• Proceedings of the Korean Information Science Society Conference
• /
• 2001.10c
• /
• pp.238-240
• /
• 2001

문선 네트워크 분야에서 기존의 Mobile IP 외에 별도의 기반 시선 없이 각 노드만으로 네트워크를 구성하여 통신하는 Mobile Ad hoc Network (MANET)에 관한 연구가 활발히 진행되고 있다. 본 논문에서는 MANET에서의 노드 에너지 소비량을 공정하게 조절하는 라우팅 알고리즘을 제안한다. 기존에 제시된 라우팅 알고리즘들은 데이터 경로 결정의 요소로 각 노드의 에너지 정보를 사용하고 있다. 이에 반해 본 논문에서 제시하는 알고리즘은 각 노드의 에너지 뿐만 아니라, 네트워치 통신에 대한 기여도를 사용한다. MANET에서 노드는 일반 호스트이면서 동시에 다른 노드의 데이터에 대한 라우터의 역할도 수행한다. 노드가 호스트가 아닌 라우터로써 많은 에너지를 소비하게 되면, 이 노드는 네트워크 통신에 대한 기여도가 높다고 한 수 있다. 시뮬레이션을 통한 견과는 우리가 제시하는 라우팅 알고리즘이 네트커핀 전반에 걸쳐 에너지를 공정하고 균등하게 분포 시킬 수 있다는 것을 보여준다.

• Science of Emotion and Sensibility
• /
• v.13 no.1
• /
• pp.111-120
• /
• 2010

Initial stage of emotion has a great influence on building up product image and impression. Because of its influencing effects, measuring initial stage of emotion has potential to be a key factor for designers and marketers to achieve a distinct product concept. While many researchers have studied this topic with the emotion measurement method in product use stage, there are very few cases specialized in the initial stage of emotion. Even though present emotion measurement methods have difficulties to derive accurate user's initial stage of emotion, most case of initial emotion study applies these defective methods. The purpose of this study is to develop initial stage of emotion measurement method and apply this method to real product context. In the design of the initial stage of emotion measurement method, noticeable characteristics of initial stage of emotion were explored and initial emotion measurement framework was presented. Based on this framework, Initial Emotion Measurement System(IEMS) was suggested. This method collects user's eye movement, behavior and verbal data accurately and objectively.

• Education of Primary School Mathematics
• /
• v.20 no.4
• /
• pp.305-319
• /
• 2017

In the process of finding the triangle height, 26 students in the 6th grade were surveyed to understand the students' triangle height through the eye movement data and to investigate the cognitive load of the students. As a result, the correctness rate of the pre-test was significantly increased in the post-test, and the frequency and retention of gaze data were smaller in the post-test than in the AOI of each question. The Participants's subjective cognitive load indicated that it was more difficult to understand the concept of rotated triangles compared with upright triangles that were parallel to the ground. More frequent and more retentions in the eye-tracking data were detected in the right triangles and acute triangles by rotating configuration. Eye movement data show that eye tracking technology can provide an objective measure of students' cognitive load for feedback on instructional design.

• The Journal of the Convergence on Culture Technology
• /
• v.9 no.1
• /
• pp.135-140
• /
• 2023

VR animation allows you to see 360-degree screen production that cannot be seen in existing animation production while being located in the space within the animation. <Goodbye Mr Octopus>, a VR animation produced in 2020, was selected at the 77th Venice Film Festival as an immersive short film. This is the story of an adolescent girl, Stella, who is celebrating her 16th birthday, and her conflict with her strict father is resolved through a letter from her mother. It is a narrative composed of a total of 11 scenes, and in each scene, new directing elements of VR video grammar, such as gaze induction, time flow, and space conversion directing, were analyzed. Gaze-inducing directing minimized the inconvenience of 360-degree gaze, and time and space conversion directing was analyzed as an effect of increasing the audience's immersion according to narrative events.

• The Journal of the Korea institute of electronic communication sciences
• /
• v.18 no.5
• /
• pp.965-970
• /
• 2023

Wind profiler and wind lidar produce a vertical profile of winds in high spatiotemporal resolution in the atmospheric boundary layer. The wind lidar makes the wind vector using DBS (Doppler Beam Swinging) and VAD (Velocity Azimuth Display) methods. The DBS method has the advantage of obtaining a wind profile with a fast scan time. On the other hand, there is a restriction that requires at least two beams including vertical beam, which causes a decrease in the data acquisition rate. The VAD method was improved to produce more wind vector of the wind profiler as well as the wind lidar, which generally uses 5 beams. Fourier series was estimated with the radial velocity by the DBS method and wind vector was determined by setting the azimuth interval and applying the radial velocity by the Fourier series to the VAD method. The wind vectors were retrieved at the altitude where the wind was not calculated by the DBS method, and the results of the two methods were consistent.

