• 한국화재소방학회논문지
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• 제25권2호
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• pp.101-106
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• 2011

본 연구에서는 예기치 않는 화재 등의 재해가 돌발적으로 발생하였을 경우 소리 정보에 의해서 사람들을 적극적으로 올바른 방향으로 피난 유도시키려면 피난자가 유도 정보의 내용을 알아들을 뿐만 아니라 피난 방향도 지각할 수 있는 것이 필요하다. 이에 피난 유도음의 방향을 감지할 수 있는 선행음 효과를 이용하여 각 건물공간에서 선행음과 후속음에 대해서 음압레벨 변화와 지연시간 변화에 따른 청감실험 결과 즉, 최적의 음성 피난유도음을 도출하였다. 각 실내공간에서 최적의 음성 피난 유도음은 다음과 같다. 1) 강의실 공간에서 음성 피난 유도음의 최적의 조건은 선행음보다 후속음이 지연시간을 10ms~50ms 갖는 경우와 선행음과 후속음의 음압레벨 차이가 없거나 선행음이 높은 경우에 선행음 방향에 대하여 양호하게 인지하였다. 2) 복도 공간에서의 최적의 음성 피난 유도음은 선행음보다 후속음이 지연시간 20~60ms인 경우에 선행음에 대하여 양호하게 인지하였다. 3) 체육관에서는 최적의 음성 피난유도음은 선행음보다 후속음이 지연시간 10~40ms인 경우와 선행음이 후속음보다 음압레벨이 크거나 같은 경우에 선행음에 대하여 양호하게 인지하였다.

• 한국펄프종이공학회:학술대회논문집
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• 한국펄프종이공학회 2002년도 추계학술발표논문집
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• pp.74-80
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• 2002

A mathematical tension model for a moving web in a multi-span web handling system was derived and validated by using a simulator which includes unwinder, driven roller, winder, load cells, controllers, etc. A tension controller was designed to compensate tension disturbances generated by velocity changes of the unwinder and driven roller. From experimental results it was proved that the tension model properly expressed the tension behavior of a moving web for specific conditions. The distributed tension controller designed by using the pole-placement technique compensated the tension disturbances transfered from upsteram tension variation. Interactions between web spans including "tension transfer phenomenon" were clearly confirmed through the study. A mathematical model of lateral motion of a moving web was verified also by using the same experimental apparatus which includes displacement type guidance systems. And a feedforward control strategy was designed for more accurate control of the lateral motion of a moving web, which utilize a measured signal of the lateral displacement of web in a previous span and a more correctly identified mathematical model to estimate the disturbance of lateral motion from the previous span. This approach was turned out to be effective in improving the performance of the guidance system for more wide range disturbances.

• 대기
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• 제25권2호
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• pp.367-374
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• 2015

Korean Peninsula has high potential for occurrence of aviation turbulence. A Korean aviation Turbulence Guidance (KTG) system focused on the Korean Peninsula, named Korean-Peninsula KTG (KP-KTG) system, is developed using the high resolution (horizontal grid spacing of 1.5 km) Local Data Assimilation and Prediction System (LDAPS) of the Korea Meteorological Administration (KMA). The KP-KTG system is constructed first by selection of 15 best diagnostics of aviation turbulence using the method of probability of detection (POD) with pilot reports (PIREPs) and the LDAPS analysis data. The 15 best diagnostics are combined into an ensemble KTG predictor, named KP-KTG, with their weighting scores computed by the values of area under curve (AUC) of each diagnostics. The performance of the KP-KTG, represented by AUC, is larger than 0.84 in the recent two years (June 2012~May 2014), which is very good considering relatively small number of PIREPs. The KP-KTG can provide localized turbulence forecasting in Korean Peninsula, and its skill score is as good as that of the operational-KTG conducting in East Asia.

• Journal of Electrical Engineering and Technology
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• 제10권2호
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• pp.647-652
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• 2015

A fully coupled finite element analysis (FEA) technique was developed for analyzing the discharge phenomena and dielectric liquid flow while considering surface charge density effects in dielectric flow guidance. In addition, the simulated speed of surface charge propagation was compared and verified with the experimental results shown in the literature. Recently, electrohydrodynamics (EHD) techniques have been widely applied to enhance the cooling performance of electromagnetic systems by utilizing gaseous or liquid media. The main advantage of EHD techniques is the non-contact and low-noise nature of smart control using an electric field. In some cases, flow can be achieved using only a main electric field source. The driving sources in EHD flow are ionization in the breakdown region and ionic dissociation in the sub-breakdown region. Dielectric guidance can be used to enhance the speed of discharge propagation and fluidic flow along the direction of the electric field. To analyze this EHD phenomenon, in this study, the fully coupled FEA was composed of Poisson's equation for an electric field, charge continuity equations in the form of the Nernst-Planck equation for ions, and the Navier-Stokes equation for an incompressible fluidic flow. To develop a generalized numerical technique for various EHD phenomena that considers fluidic flow effects including dielectric flow guidance, we examined the surface charge accumulation on a dielectric surface and ionization, dissociation, and recombination effects.

