• 광학세계
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• 통권171호
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• pp.23-24
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• 2017

• 철도저널
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• 제20권4호
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• pp.70-73
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• 2017

• 전자통신동향분석
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• 제36권4호
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• pp.23-33
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• 2021

Wireless communication for train control is an active research field. The World Railway Federation in Europe developed GSM-R, which integrates the GSM-based voice call standard and train control signals. To provide advanced railway services, the LTE-R wireless communication system was developed in Korea for passenger services and wireless image information required by the railroad industry. Recently, direct communication technology for autonomous train driving has been studied to decrease the driving interval, and research is being conducted on a hyperloop train control system that runs at a maximum speed of 1,220km/h in a subvacuum environment of 0.001 atmosphere. In this paper, we summarize the trends in wireless communication technologies used for GSM-R/LTE-R railway systems. For future wireless communication in railway systems, we discuss autonomous train driving and the hyperloop railway control system, define wireless communication technology, and discuss trends in domestic and foreign technologies.

• 한국정보전자통신기술학회논문지
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• 제13권5호
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• pp.443-451
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• 2020

하이퍼루프는 튜브 내를 부상한 상태로 초고속주행하는 미래형 이동 시스템으로 제안되었다. 하이퍼루프에서 달리는 포드 차량은 선형 동기모터 상에서 주행하기에 위치측정이 근본적 중요성을 가진다. 1000km/h 이상의 속도로 주행하는 포드 차량의 가속과 감속에 정밀한 위치측정이 요구되며 또한 차량간 거리 유지를 위한 속도 조절에도 요구된다. 본 논문은 laser surface velocimeter를 개량하여 새로운 범위조건의 위치측정을 시도한다. 높은 정밀도로 초고속 이동체의 위치를 측정해야 하기에 지나가는 타일의 레이저 반사율 차이 검출로 변위를 계산하는 상대위치 측정장치를 구현하여 성능시험으로 평가하였다. 500km/h 미만의 포드 속도에서 cm 단위의 정밀도로 정확한 위치 측정을 보였으며, 500km/h 이상의 포드 속도에서도 0.1% 미만의 매우 낮은 오차율로 위치측정 결과를 보여주었다. 향후 500km/h 이상에서의 오차율도 0에 수렴하도록 연구를 진행해야 한다.

• International Journal of Aeronautical and Space Sciences
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• 제18권4호
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• pp.614-622
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• 2017

The characteristics of aerodynamic drag for Transonic Vehicle in Evacuated Tube was investigated using computational fluid dynamics. At first, parametric study on the system was performed according to the Mach number of the vehicle's speed ($Mach_v$), evacuated pressure of the tube ($Pre_t$), and blockage ratio (BR) between the vehicle and tube via axisymmetric flow analysis; the $Mach_v$ ranged from 0.3 to 1.0. The $Pre_t$ was 100, 1,000 and 10,000 Pa and the BR was 0.1, 0.2, and 0.4. In the calculations, the aerodynamic drag of the vehicle was larger when the BR and the pressure became larger. Concerning the $Mach_v$, the drag coefficient ($C_d$) became the maximum when the $Mach_v$ was near the Kantrowitz limit and decreased, which showed the typical transonic flow pattern. Then, three dimensional flow analysis was performed by changing the $Mach_v$ from 0.3 to 1.0 and setting the BR and the $Pre_t$ as 0.34 and 100 Pa, respectively by referring the Hyperloop Alpha documentation. From the calculations, the $C_d$ from three dimensional flow simulations were somewhat larger than those of axisymmetric ones because of the eccentricity of the vehicle inside the tube. However, the pattern of $C_d$ according to the $Mach_v$ was compatible with that of axisymmetric ones.