• 가정과삶의질연구
• /
• 제7권2호
• /
• pp.15-30
• /
• 1989

This study deals with the following problems about leisure activity of young people and leisure guidance of mothers, (1) Leisure activity of children by the independent variables, (2) Leisure guidance of mothers by the independent variables. (3) The relation between leisure guidance of mothers and leisure activity of young people. This research used the questionaire survey. The subjects were 830 couples of mother and pupil (pupils of 4, 5 and t grades in six primary school in Kwang-Ju city). The statistics used for data analysis were percentage, t, F-test, X2. The results of this study are summarized as follows; (1) Boys and girls average leisure hours: week days…2 hour, saturday…3 hours, Sunday and holiday…4.5 hours, the school vacation…6.2 hours. And leisure activity showed the significant difference in sex, age, educational level, family form (p 0.001, p 0.05, p 0.010). Generally, they had social & amusing leisure activity. And a hindrance cause of leisure activ ty is due to hard working in learning practice. (2) The necessity of leisure activity showed higher in the aged mother and high educated mother, lower in the poor family. And guidance content showed the significant difference in sex of children(p 0.001), educational level of parents(p 0.05). Actually mothers wanted intellectual leisure activity. (3) The relation between the leisure activity pattern desired by leisure activity of mothers and children pattern showed that mothers demanded the various patterns, but children wanted social & amusing leisure activities mainly. Only children's patterns agreed with mothers in the artistic, intellectual, activities on Saturday and during the vacation. And the relation between mothers satisfaction degree in the leisure activity of children and children's satisfaction degree showed the significant difference (p 0.05). Children's satisfaction degree is high, irrespective of mothers satisfaction degree.

• 지능정보연구
• /
• 제20권2호
• /
• pp.149-162
• /
• 2014

수강지도는 학생의 졸업인증이나 공학교육인증 이수를 위해 수강 신청 이전에 수행되는 과정을 지칭한다. 수강지도는 학생의 수강이력 점검과 향후 수강 과목의 안내 등을 포함하여 학생들의 졸업 및 교과과정 인증과 관련된 중요한 역할을 하고 있다. 현재 대부분 대학에서는 수강지도를 위한 전산시스템의 부재로 인해 지도교수가 직접 수동적으로 수강지도를 진행하고 있다. 하지만 이러한 수동적인 방식의 수강지도는 지도교수가 각 학생에 대한 정보를 분석해야 하고, 때때로 휴먼에러를 일으키게 된다. 수강신청이 학기 단위로 이루어지기 때문에 휴먼에러로부터 발생된 피해는 원상태로 되돌리는 것이 거의 불가능하다. 따라서 수강지도를 진행함에 있어 자동화된 시스템은 필수적인 요소로 판단된다. 관계 데이터 모델을 이용한 수강지도 시스템의 도입은 수동적인 수강지도의 문제점을 해결할 수 있게 해준다. 하지만 교육과정 및 인증제도의 변화에 따라 기존 시스템의 스키마 변경이 요구되고, 수강 과목 사이에 존재하는 관계 및 의미적인 검색을 제공하는 것이 어렵다는 한계가 존재한다. 본 논문에서는 수강지도 시스템을 위한 수강지도 온톨로지를 모델링하고, 온톨로지 기반의 수강지도 시스템을 설계한다. 온톨로지 인스턴스 생성을 위해 JENA 프레임워크를 이용하여 온톨로지 생성 모듈을 개발하였고, 실험에 참가한 학생의 수강 이력 데이터를 기반으로 온톨로지 인스턴스를 생성하고 추론과정을 통해 트리플 저장소에 저장하였다. 실험은 제안하는 시스템이 학생들이 향후 수강할 수 있는 과목을 모두 제공하는지 여부와 제공되는 과목에 대한 정보 및 학점 계산들이 정확한 지를 측정하였다. 실제 학생의 수강내역을 이용한 실험의 결과는 온톨로지 기반의 수강지도 시스템이 현 수강지도 시스템의 수동적 방법을 해결하고, 사람이 지도한 내용과 같은 내용을 도출하는 것을 확인함으로써 제안하는 시스템의 유효성을 보여준다.

