• 한국항해항만학회:학술대회논문집
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• 한국항해항만학회 2015년도 추계학술대회
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• pp.95-97
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• 2015

자동충돌예방 교육과 레이더시뮬레이션 교육은 STCW 협약 상 지정된 교육으로 항해사들이 항해사로 승선 시 필수적으로 수료해야 하는 교육이다. 최근에는 지정교육기관기준에 의거 교육과정 및 필요시설의 요건을 권고규정으로 두고 있어 각 교육기관은 그에 맞추어 시뮬레이션 수업을 위한 장비, FMSS(Full Mission Simulator System)을 도입하였다. 본 연구는 도입 후부터 현재까지 FMSS를 이용해서 이루어지고 있는 알파/레이더/시뮬레이션 교육이 어느 정도 효과가 있는지를 정량적으로 분석하기 위해 재학생을 대상으로 1년에 걸쳐 설문조사를 실시하였다. 그리고 분석 결과 응답자들은 수업 전과 비교하여 2.13배 능력이 향상 되었다고 답변하였다. 또한 분석 결과를 바탕으로 시뮬레이션 수업 시 발생하는 문제점을 도출하고 개선방안을 제시하고자 한다.

• 교육시설 논문지
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• 제20권6호
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• pp.3-10
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• 2013

The purpose of this research is to understand the basic correlation between CPTED based 'Safe School Guidelines' and the physical properties of Korean elementary schools. Fundamentally, the guidelines are consisted with phrases that contain a detailed explanation of how the spaces within the school campuses should be and which aspects have to be avoided. Furthermore, the guidelines categorized among the several areas in school are grouped by CPTED elements such as 'Natural Surveillance', 'Territorial Integrity' and 'Natural Access'. The mission of the researchers was to check the applicability of these guidelines for each school samples and investigate which of the categories or subcategories have strong correlation with the current school crime rates. With these results, a new outline of CPTED guideline exclusive to Korean elementary schools will be obtained which can be applied on earlier stages for future school projects.

• Journal of Astronomy and Space Sciences
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• 제21권4호
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• pp.329-342
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• 2004

In this paper, we present preliminary feasibility studies on three types of solar observation payloads for future Korean Science and Technology Satellite (STSAT) programs. The three candidates are (1) an UV imaging telescope, (2) an UV spectrograph, and (3) an X-ray spectrometer. In the case of UV imaging telescope, the most important constraint seems to be the control stability of a satellite in order to obtain a reasonably good spatial resolution. Considering that the current pointing stability estimated from the data of the Far ultraviolet Imaging Spectrograph (FIMS) onboard the Korean STSAT-1, is around 1 arc minutes/sec, we think that it is hard to obtain a spatial resolution sufficient for scientific research by such an UV Imaging Telescope. For solar imaging missions, we realize that an image stabilization system, which is composed of a small guide telescope with limb sensor and a servo controller of secondary mirror, is quite essential for a very good pointing stability of about 0.1 arcsec. An UV spectrograph covering the solar full disk seems to be a good choice in that there is no risk due to poor pointing stability as well as that it can provide us with valuable UV spectral irradiance data valuable for studying their effects on the Earth's atmosphere and satellites. The heritage of the FIMS can be a great advantage of developing the UV spectrograph. Its main disadvantage is that two major missions are in operation or scheduled. Our preliminary investigations show that an X-ray spectrometer for the full disk Sun seems to be the best choice among the three candidates. The reasons are : (1) high temporal and spectral X-ray data are very essential for studying the acceleration process of energetic particles associated with solar flares, (2) we have a good heritage of X-ray detectors including a rocket-borne X-ray detector, (3) in the case of developing countries such as India and Czech, solar X-ray spectrometers were selected as their early stage satellite missions due to their poor pointing stabilities, and (4) there is no planned major mission after currently operating Reuven Ramaty High-Energy Solar Spectroscopic Imager (RHESSI) mission. Finally, we present a preliminary design of a solar X-ray spectrometer covering soft X-ray (2 keV) to gamma ray (10 MeV).

