• 전기전자학회논문지
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• 제20권1호
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• pp.1-8
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• 2016

In this paper, we propose an effective time-of-arrival (TOA)-based localization method with adaptive bias computation in indoor environments. The goal of the localization is to estimate an accurate target's location in wireless localization system. However, in indoor environments, non-line-of-sight (NLOS) errors block the signal propagation between target device and base station. The NLOS errors have significant effects on ranging between two devices for wireless localization. In TOA-based localization, finding the target's location inside the overlapped area in the TOA-circles is difficult. We present an effective localization method using compensated distance with adaptive bias computation. The proposed method is possible for the target's location to estimate an accurate location in the overlapped area using the measured distances with subtracted adaptive bias. Through localization experiments in indoor environments, estimation error is reduced comparing to the conventional localization methods.

• 천문학회보
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• 제43권2호
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• pp.43.2-43.2
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• 2018

The line-of-sight component in the relative motion of galaxy pairs sources the redshift space distortion (RSD) in galaxy surveys. By knowing the probability density function (PDF) of pair-wise motions and projecting it to the line-of-sight direction, one can compute the RSD effect precisely. I present the pair-velocity PDF of dark matter and galaxies in the Horizon-run 4 simulation. I also derive a model motivated by the perturbation theory which fits the results fairly well. I also discuss the application of the model in constraining the cosmology.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 1996년도 한국자동제어학술회의논문집(국내학술편); 포항공과대학교, 포항; 24-26 Oct. 1996
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• pp.245-248
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• 1996

This paper suggests a new concept for missile guidance control, called linearized common curvature guidance law that enhances the probability to kill a target. The proposed guidance system is composed of two switching modes; one for the midcourse guidance and the other for the terminal guidance, which is switched by a specified critical value (.epsilon.). And the system and the commands are formulated and its simulations are provided in comparison with the conventional commanded line of sight guidance algorithm. Miss distance and angle of attack are denoted as performance of parameters. This new concept, common curvature guidance algorithm, revises the navigation guidance and accompanies, various considerations.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 1989년도 한국자동제어학술회의논문집; Seoul, Korea; 27-28 Oct. 1989
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• pp.93-98
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• 1989

This paper describes the application of the recently developed feedback linearization technique to designing a new Command to Line-of-Sight (CLOS) guidance law. We show that the CLOS guidance problem can be formulated as a tracking problem. Then, using the feedback input-output linearization technique, we find a new 3dimensional CLOS guidance law that can assure zero miss distance for a randomly maneuvering target. It sheds light on the feedforward acceleration compensation terms used in the conventional CLOS guidance laws to improve the performance. To illustrate further the significance of our result, simulation results are given.

• 한국정보과학회:학술대회논문집
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• 한국정보과학회 2005년도 가을 학술발표논문집 Vol.32 No.2 (2)
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• pp.610-612
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• 2005

사용자의 환경정보(Context)는 기존 서비스나 정보 검색을 효과적으로 하기위해 이용되고 있다. 이러한 환경정보중의 사용자 위치정보는 많은 어플리케이션이나 연구에서 유용하게 사용되고 있다. 이미 많은 연구에서 사용자의 위치를 인식하기 위해서 다양한 기술을 이용한 방법을 제안했다. 하지만 기존 연구들은 특정 환경기반 시나리오를 기반으로 개발해서 다양한 위치정보를 필요로 하는 위치기반 서비스를 제공하기 어렵다는 단점이 있다. 본 논문에서는 이러한 문제를 해결하기 위해서 IrDA(Infrared Data Association)의 Line of Sight 통신 특성을 이용하는 방법을 제안한다. 또한 위치인식 시스템의 유효성을 보여주기 위한 방법으로 "박물정보 제공 서비스"를 프로토타입으로 구현하였다.

• 항공우주시스템공학회지
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• 제2권1호
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• pp.13-16
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• 2008

The line of sight(LOS) is affected by the vibration of spacecraft. It is necessary to predict the effect of disturbance on LOS stability. Reaction wheel assembly is anticipated to be the largest disturbance source on spacecraft. The disturbance which is occurred mainly due to the mass imbalance is analyzed with harmonic numbers. The accuracy and stability are verified by probability density function with dynamic equation of the satellite motion.

• 한국정보통신학회:학술대회논문집
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• 한국정보통신학회 2013년도 추계학술대회
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• pp.609-611
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• 2013

장애물이 거의 없는 대기 중이나 주로 고정된 장애물이 존재하는 지상과 달리 해수면에서는 파도에 의해 수시로 통신 장애가 발생 할 수 있다. 특히 파도의 영향을 크게 받고 안테나 고도가 낮은 소형 통신국에서는 무선 통신을 위한 안테나 가시선(Line Of Sight, LOS) 확보가 어렵다. 본 논문에서는 해수면에서 파고와 송 수신 안테나의 고도 변화에 따른 가시선(LOS)과 통신망 운용을 위한 최소 안테나 고도를 계산하였다.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 2001년도 ICCAS
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• pp.58-58
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• 2001

This paper shows a practical approach that is robust to the errors causing path-delay in mobile wireless location, and analyzes its performance by comparing with other methods. NLOS(non-line-of-sight) error and multipath are two big sources of positioning error in wireless location. Contrary to GPS(global positioning system), they result from the terrestrial propagation of a signal. Especially, since LOS(line-of-sight) path between a transceiver and a receiver is blocked by intermediate buildings and topography, NLOS causes a signal to be reflected and diffracted. This path-delay error is very localized, and so, it is not easy to be estimated and mitigated. To treat such localized error, therefore ...

• 대한전자공학회:학술대회논문집
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• 대한전자공학회 2003년도 하계종합학술대회 논문집 I
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• pp.298-301
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• 2003

본 논문에서는 2.4 [GHz] 대역에서 1(equation omitted)2 마이크로스트림 배열 안테나를 이용한 지하철 터널내의 전파특성을 고찰하였다. 445 [m]의 터널구간에서 협대역 측정결과 LOS (Line-of-Sight)구간에 비하여 NLOS(Non-Line-of-Sight)구간에서는 수신 전력 레벨이 급격히 감소 하였으며, 10단 길이의 PN Sequence를 이용한 광대역 채널 측정에서는 Fan Beam의 평균과도지연과 RMS 지연확산이 각각 3.5736 [ns]과 11.7327 [ns]로서 원편파와 지향성 빔에 비하여 우수함을 확인하였다. 또한 전체 측정구간에 대한 평균과도지연과 RMS 지연확산의 중간값과 표준편차를 구하였고 각각의 빔에 대하여 비교하였다.

• 한국전자파학회:학술대회논문집
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• 한국전자파학회 2002년도 종합학술발표회 논문집 Vol.12 No.1
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• pp.127-131
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• 2002

This paper presents the a measured path-loss characteristics in urban line-of-sight(LOS) and non line-of-sight(NLOS) environments for 3.4, 5.3, and 6.4 ㎓ band signals. A two-ray model is applied to analyse the path-loss characteristics in LOS areas. In LOS areas, an empirical break point, whose distance is shorter than a theorical break point, is founded. Further, a sudden power level drop occurs at a transition point from LOS region to NLOS area and different path-loss exponents are occured various cases. The power level drop due to comer loss and path-loss exponents both increase as the distance between the transmitter and the corner increases.