• The Journal of The Korea Institute of Intelligent Transport Systems
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• v.18 no.5
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• pp.142-155
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• 2019

This study was conducted with the aim of developing a system to collect taxi GPS probe information to prevent link defects and to improve the accuracy of the standard link-based travel speed by determining when to go into and come out the link. For this purpose, a framework and algorithm consisting of a five-step process for standard link-based map matching and individual vehicle travel speed are presented and used it to calculate the average travel speed of the service link. Two on-site surveys of Teheran and Hakdong-ro were conducted to verify the results by the methods proposed in this paper. On the basis of the overall time of the field survey, the deviation in the travel speed was 0.2 km/h and 0.6 km/h, the accuracy was 99% and 96%, and the MAPE(Mean Absolute Percentage Error) was 1% and 4% in Teheran and Hakdong-ro, respectively. These results were more accurate thand those obtained using conventional methodologies without standard links.

• Journal of the Korea Institute of Information and Communication Engineering
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• v.25 no.12
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• pp.1770-1776
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• 2021

For hand expression recognition, hand pose recognition based on the static shape of the hand and hand gesture recognition based on hand movement are used together. In this paper, we proposed a hand expression recognition method that recognizes symbols based on the trajectory of a hand movement on a virtual blackboard. In order to recognize a sign drawn by hand on a virtual blackboard, not only a method of recognizing a sign from a hand movement, but also hand pose recognition for finding the start and end of data input is also required. In this paper, MediaPipe was used to recognize hand pose, and LSTM(Long Short Term Memory), a type of recurrent neural network, was used to recognize hand gesture from time series data. To verify the effectiveness of the proposed method, it was applied to the recognition of numbers written on a virtual blackboard, and a recognition rate of about 94% was obtained.

• Journal of Advanced Navigation Technology
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• v.28 no.3
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• pp.278-287
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• 2024

In this paper, telemetry link budget model for small launch vehicle is proposed, and telemetry link budget simulator is implemented. The proposed link budget model consist of geometry model and propagation loss model. The geometry model is calculation of look angle between ground station and small launch vehicle. The propagation loss model consist of free space loss, polarization loss, and de-pointing loss which are appropriate to the small launch vehicle flight environment. The proposed propagation loss model can be calculate propagation loss without complex calculation of propagation environments. The link budget simulator is implemented in MATLAB. The simulator calculate look angle, free space loss, polarization loss parameter, de-pointing loss and received signal level in ground station by using position of ground station, routing of small launch vehicle, 3-D radiation patterns of antennas.

• Journal of the Korean Society of Surveying, Geodesy, Photogrammetry and Cartography
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• v.28 no.1
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• pp.73-82
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• 2010

TERCOM(TERrain COntour Matching), which is the one of the Terrain Referenced Navigation and used in the cruise missile navigation system, is still under development. In this study, the TERCOM based on area-based matching algorithm and extended Kalman filter is analysed through simulation. In area-based matching, the mean square difference (MSD) and cross-correlation matching algorithms are applied. The simulation supposes that the barometric altimeter, radar altimeter and SRTM DTM loaded on board. Also, it navigates along the square track for 545 seconds with the velocity of 1000km per hour. The MSD and cross-correlation matching algorithms show the standard deviation of position error of 99.6m and 34.3m, respectively. The correlation matching algorithm is appeared to be less sensitive than the MSD algorithm to the topographic undulation and the position accuracy of the both algorithms is extremely depends on the terrain. Therefore, it is necessary to develop an algorithm that is more sensitive to less terrain undulation for reliable terrain referenced navigation. Furthermore, studies on the determination of proper matching window size in long-term flight and the determination of the best terrain database resolution needed by the flight velocity and area should be conducted.

• Journal of the Korean Society of Surveying, Geodesy, Photogrammetry and Cartography
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• v.32 no.1
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• pp.63-73
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• 2014

Recently, researches on DBRN(DataBase Referenced Navigation) system are being carried out to replace GNSS(Global Navigation Satellite System), as weaknesses of GNSS were found that are caused by the intentional interference and the jamming of the satellite signal. This paper describes the gravity gradient modeling and the construction of EKF(Extended Kalman Filter) based GGRN(Gravity Gradient Referenced Navigation). To analyze the performance of GGRN, fourteen flight trajectories were made for simulations over whole South Korea. During the simulations, we considered the errors in both DB(DataBase) and sensor as well as the flight altitudes. Accurate performances were found, when errors in the DB and the sensor are small and they located at lower altitude. For comparative evaluation, the traditional TRN(Terrain Referenced Navigation) was also developed and performances were analyzed relative to those from the GGRN. In fact, most of GGRN performed better in low altitude, but both of precise gravity gradient DB and gradiometer were required to obtain similar level of precisions at the high altitude. In the future, additional tests and evaluations on the GGRN need to be performed to investigate on more factors such as DB resolution, flight speed, and the update rate.