• 항공우주시스템공학회지
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• 제17권4호
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• pp.10-17
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• 2023

본 논문은 한국항공대학교에서 연구 및 개발한 태양광 무인기에 관한 것으로, 주익 4.2 m 장기체공 태양광 무인항공기 KAU-SPUAV-2019에 대한 연구를 기반으로 하여 임무 비행을 위해 개발한 주익 3.0 m 태양광 무인항공기 KAU-SPUAV-2020의 시스템 설계에 관하여 기술하였다. 기체의 경량화를 위하여 동체에 복합재료를 적용하였고, 태양광 충전 시스템을 적용하였다. 임무 수행 활용성을 위하여 비상시 긴급하게 착륙하기 유리하도록 Deep Stall Landing이 가능하도록 제작하였으며, 강제 실속 착륙 시 항공기에 가해지는 충격을 흡수하기 위한 에어백 모듈을 장착하였다. 개발된 3.0 m 태양광 무인항공기의 비행 성능 및 임무 수행 능력은 비행 실험을 통해 그 수행 능력을 검증하였으며, 147 km에 달하는 제주도 해안선을 3 시간 50 분 만에 비행하는 것에 성공함으로 태양광 무인항공기가 다양한 분야에서 촬영, 모니터링 임무에 활용 가능함을 확인하였다.

• 천문학회보
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• 제39권2호
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• pp.108.2-108.2
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• 2014

과거 달 탐사 미션으로 달에는 global magnetic fields는 존재하지 않고 표면에 국부적으로 자기장이 존재함이 확인되었다. 그러나 이렇게 측정된 자기장 데이터는 일정 고도 (> 20 km) 이상에서 측정되었기 때문에, 지표에 비해 그 세기가 매우 약해 자기장의 형태와 분포를 연구하는데 한계가 있다. 보다 자세한 연구를 위해서는 표면에서부터 다양한 고도에 이르는 위치에서 측정된 자기장 데이터가 필요하며, 이는 달 표토의 자화나 Swirl 형성 메커니즘을 이해하는데 중요한 정보이다. 따라서 본 연구에서는 큐브위성을 이용하여 저궤도부터 지표까지의 자기장을 측정하는 방안을 소개한다. 큐브위성은 달 궤도 모선에서 사출되어 자기이상 지역 표면에 충돌하는 임무를 가진다. 자력계는 모선과 큐브위성에 각각 탑재되어 자기장을 측정하며, 모선으로 부터 사출된 큐브위성은 충돌 직전까지 자기장을 측정하고 모선에 습득한 데이터를 실시간으로 전송한다. 이렇게 측정된 자기장 데이터는 모선의 궤도부터 표면에 이르기까지 여러 고도에서 측정되었기 때문에 자기이상 지역의 자기장 구조를 파악하는데 중요한 자료로 활용할 수 있다. 이에 본 연구에서는 달의 자기이상 지역과 큐브위성 임무 설계에 대하여 기술하였다.

• 한국문헌정보학회지
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• 제39권2호
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• pp.57-84
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• 2005

교구$\cdot$ 설비기준은 학교 교육과정을 위한 기본 요소를 의미한다. 지식기반사회에서 학교도서관은 교육과정을 지원하고 정보활용과 독서지도를 위한 기본적인 교육환경이다. 따라서 학교도서관 교구 설비기준은 학교도서관의 사명을 담아야 하며, 교육적 역할에 적합한 구성요소를 포함하여야 한다. 그러나 현행 기준은 양적 질적 측면에서 불충분하다. 따라서 학교교구·설비기준 개정 시, 학교도서관 교구 ·설비기준은 특히 다음과 같은 내용을 포함하여야 한다. 1. 시설 지침; 2. 기본 설비 방안; 3. 교육적 역할에 적합한 교구 기준; 4. 기본 공간별 설비 종목; 5. 보다 상세한 정보기기 종목; 6. 특수학교도서관 기준 개선