• Proceedings of the ESK Conference
• /
• 1995.04a
• /
• pp.199-208
• /
• 1995

본 연구에서는 사람이 한글을 읽는 동안에 문자인식에 영향을 미치는 문장구조의 여러 요소 중 글자크기와 줄간간격에 대한 주시시간과 오독률을 분석함으로써 한글 인식에 있어서 사람에게 적합한 문장구조를 제시하는 데 그 목적이 있다고 할 수 있다. 실험에서는 남녀 각 5명씩의 피실험자에게 아이카메라를 착용시킨 후, 40cm 거리에서 문장중심과 피실험자의 시선이 일치되게 하여, 각기 다른 문장구조를 가 지는 9개의 실험예문(B5용지)을 소리내어 읽게 하였다. 실험결과로 부터 글자크기 와 줄간간격은 읽기수행도(reading performance)에 영향을 미치는 것으로 나타났다. 이를 이용하여 인쇄물의 제작시에 적용시켜 읽기수행도를 제고시킬 수 있다.

• 한국HCI학회:학술대회논문집
• /
• 2007.02b
• /
• pp.15-20
• /
• 2007

본 연구는 시선 추적 방법(Eye-Tracking Method)을 이용한 디지털 컨버전스 제품의 정보 설계 및 평가에 관한 방법론을 제시하였다. Eye-tracking 데이터는 visual search의 효율성 뿐 아니라 타겟의 유의미성이나 가시성등을 측정하는데 유익하다. 응시 횟수와 응시 시간을 통하여 사용자의 심성 모형에 따른 시선 행위와 제품 메뉴 구조간의 전체적인 일치도를 정량적으로 분석하였고, 각 메뉴 item의 세부적인 인지 반응 정도를 평가하였다. 컨버전스 제품의 한 예로 휴대폰을 선정하여 실험을 실시하였으며, 활성화 확산 실험(SAT)을 수행하여 메뉴 항목 상호간의 인지반응 정도를 통한 문제점을 도출한 후 사용자 시나리오를 작성하였다. 1차 테스트를 통하여 피실험자의 시나리오 수행 시 어려움을 알 수 있었으며, 1차 테스트의 결과와 인터뷰 결과를 바탕으로 프로토타입의 메뉴명을 개선하여 2차 테스트를 실시하였다. 실험 결과 개선 전보다 후의 응시 횟수, 응시 시간 또한 감소하여 수행도가 향상됨으로 메뉴 구조의 개선된 결과를 가져왔다. 본 연구는 인간의 눈 움직임 측정치 결과를 토대로 사용자 심성 모형에 부합하여 누구나 접근이 쉬운 정보 구조를 설계할 수 있었다. 그러므로 본 연구에서 제시하는 Eye-tracking Method는 디지털 컨버전스로 인한 복잡한 정보 구조의 설계와 평가에 기여할 것으로 보인다.

• Journal of the Korean Society for Aeronautical & Space Sciences
• /
• v.39 no.11
• /
• pp.1013-1020
• /
• 2011

This paper deals with the tracking problem of a moving target using multiple unmanned aerial vehicles. A decentralized extended information filter is designed to cooperatively estimate the position and the velocity of the moving target. The extended information filter is adopted to consider the range and the line-of-sight angle as measurement data. The decentralized scheme is applied to enhance the estimation performance using the information provided by other vehicles. Numerical simulation is performed to verify the tracking performance of the proposed decentralized filters.

• Journal of the Korean Society for Aeronautical & Space Sciences
• /
• v.32 no.7
• /
• pp.69-75
• /
• 2004

An avoidance/guidance problem of an aircraft against moving obstacle is considered in two dimensional space. The aircraft is modelled as a point mass flying with constant speed. The lateral acceleration is assumed the control input. Artificial potential functions are applied to the terminal point and moving obstacles in order that repulsive forces and an attractive force are produced by the obstacles and the terminal point respectively. A real time guidance/avoidance law is proposed by using the potential forces and relative velocity. The guidance law for a logarithm potential function results the well-known proportional navigation law. The avoidance control command is inverse proportional to the time-to-go to the obstacle and turns the aircraft toward the negative direction of the line-of-sight change. The performance of the proposed guidance/avoidance law is verified with simulations.

• Journal of the Korea Academia-Industrial cooperation Society
• /
• v.9 no.6
• /
• pp.1585-1591
• /
• 2008

Recently it is tried to use load control for maneuver moving object. MIN design method proposed to solve control problem of nonlinear system using load concept. Min design method shows direct method for finding control value on the load control model. In this paper, is shown load control value for problem of line of sight on missile guidance. The load control value keep given velocity of missile and angle of attack for tracking target.