• Proceedings of the Korean Society of Broadcast Engineers Conference
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• 2010.11a
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• pp.129-131
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• 2010

분산 비디오 부호화(distributed video coding)는 분산 소스 부호화의 대표적인 응용분야로서 부호화 복잡도가 부호화기에서 복호화기로 이동되어 저전력 부호화 환경에 매우 적합하다. 본 논문에서는 분산 비디오 부호화의 성능 향상에 있어 가장 중요한 보조 정보의 효과적인 생성 방법을 제안한다. 우선 보조 정보 생성을 위한 키 프레임들 간의 블록 움직임 추정에 있어 기존 방법들이 대체적으로 가정하고 있는 선형적인 움직임 이동에 따른 잘못된 예측을 해결하기 위해 두 장 이상의 키 프레임을 사용하여 블록 움직임을 추정한 후, 선형 회귀(linear regression)를 이용하여 보조 정보 상의 블록 움직임 궤적을 추정한다. 이때 움직임 추정을 위한 키 프레임 번호를 증가하며 선입선출(FIFO)형 버퍼에 저장 및 삭제하여 동일한 보조정보에 해당하는 여러 움직임 벡터 필드와, 기존의 선형적인 움직임이 가정된 움직임 벡터 필드를 동시에 생성한다. 다음으로 보간(interpolation)하려는 보조 정보 프레임 내의 임의의 블록에 가장 가깝게 통과하는 움직임 벡터 필드를 선택하여 해당하는 블록의 최종 움직임 벡터로 선택한다. 실험결과 제안하는 보조 정보 생성 방법은 기존의 방법과 비교했을 때 비대칭성 움직임 벡터 사용만으로 평균 PSNR이 0.216dB 만큼 증가하는 것을 확인할 수 있었다.

• The Transactions of The Korean Institute of Electrical Engineers
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• v.67 no.3
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• pp.427-432
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• 2018

This paper uses a recursive least squares method to estimate the projectile motion trajectory of an object in real time. The equations of motion of the object are obtained considering the air resistance which occurs in the actual experiment environment. Because these equations consider air resistance, parameter estimation of nonlinear terms is required. However, nonlinear recursive least squares estimation is not suitable for estimating trajectory of projectile in that it requires a lot of computation time. Therefore, parameter estimation for real-time trajectory prediction is performed by recursive least square estimation after using Taylor series expansion to approximate nonlinear terms to polynomials. The proposed method is verified through experiments by using VICON Bonita motion capture system which can get three dimensional coordinates of projectile. The results indicate that proposed method is more accurate than linear Kalman filter method based on the equations of motion of projectile that does not consider air resistance.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.39 no.1
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• pp.16-24
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• 2011

In this paper, we propose a new guidance law for target observability enhancement, which can control both terminal impact angle and acceleration. The proposed guidance law is simple form, combined conventional time-to-go polynomial guidance and a additional bias term which consists of relative position and proportional gain. The guidance law provides oscillatory flight trajectory and it maintains the conventional time-to-go polynomial guidance performance. To investigate the characteristics of the guidance law, we derive the closed-form solution, and various simulations are performed for proving the validity of the proposed guidance.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.36 no.5
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• pp.448-454
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• 2008

This paper deals with a behavior based decentralized control strategy for UAV swarming utilizing the artificial potential functions and the sliding mode control technique. Individual interactions for swarming behavior are modeled using the artificial potential functions. The motion of individual UAV is directed toward the negative gradient of the combined potential. For tracking the reference trajectory of UAV swarming, a swarming center is considered as the object of control. The sliding-mode control technique is adopted to make the proposed swarm control strategy robust with respect to the system uncertainties and the varying mission environment. Numerical simulation is performed to verify the performance of the proposed controller.

• Proceedings of the Technology Innovation Conference
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• 2009.02a
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• pp.391-412
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• 2009

국가의 신성장 동력을 찾고 국가 연구개발과제를 기획 평가하는 것은 국가 경쟁력에 직결되는 것이라 할 수 있으며, 이것은 해당 기술에 대한 철저한 분석을 토대로 정확한 기술궤적 (technology trajectory)을 도출할 수 있을 때 효과적으로 수행될 수 있다. 기존에는 이러한 과정이 직관에 의한 판단이나 경험에 의존하는 경향이 높았으나, 최근에는 기술이 보유하고 있는 지식과 정보에 대한 정량적인 수치화, 즉 계량화를 기반으로 분석하려는 시도가 미국, 일본 등 선진국을 중심으로 이뤄지고 있으며, 계량정보분석은 과학기술정책 수립에 주요 방법론으로 자리잡고 있다. 그러나 계량정보분석에 대한 기존 연구들은 방법론 적용 및 활용 프로세스 등과 관련된 한계를 가지고 있다. 따라서 본 연구는 이러한 한계를 극복하기 위하여 선진국의 계량정보분석방법론의 적용 사례를 바탕으로 방법론의 유형 및 활용영역을 분석함으로써 활용목적에 맞는 계량정보분석방법론 포트폴리오 구축하는 것을 목표로 한다. 이를 위해 과학기술정책 수립에 활용될 수 있는 계량정보분석방법론 적용 가이드라인을 제공하고 활용 목적에 맞는 적용 프로세스를 제시하였다. 본 연구의 결과는 유망 기술 영역과 핵심 기술을 탐색하고 모니터링하는 방향으로 계량정보분석방법론의 활용영역이 확장될 수 있는 토대가 되며, 기술 지능(technology intelligence)적인 정보를 창출하여 실질적인 업무 지원 역할을 할 수 있는 계기가 될 것이다.