• 패션비즈니스
• /
• 제4권4호
• /
• pp.123-133
• /
• 2000

The purpose of this study was to examine the usage of internet advertisement, to define the convenient dimensions of information navigation medium, and to examine the difference of convenient information navigation among advertisement types and information design methods. Thirty-four subjects were selected for the survey study and descriptive anlysis, factor analysis and ANOVA were used for the data analysis. The results of this study were: 1. the most perceived channel about the web site information was the search engine, the most preferred type of information design was the mixed type with text and image, and the most preferred medium for fashion information is the magazine. 2. the convenient dimensions of information navigation medium were information understanding, design composition, easy navigation, timely navigation, and convenient navigation. 3. the information design method is the significant factor influencing on the convenient information navigation.

• Journal of Positioning, Navigation, and Timing
• /
• 제11권2호
• /
• pp.109-117
• /
• 2022

This paper proposes a method for detecting flight anomalies of drones through the difference between the command of flight controller (FC) and the navigation solution. If the drones make a flight normally, control errors generated by the difference between the desired control command of FC and the navigation solution should converge to zero. However, there is a risk of sudden change or divergence of control errors when the FC control feedback loop preset for the normal flight encounters interferences such as strong winds or navigation sensor abnormalities. In this paper, we propose the method with a deep neural network model that predicts the control error in the normal flight so that the abnormal flight state can be detected. The performance of proposed method was evaluated using the real-world flight data. The results showed that the method effectively detects anomalies in various situation.

• 대한원격탐사학회:학술대회논문집
• /
• 대한원격탐사학회 2004년도 Proceedings of ISRS 2004
• /
• pp.72-76
• /
• 2004

For successful route guidance, navigation systems should provide to users more realistic and actual information such as photographs than those in either 2-dimensional and 3-dimensional models. In this paper, we propose a method for servicing photographs for route guidance in navigation systems. The method includes how to acquire photographs with the most successful view for the guidance, how to construct link information among them and navigational map data, and how to provide the images to users efficiently.

• 한국항해항만학회지
• /
• 제48권1호
• /
• pp.1-6
• /
• 2024

항로표지는 해상교통안전에 중요한 시설이며 이를 위해 해양수산부에서는 관리운영 시스템을 개발, 운영 중이다. 현재 항로표지관리 시스템은 텍스트 기반으로 정보를 표출한다. 따라서, 항로표지에 장애나 사고시에 발생하는 경우의 영향을 판단하기가 어렵다. 항로표지의 배치 검증을 위해 항로표지 시뮬레이터를 활용할 수 있으나, 실시간 정보가 적용되지 않고 시뮬레이터의 유지보수에 많은 비용이 필요하다. 또한 항로표지 시뮬레이터는 항만 배후광으로 인한 영향을 시뮬레이션할 수 없다. 본 연구에서는 이러한 단점을 개선하기 위해, 디지털트윈 기술을 적용한 항로표지 관리운영 플랫폼의 개발을 제안한다. 시스템은 항로표지로부터 수집되는 실시간 센서 데이터를 분석하여 고장을 예측할 수 있다. 항로표지 배치를 시뮬레이션할 수 있는 기능을 개발할 예정이다. 디지털트윈 기술을 적용함으로써 항로표지를 효율적으로 관리할 수 있을 것으로 기대한다.

• 한국항공우주학회지
• /
• 제42권11호
• /
• pp.947-957
• /
• 2014

본 논문은 의사위성 항법시스템의 항법성능 분석기법을 제시하고, 실제 시험 데이터를 이용한 의사위성 항법시스템의 항법결과 성능분석을 통해 이를 검증하고자 하였다. 기존 GPS 및 Galileo 등의 위성항법 분야에서 적용되는 항법성능 분석방법들을 통해 오차 요소들을 식별하고, 표준화된 문서에서 정의한 UERE의 기준을 확인하고, 실험적으로 UERE를 계산하는 방안을 살펴보았다. 이를 기준으로 의사위성 항법시스템에서의 오차 요소를 식별하고, 가용한 UERE 관측 방법과 UERE 계산 방법 및 UERE와 위성 배치로부터의 항법해 성능 추정 방안을 제안하고 몇 가지 상황을 고려한 시뮬레이션을 수행하였으며, 최종적으로 비행시험을 통한 실제 데이터를 이용하여 이를 검증하였다.