• 한국대기환경학회지
• /
• 제2권2호
• /
• pp.1-8
• /
• 1986

To obtain the guidance of plants sensitivity or resistance to $SO_2$ gas, 16 species, 25 varieties of plants were exposed to 0, 0.2, 0.4, 0.7 and 1.5 ppm of $SO_2$ gas in controlled environmental chamber and the visible injury on the plants was observed. Plant sensitivity and/or resistance rankings at each guidance appeared different, based on first injured time, injury degree, and injury index. Only 10 varieties of plant are equal in the ranking at different base. It is concluded that recommended guidance for sensitivity and resistance of plants to $SO_2$ gas are the first injured time and the injury degree, respectively.

• Journal of the Korean Society for Industrial and Applied Mathematics
• /
• 제19권3호
• /
• pp.271-287
• /
• 2015

In this article, a more generalized form of the impact time and angle control guidance law is proposed based on the linear quadratic optimal control methodology. For the purpose on controlling an additional constraint such as the impact time, we introduce an additional state variable that is defined to be the jerk (acceleration rate). Additionally, in order to provide an additional degree of freedom in choosing the guidance gains, the performance index that minimizes the control energy weighted by an arbitrary order of time-to-go is considered in this work. First, the generalized form of the impact angle control guidance law with an additional term which is used for the impact time control is derived. And then, we also determine the additional term in order to achieve the desired impact time. Through numbers of numerical simulations, we investigate the superiority of the proposed guidance law compared to previous guidance laws. In addition, a salvo attack scenario with multiple missile systems is also demonstrated.

• International Journal of Aeronautical and Space Sciences
• /
• 제4권2호
• /
• pp.26-36
• /
• 2003

The objective of this study is to enhance neural-network guidance to consider the impact condition. The optimal impact condition in this study is defined as an head-on attack. Missile impact-angle error, which is a measure of the degree to which the missile is not steering for a head-on attack, can also have an influence on the final miss distance. Therefore midcourse guidance is used to navigate the missile, reducing the deviation angle from head on, given some constraints on the missile g performance. A coordinate transformation is introduced to simplify the three-dimensional guidance law and, consequently, to reduce training data. Computer simulation results show that the neural-network guidance law with the coordinate transformation reduces impact-angle errors effectively.

• International journal of advanced smart convergence
• /
• 제10권4호
• /
• pp.233-240
• /
• 2021

The purpose of this study was to provide a 360-degree video on intensive care unit admission guidance to family members admitted to the intensive care unit, and then to identify anxiety, safety perception, and satisfaction. This study was a single-group pre-post design, and the data collection period was from October 1, 2020 to August 30, 2021. The subjects of this study were 19 people who applied 360 degree hospitalization guide video. For data analysis, SPSS WIN 24.0 program was used, and real number, percentage, mean, standard deviation, minimum value, maximum value, and Wilcoxon signed rank test were used. The subjects' anxiety before intervention was an average score of 6.21±2.30 and the anxiety after intervention was an average score of 3.95±2.46, which was statistically significant (z=4.13, p<.001). The safety consciousness of the subjects before the intervention was an average of 4.08±0.39 and the safety consciousness after the intervention was an average of 4.54±0.48, which was statistically significant (z=5.00, p=.001). The highest level of satisfaction with the 360-degree hospitalization guidance image of the subjects was 4.58±0.51 and the lowest was 4.16±0.96. In this study, when 360-degree hospitalization guide video was applied, there was a difference in anxiety and safety perception, and satisfaction was high. Based on the research results, various programs for guardian education can be developed and utilized in the future.

