• 한국지능시스템학회논문지
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• 제25권4호
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• pp.398-404
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• 2015

본 논문에서는 관성측정장치를 기반으로 블루투스 환경에서의 자율비행을 위한 멀티 로터형 헬리콥터에 대한 설계 및 성능을 제시하였다. 멀티 로터관련 다양한 연구가 진행되어오고 있긴 하지만 최근에는 다양한 서비스를 목적으로 짐벌이 장착된 헥사로터형의 헬리콥터에 대한 관심이 모아지고 있다. 따라서, 본 논문에서는 지상의 원격조정 PC나 고성능의 원격제어장치나 영상시스템과 같은 외부보조 시스템 없이 연구와 구조활동, 모니터링 활동을 수행할 수 있는 컴팩트하고 자율비행을 위한 헥사로터(hexa rotor)형 헬리콥터에 대한 하드웨어 및 소프트웨어를 소개하고자 한다. 제안한 시스템은 헥사로터 헬리콥터의 구조와 관성측정장치 관련 하드웨어 구성과 수학적 모델링 및 시뮬레이션 결과를 각각 제시하였다. 또한, IMU 구현을 위하여 MCU(ARM-cortex) 보드를 장착하여 각 로터의 회전과 관성 측정장치의 입력신호에 대한 상태를 제어할 수 있도록 하였다. 그리고 시스템 시뮬레이션과 실험을 통한 시스템의 성능을 각각 검증하였다.

• 한국지반공학회:학술대회논문집
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• 한국지반공학회 2006년도 춘계 학술발표회 논문집
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• pp.784-793
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• 2006

As the number of CFRD constructions increases, the necessity of an accurate assessment on its behavior also has been increasing accordingly. The performance of concrete faced rockfill dam (CFRD) under different water levels is greatly concerned by dam engineers and designers in the world. However, domestic research on CFRD design and construction has yet been insignificant. This study deals with three centrifuge model tests, mainly investigates the deformation of the concrete faced slabs with different face slab stiffness under different water levels. The prototype of a centrifugal model dam is half size of domestic CFRD dam. Detailed material preparation, model design, model set-up, model instrumentation and testing procedures are presented. In order to simulate the prototype concrete faced slab, three kinds of thin fiberglass plates with different thickness was adopted in the three model tests. The water level control facility was specially designed for this experiment to control the water level rise and drawdown during centrifuge flight. Although most of the results from the three model tests are satisfactory, it is also required that the centrifuge test results should be compared with those of numerical analysis and field measurements to analyze the centrifuge test results more in detail.

• 한국항공우주학회지
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• 제43권3호
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• pp.224-231
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• 2015

람다 날개 형상의 공력 계수에 대한 실험적 연구를 국방과학연구소의 중형아음속 풍동에서 수행하였다. 본 연구의 주목적은 옆미끄럼각의 변화에 따라 다양한 공력 계수가 어떻게 변화하는지를 조사하는 것이다. 옆미끄럼각이 $0^{\circ}C$인 경우, 피칭 모멘트가 급격히 불안정해지는 현상을 확인하였으며, 옆미끄럼각이 증가함에 따라 pitch break 현상이 더 높은 받음각에서 발생하는 것을 확인하였다. 롤링 모멘트는 옆미끄럼각이 있는 경우 pitch break와 유사한 특성을 보여준다. 이런 경향은 옆미끄럼각이 증가할수록 더 심하게 나타났다. 요잉 모멘트는 높은 받음각에서 옆미끄럼각에 따라 기울기가 크게 변화하였고 불안정한 방향 안정성이 뚜렷이 나타났다. 모멘트의 이런 특성들은 비행 제어를 위해서는 보다 효과적인 조종성 증가 장치가 필수적이란 것을 의미하고 있다.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2002년도 춘계학술대회논문집
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• pp.441-447
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• 2002

KSR-III(Korea Sounding Rocket - III), which is being developed by Space Technology R&D Division of KARI(Korea Aerospace Research Institute) will be launched in late 2002. It is a three-stage, liquid propellant rocket which can reach 250 km altitude and will carry out observation of ozone layer and scientific experiments, such as microgravity experiment, and atmospheric measurement. KSR-III is believed to be an intermediate to the launch vehicle capable of carrying a satellite to its orbit. Space Test Department of KARI performed GVT(Ground Vibration Test) fer KSR-III EM at Rocket Test Building of KARI. GVT is very important for predicting the behavior of rocket in its operation, developing flight control program and performing aerodynamic analysis. This paper gives an introduction of rocket GVT configuration and information on test procedures, techniques and results of It. In this test. to simulate free-free condition, test object hung in the air laterally by 4 bungee cords specially devised. For the excitation of test object, pure random signal by two electromagnetic shakers was used and total 22 frequency response functions were achieved. Polyreference parameter estimation was performed to identify the modal parameters with MIMO(Multi-Input-Multi-Output) method. As the result of the test, low frequency mode shapes and modal parameters below 60Hz were identified

