature dependence on the variation of a subthreshold slope for different fin widths shows a similar behavior regardless of fin width. From the temperature dependence on the variation of a subthreshold slope for different substrate biases, it has been observed that the variation of a subthreshold slope is less significant when the substrate bias was applied. It is worth noting that one can achieve a subthreshold slope of below 41mV/dec at elevated temperature of 400K using the junctionless MuGFETs with a positive substrate bias.