• 의학교육논단
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• 제25권1호
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• pp.3-16
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• 2023

Unlike in the past, standards for the quantity and quality of work expected from medical school faculty are continuously rising, causing changes and stress in various areas. This highlights the need for career development among medical school faculty for professional, personal, organizational, and societal reasons. The role of medical school faculty has become more diverse, leading to an increase in the types and levels of competencies required. Medical schools must support their faculty members with diverse identities in fully utilizing their capabilities to achieve the institution's mission. Furthermore, societal changes suggest that career development for medical school faculty will become even more crucial in the future. To achieve this, both individuals and organizations must make efforts and play appropriate roles. For this purpose, medical schools use a combination of promotion and tenure evaluations and faculty development programs, while individual faculty members follow a career path within the medical school environment. Medical school faculty must be able to meet the evolving demands at each stage of their careers. It is important for professors, who engage in career development, to have a clear sense of their identity and values, and to prioritize their career goals. Medical schools should also ensure that the implicit messages they convey align with the organization's explicit values. Finally, proactively preparing for future changes in society and generations is essential from a long-term perspective.

• 반도체디스플레이기술학회지
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• 제21권4호
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• pp.121-125
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• 2022

This paper deals with the development of a deep-learning-based robot that recognizes various types of stairs and performs a mission to go up to the target floor. The overall motion sequence of the robot is performed based on the ROS robot operating system, and it is possible to detect the shape of the stairs required to implement the motion sequence through rapid object recognition through YOLOv4 and Cuda acceleration calculations. Using the ROS operating system installed in Jetson Nano, a system was built to support communication between Arduino DUE and OpenCM 9.04 with heterogeneous hardware and to control the movement of the robot by aligning the received sensors and data. In addition, the web server for robot control was manufactured as ROS web server, and flow chart and basic ROS communication were designed to enable control through computer and smartphone through message passing.

• 천문학회보
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• 제45권1호
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• pp.40.1-40.1
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• 2020

The Korea Astronomy and Space Science Institute is participating as a South Korean partner in the Commercial Lunar Payload Services (CLPS)of NASA. In response, the Korea Astronomy and Space Science Institute is currently conducting basic research for the development of four candidate instrument payloads. The magnetic field instrument is one of them and it's scientific mission objective is the moon's surface magnetic field investigation. Therefore, the development requirement of the lunar surface magnetic field instrument were derived and the initial conceptual design was started. The magnetic field instrument has a 1.2 meter boom which has two three-axis fluxgate magnetometer sensors and one gyro sensor to get a attitude information of the boom. The concept of measuring the lunar surface magnetic field will carry out using multiple sensors by placing semiconductor type magnetic field sensors inside the electric box including boom mounted fluxgate sensors. In order to overcome the very short development period, we will use the KPLO (Korean Lunar Pathfinder Orbiter) magnetometer design and parts to improve reliabilities for this instrument. In this presentation, we introduce the instrument requirements and conceptual design for the Lunar surface magnetic field instruments.

• International Journal of Aeronautical and Space Sciences
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• 제14권1호
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• pp.67-74
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• 2013

Nonlinear guidance law combined with a pseudo pursuit guidance is proposed, to perform stationary target observation mission. Multiple UAVs are considered, with waypoint constraint. The whole guidance is divided into two steps: firstly, waypoint approach, with specified incidence angle; and secondly, loitering around the stationary target. Geometric approach is used to consider the constraint on the waypoint, and a specified phase angle between the loitering UAV and the approaching UAV. In the waypoint approach step, UAVs fly to the waypoint using the pseudo pursuit guidance law. After passing the waypoint, UAVs turn around the target, using a distance error dynamics-based guidance law. Numerical simulations are performed, to verify the performance of the proposed guidance law.