• Journal of Astronomy and Space Sciences
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• 제30권4호
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• pp.335-344
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• 2013

TRiplet Ionospheric Observatory-CubeSat for Ion, Neutron, Electron & MAgnetic fields (TRIO-CINEMA) is a CubeSat with 3.14 kg in weight and 3-U ($10{\times}10{\times}30$ cm) in size, jointly developed by Kyung Hee University and UC Berkeley to measure magnetic fields of near Earth space and detect plasma particles. When a satellite is launched into orbit, it encounters ultra-high vacuum and extreme temperature. To verify the operation and survivability of the satellite in such an extreme space environment, experimental tests are conducted on the ground using thermal vacuum chamber. This paper describes the temperature control device and monitoring system suitable for CubeSat test environment using the thermal vacuum chamber of the School of Space Research, Kyung Hee University. To build the chamber, we use a general purpose thermal analysis program and NX 6.0 TMG program. We carry out thermal vacuum tests on the two flight models developed by Kyung Hee University based on the thermal model of the TRIO-CINEMA satellite. It is expected from this experiment that proper operation of the satellite in the space environment will be achieved.

• 대한인간공학회지
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• 제28권1호
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• pp.37-51
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• 2009

The nuclear power industry in the world has recognized the importance of integrating non-technical and team skills training with the technical training given to its control room operators to reduce human errors since the Three Mile Island and Chernobyl accidents. The Nuclear power plant (NPP) industry in Korea has been also making efforts to reduce the human errors which largely have contributed to 120 nuclear reactor trips from the year 2001 to 2006. The Crew Resource Management (CRM) training was one of the efforts to reduce the human errors in the nuclear power industry. The CRM was developed as a response to new insights into the causes of aircraft accidents which followed from the introduction of flight recorders and cockpit voice recorders into modern jet aircraft. The CRM first became widely used in the commercial airline industry, but military aviation, shipboard crews, medical and surgical teams, offshore oil crews, and other high-consequence, high-risk, time-critical industry teams soon followed. This study aims to develop a CRM training program that helps to improve plant performance by reducing the number of reactor trips caused by the operators' errors in Korean NPP. The program is; firstly, based on the work we conducted to develop a human factors training from the applications to the Nuclear Power Plant; secondly, based on a number of guidelines from the current practicable literature; thirdly, focused on team skills, such as leadership, situational awareness, teamwork, and communication, which have been widely known to be critical for improving the operational performance and reducing human errors in Korean NPPs; lastly, similar to the event-based training approach that many researchers have applied in other domains: aircraft, medical operations, railroads, and offshore oilrigs. We conducted an experiment to test effectiveness of the CRM training program in a condition of simulated control room also. We found that the program made the operators' attitudes and behaviors be improved positively from the experimental results. The more implications of the finding were discussed further in detail.

• 문화기술의 융합
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• 제9권1호
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• pp.697-702
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• 2023

최근 4차 산업혁명의 핵심기술인 드론의 도입으로 학교 교육 현장에서는 드론을 활용한 다양한 융합교육이 진행되고 있다. 특히 자유학기제 수업 및 진로탐색과 연계하여 드론 이론 및 실습 교육을 진행하고 있다. 드론융합 교육프로그램은 단순 시연 실습교육 보다 학습자의 만족도가 높고 직접적인 실습 경험으로 인하여 학습효과가 높게 나타나고 있다. 그러나 다수의 학습자를 상대로 실습교육을 진행하고 있어 한정된 장소에서의 다중드론 비행에 제약 및 학습자 통제가 불가능한 실정이다. 본 논문에서는 학교에서 다중드론 교육 운영 시 교수자가 다수의 드론을 실시간 감시하고 드론 간의 충돌을 사전에 학습자에게 인식시켜 실시간으로 다수의 드론 감시가 가능한 감시시스템을 제안하였다. 실험에서 사용된 통신 모듈은 Murata LoRa에 GPS를 탑재하였고, 실시간으로 수신된 위치 데이터를 기반으로 모니터링이 가능하도록 서버와 클라이언트를 구성하였다. 개방형 공간에서 제안한 시스템의 성능을 평가하였으며, 약 120m 거리까지 통신 신호가 양호함을 확인하였다. 즉 240m 범위 안에서 25대의 교육용 드론의 제어가 가능하고, 교수자가 모니터링할 수 있음을 확인하였다.