• 한국초등수학교육학회지
• /
• 제16권2호
• /
• pp.227-252
• /
• 2012

본 논문은 그동안 별반 연구되지 않았던 측정 영역과 관련하여, 길이와 넓이를 대상으로 안내 정도와 측정의 주요 학습 요소를 분석 기준으로 하여 제7차와 현행 교육과정 자료를 비교분석하였다. 분석 결과 교과서와 익힘책에 제시된 안내 정도와 측정의 학습요소가 비슷한 점이 많았으나, 현행 교육과정 자료에서 안내형의 비율이 줄어들고 복합형과 개방형의 비율이 늘어난 점, 그리고 측정값 계산의 비율이 줄어들고 측정추론 양감 어림, 측정단위, 측정의 구성요소에 대한 비율이 늘어난 점이 차이점으로 드러났다. 이와 같은 연구결과를 토대로 본 논문은 측정 영역의 교과서 개정과 교과서 분석에 대한 시사점을 제시한다.

• International Journal of Aeronautical and Space Sciences
• /
• 제7권2호
• /
• pp.137-144
• /
• 2006

The objective of this paper is to present trajectory guidance and control system with a dynamic inversion for a small unmanned aerial vehicle (UAV). The UAV model is expressed by fixed-mass rigid-body six-degree-of-freedom equations of motion, which include the detailed aerodynamic coefficients, the engine model and the actuator models that have lags and limits. A trajectory is generated from the given waypoints using cubic spline functions of a flight distance. The commanded values of an angle of attack, a sideslip angle, a bank angle and a thrust, are calculated from guidance forces to trace the flight trajectory. To adapt various waypoint locations, a proportional navigation is combined with the guidance system. By the decision logic, appropriate guidance law is selected. The flight control system to achieve the commands is designed using a dynamic inversion approach. For a dynamic inversion controller we use the two-timescale assumption that separates the fast dynamics, involving the angular rates of the aircraft, from the slow dynamics, which include angle of attack, sideslip angle, and bank angle. Some numerical simulations are conducted to see the performance of the proposed guidance and control system.

• 한국항해항만학회지
• /
• 제41권5호
• /
• pp.277-286
• /
• 2017

IMO introduced e-Navigation concept to improve the efficiency of ship operation, port operation, and ship navigation technology. IMO proposed sixteen MSPs (Maritime Service Portfolio) applicable to the ships and onshore in case of e-Navigation implementation. In order to meet the demands of the international society, the system implementation work for the Korean e-Navigation has been specified. The Korean e-Navigation system has five service categories: the S2 service category, which is a ship anomaly monitoring service, is a service that classifies emergency levels according to the degree of abnormal condition when a ship has an abnormality in ship operation, and provides guidance for emergency situations. The navigation safety module is a sub-module of the S2 service that determines the emergency level in case of navigation equipment malfunctioning, engine or steering gear failure during navigation. It provides emergency response guidance based on emergency level to the abnormal ship. If an abnormal condition occurs during the ship operation, first, the ship shall determine the emergency level, according to the degree of abnormality of the ship. Second, an emergency response guidance is generated based on the determined emergency level, and the guidance is transmitted to the ship, which helps the navigators prevent accidents and not to spread. In this study, the operational concept for the implementation of the Korean e-Navigation system is designed and the concept is focused on the navigation safety module of S2 service.

• 한국전자통신학회논문지
• /
• 제10권11호
• /
• pp.1277-1284
• /
• 2015

본 논문에서는 태양전지를 태양과 항상 법선 방향이 되도록 하기 위해 수평방향으로 놓여진 태양전지판을 ${\pm}90^{\circ}$까지 대칭 회전 가능토록 하는 비선형형상의 가이드홈을 가진 단축 추적장치를 제안하고, 비선형형상에 대한 수식을 정립하고자 한다. 그 결과 가이드 홈의 비선형 형상을 확정할 수 있었고, 특히 회전 링크의 길이가 달라져도 회전링크의 길이를 반영하는 가이드 홈을 정확히 확정할 수 있다. 이를 통해 기존의 1축 추적장치에 비해 약 10%이상의 태양전지 효율향상이 가능하며, 또한 어떤 크기의 태양전지판에 대해서도 최적의 비선형 형상 가이드 홈을 갖는 가이드 부재를 제공할 수 있고 대량 생산도 가능하다.