• 대한인간공학회지
• /
• 제32권5호
• /
• pp.443-448
• /
• 2013

Objective: Purposes of this study are selecting main factors in evaluating the usability of mobile navigation and comprehending mutual importance among the factors. Background: Mobile navigation services have been more diffused than ever as the number of smartphone users sharply increased. However users are having trouble with the usage of mobile navigation services due to the lack of research in the area. Method: In order to attain results, general research on mobile navigation, 1st general survey, and 2nd comparative survey on navigation UI experts were performed. Empirical studies about the results were performed using AHP method. Results: As the result of AHP analysis, accuracy was drawn out to be the most important factor followed by accessibility and visibility. Regarding the characteristics of navigation system, the provision of accurate POI(Point of Interest) was considered to be the most important factor for the experts. And effectiveness was considered to be the most important, followed by satisfaction and efficiency. Conclusion: When evaluating the usability of mobile navigation, prior factors such as accuracy, visibility, and aesthetics should be considered in advance and general evaluation concentrated on effectiveness must be performed. Application: The results of this study are expected to be a fundamental data to mobile navigation design.

• Journal of Positioning, Navigation, and Timing
• /
• 제10권4호
• /
• pp.353-361
• /
• 2021

This paper presents the jamming effect on the L5 band of Global Navigation Satellite System (GNSS) by analyzing real data collected via measurement campaigns in Korea region. In fact, the L5 band is one of the dedicated bands for various satellite navigation systems such as Global Positioning System (GPS), Galileo, BeiDou (BDS), and Quasi Zenith Satellite System (QZSS). And this band is also allocated along with various systems used for aeronautical radio navigation systems (ARNS). Among ARNS, the Distance Measuring Equipment (DME) and the Tactical Air Navigation System (TACAN) are systems that transmit and receive strong power pulse signals, which may cause unintentional jamming in the reception of GNSS signals. In this paper, signals in the main lobe of GPS L5, Galileo E5a, BDS B2a, and QZSS L5 are collected in Korean region to confirm whether the jamming effect exists in the band. And then, the pulse blanking technique, which is a simple signal processing technique capable of responding to pulsed jamming, is applied to analyze the jamming effect of DME/TACAN on the L5 band.

• Journal of Positioning, Navigation, and Timing
• /
• 제12권4호
• /
• pp.335-342
• /
• 2023

Lunar Navigation Satellite System refers to a constellation of satellite providing PNT services on the moon. LNSS consists of main satellite and navigation satellites. Navigation satellites orbiting around the moon and a main satellite moves the area between the moon and the L2 point. The navigation satellite performs the same role as the Earth's GNSS satellite, and the main satellite communicates with the Earth for time synchronization. Due to the effect of the non-uniform shape of the moon, it is necessary to focus on the influence of the lunar gravitational field when designing the orbit simulation for navigation satellite. Since the main satellite is farther away from the moon than the navigation satellite, both the earth's gravity and the moon's gravity must be considered simultaneously when designing the orbit simulation for main satellite. Therefore, the main satellite orbit simulation must be designed through the three-body problem between the Earth, the moon, and the main satellite. In this paper, the orbit simulation tool for main satellite and navigation satellite required for LNSS was designed. The orbit simulation considers the environment characteristics of the moon. As a result of comparing long-term data (180 days) with the commercial program GMAT, it was confirmed that there was an error of about 1 m.

• 한국정보통신학회:학술대회논문집
• /
• 한국정보통신학회 2018년도 추계학술대회
• /
• pp.217-219
• /
• 2018

본 기법은 한화시스템에서 2016년부터 착수한 한국형 e-Navigation 사업 중 대용량 데이터 처리 플랫폼(Data Service Platform, 이하 DSP)의 현장 운용성을 증대시키기 위해 DSP의 서비스 큐로 유입되는 다양한 외부 요청을 최적으로 재구성하여 끊김없는(Seamless) 서비스를 제공하는 방법이다. 항해 중인 선박이 DSP에 요청하는 다양한 서비스에 즉시 응답하기 위해서는 DSP가 응답데이터를 구성하는데 소요되는 시간과 선박이 요구하는 서비스를 사전에 예측하는 행위가 필요하다. 따라서 단기간에 DSP로 유입되는 다수의 요청들을 병렬로 예측분석하고 응답 큐를 재구성하여 응답 시간을 단축하는 기법을 구현함으로써 데이터의 크기나 서비스 동시 요청 수에 관계없이 DSP가 끊김 없는 서비스를 제공할 수 있게 하였다.

• Journal of Positioning, Navigation, and Timing
• /
• 제2권1호
• /
• pp.49-57
• /
• 2013

When pseudolite navigation system is applied to wide area, the tropospheric delay is the main error factor. In this study, we experimentally compared and analyzed the performance of the conventional pseudolite tropospheric delay models. The integration method using radiosonde meteorological data was suggested to derive the reference value for the comparison and analysis. Flight tests were carried out to analyze the performance of the tropospheric delay models according to the elevation angle and distance conditions between the user receiver and the pseudolite. As the results of this study, we provided the basis for the choice of tropospheric delay model appropriate to the relative location characteristics of the pseudolite and the user.