• 로봇학회논문지
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• 제8권3호
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• pp.217-227
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• 2013

We introduce a learning system for the sight reading of simple drum sequences. Sight reading is a cognitive-motor skill that requires reading of music symbols and actions of multiple limbs for playing the music. The system provides knowledge of results (KR) pertaining to the learner's performance by color-coding music symbols, and guides the learner by indicating the corresponding action for a given music symbol using additional auditory or vibrotactile cues. To evaluate the effects of KR and guidance cues, three learning methods were experimentally compared: KR only, KR with auditory cues, and KR with vibrotactile cues. The task was to play a random 16-note-long drum sequence displayed on a screen. Thirty university students learned the task using one of the learning methods in a between-subjects design. The experimental results did not show statistically significant differences between the methods in terms of task accuracy and completion time.

• 한국항공우주학회지
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• 제43권8호
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• pp.669-676
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• 2015

본 논문에서는 기동하는 표적에 대한 입사각 제어 유도법칙을 제안하였다. 제안된 유도법칙은 정지표적에 대한 최적입사각제어 유도법칙을 변형한 것으로서 기존의 PN(Proportional Navigation) 유도법칙에 입사각제어 항이 추가된 바이어스 PN 유도법칙의 형태를 갖는다. 시선각, 비행경로각, 그리고 표적에 대한 상대 비행경로각 관점에서의 세 가지 다른 종류의 입사각을 정의하였다. 다양한 공대공 교전 시나리오에 대한 수치 시뮬레이션을 통해 제안한 유도법칙의 성능을 검증하였다.

• 제어로봇시스템학회논문지
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• 제18권9호
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• pp.878-886
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• 2012

This paper investigates the implementation and flight test of realtime vision guided autopilot system based on virtual instrumentation platform. A graphical design process via virtual instrumentation platform is fully used for the image processing, communication between systems, vehicle dynamics control, and vision coupled guidance algorithms. A significatnt ojective of the algorithm is to achieve an environment robust autopilot despite wind and an irregular image acquisition condition. For a robust vision guided path tracking and hovering performance, the flight path guidance logic is combined in a multi conditional basis with the position estimation algorithm coupled with the vehicle attitude dynamics. An onboard flight test equipped with the developed realtime vision guided autopilot system is done using the rotary UAV system with full attitude control capability. Outdoor flight test demonstrated that the designed vision guided autopilot system succeeded in UAV's hovering on top of ground target within about several meters under geenral windy environment.

• 한국항공우주학회지
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• 제50권4호
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• pp.251-257
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• 2022

본 논문에서는 재사용 발사체의 종말 연착륙 구간 비행 제어를 위한 컨벡스 최적화 기반 최소 연료 정밀 착륙 문제를 수립하고 이분탐색을 통해 최단 시간 연착륙 비행궤적을 도출하였다. 계산된 유도 명령 추종을 위해 자세 제어 루프와 구동력 분배 문제를 수립하고 해결함으로 재사용 발사체의 착륙 영역 비행제어계 구조를 완성하였다. 완성된 비행제어계의 착륙 유도성능은 6-자유도 시뮬레이션을 통해 구현되고 분석되었다.

• 국제학술발표논문집
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• The 3th International Conference on Construction Engineering and Project Management
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• pp.935-941
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• 2009

In competitive society, performance management is an essential element of business success. Despite the importance of performance management, it has not been widely implemented in construction companies. In the recent years, construction companies have become more aware of its need to identify, implement, and sustain performance improvements more systematically. Thus, the objective of this paper is to develop performance management system (PMS) for construction companies. The roles of performance management system is not only measuring performance but also offering guidance to improve performance. Therefore, PMS needs benchmarking process that provides Best Practice and new knowledge. This paper investigates the case of PMSs in UK, USA, Brazil, and Chile and discusses the lessons learned. To overcome the limitations of existing PMSs, new performance measurement framework, in form of 'Construction' BSC, is proposed. Based on the 'Construction' BSC, key performance indicators are derived and methodology of performance management is suggested. This paper concludes by developing PMS for benchmarking in construction companies and recommending some further directions on this research topic.

• 전자공학회논문지SC
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• 제46권1호
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• pp.87-96
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• 2009

기존의 방법에서는 비선형 운동 물체의 운동 방정식을 선형화하므로써 비행체의 운동 상태방정식을 구하고, 각 제어 기관에 따라 전달함수를 구하여 안정성 판별과 더불어 제어기를 설계하였다. 이러한 설계 방법으로는 일반적인 비행기와 같은 형태, 비행 환경이 급격하게 변하지 않고 속도가 빠르지 않는 비행체의 유도/제어기 설계에 많이 사용되어 많은 성능을 발휘할 수 있다. 그러나 이러한 설계 방법은 통상적이지 않는 비행체 형태뿐만 아니라 빠른 속도에서 급격한 움직임을 갖는 비행체에서는, 기존의 유도/제어기 설계 방법으로는 이러한 비선형성으로 인하여 제어성(경로문제)과 안정성(안정화문제)을 동시에 충족할만한 성능을 발휘 할 수 없다. 따라서 본 논문에서는 이러한 불확실성이 내포된 비행체 제어 문제에서 제어성과 안정성을 동시에 충족시키기 위한 과정 중 먼저 제어성 문제를 해결하기 위한 비행체 제어성을 분석하고 모델을 제시한다. 또한 본 논문에서 비행체 모델과 동역학 모델에서 제어 요소로서 하중(중력수)을 설정하고 비행 특성에 따른 제어요소 값을 살펴본다. 이것은 Min 설계 방법 1단계이다.