Earticle

본 연구에서는 수도권을 중심으로 구축ㆍ운영 중에 있는 ITS 무선통신 인프라인 UTIS를 활용하여 긴급차량 우선신호제어 시스템을 개발하였다. 신호교차로에서 긴급차량의 연속주행과 일반차량의 제어지체를 최소화하는 긴급차량 우선신호제어 시스템 구현을 위해 긴급차량의 진행방향(직/좌)을 사전에 파악이 가능하도록 하였으며, 긴급차량 우선신호 제어 방식을 현시삽입과 현시조정 모드로 구분하여 개발하였다. 또한, 시스템에 대한 현장 적용 가능성을 평가하기 위해 CORSIM 모형의 RTE 기능 활용을 통해 HILS 기반의 평가 시스템을 구성하여 EVP 제어 효과에 대한 검증을 수행하였다. 본 연구를 통해 개발된 긴급차량 우선신호제어 시스템은 기 구축된 ITS 인프라를 활용한 것으로 현장 적용 시 경제적이고 효율적인 구축이 가능할 것으로 기대된다.

In this paper, we have developed the system of emergency vehicle preemption signal control based on UTIS(Urban Traffic Information System) which have been deployed and operated in the national capital area. It considered the turning direction(through or left turn) of emergency vehicle at the signalized intersection in order to provide the consecutive progression of emergency vehicle and minimize the control delay of passenger cars. we adopted several EVP control modes such as phase insertion and phase adjustment mode. Also, we evaluated the possibility of field implementation via simulation analysis using CORSIM RTE(Run Time Extension) based HILS(Hardware In the Loop Simulation). We expect that the result of this research contribute to providing the right-of-way to emergency vehicle in this country.

This paper presents a 5-bit digital step attenuator (DSA) using a commercial 0.18-${\mu}m$ silicon-on-insulator (SOI) process for the wideband phased array antenna. Both low insertion loss and low root mean square (RMS) phase error and amplitude error are achieved employing two attenuation topologies of the switched path attenuator and the switched T-type attenuator. The attenuation coverage of 31 dB with a least significant bit of 1 dB is achieved at DC to 20 GHz. The RMS phase error and amplitude error are less than $2.5^{\circ}$ and less than 0.5 dB, respectively. The measured insertion loss of the reference state is less than 5.5 dB at 10 GHz. The input return loss and output return loss are each less than 12 dB at DC to 20 GHz. The current consumption is nearly zero with a voltage supply of 1.8 V. The chip size is $0.93mm{\times}0.68mm$, including pads. To the best of the authors' knowledge, this is the first demonstration of a low phase error DC-to-20-GHz SOI DSA.

To ensure the successful launch of the Korea pathfinder lunar orbiter (KPLO) mission, the Korea Aerospace Research Institute (KARI) is now performing extensive trajectory design and analysis studies. From the trajectory design perspective, it is crucial to prepare contingency trajectory options for the failure of the first lunar brake or the failure of the first lunar orbit insertion (LOI) maneuver. As part of the early phase trajectory design and analysis activities, the required time of flight (TOF) and associated delta-V magnitudes for each recovery maneuver (RM) to recover the KPLO mission trajectory are analyzed. There are two typical trajectory recovery options, direct recovery and low energy recovery. The current work is focused on the direct recovery option. Results indicate that a quicker execution of the first RM after the failure of the first LOI plays a significant role in saving the magnitudes of the RMs. Under the conditions of the extremely tight delta-V budget that is currently allocated for the KPLO mission, it is found that the recovery of the KPLO without altering the originally planned mission orbit (a 100 km circular orbit) cannot be achieved via direct recovery options. However, feasible recovery options are suggested within the boundaries of the currently planned delta-V budget. By changing the shape and orientation of the recovered final mission orbit, it is expected that the KPLO mission may partially pursue its scientific mission after successful recovery, though it will be limited.

This paper describes the performance of a Ku-band 5-bit monolithic phase shifter with metal semiconductor field effect transistor (MESFET) switches and the implementation of a ceramic packaged phase shifter for phase array antennas. Using compensation resistors reduced the insertion loss variation of the phase shifter. Measurement of the 5-bit phase shifter with a monolithic microwave integrated circuit demonstrated a phase error of less than $7.5{\circ}$ root-mean-square (RMS) and an insertion loss variation of less than 0.9 dB RMS for 13 to 15 GHz. For all 32 states of the developed 5-bit phase shifter, the insertion losses were $8.2{\pm}1.4$dB, the input return losses were higher than 7.7 dB, and the output return losses were higher than 6.8 dB for 13 to 15 GHz. The chip size of the 5- bit monolithic phase shifter with a digital circuit for controlling all five bits was 2.35 mm ${\times}$1.65 mm. The packaged phase shifter demonstrated a phase error of less than $11.3{\circ}$ RMS, measured insertion losses of 12.2 ${\pm}$2.2 dB, and an insertion loss variation of 1.0 dB RMS for 13 to 15 GHz. For all 32 states, the input return losses were higher than 5.0 dB and the output return losses were higher than 6.2 dB for 13 to 15 GHz. The size of the packaged phase shifter was 7.20 mm${\times}$ 6.20 mm.

기반암의 상부 토양층에 협재하는 속도이상층이 레일리파 위상속도와 수직변위의 스펙트럼 진폭에 미치는 영향을 분석하기 위하여 Thomsen-Haskell 방법을 사용하였다. 기본모델은 횡파속도(${\nu}_s$) 300 m/s의 토양층이 9 m 두께로 ${\nu}_s$가 1000 m/s인 반무한 기반암 위에 쌓여 있다. 토양층 내에 두께 1, 2, 3 m, S파속도 150, 225, 375, 450 m/s인 삽입층은 지표부터 깊이 1 m 간격으로 놓여있다. 레일리파 위상속도($C_R$)는 4 ~ 30 Hz 주파수 구간에서 계산하였다. 삽입층 모델은 두께가 1 m일 때, 기본모델과 삽입모델의 위상속도 차이인 ${\Delta}C_R$에 민감하게 반응하는 주파수 대역은 8 ~ 20 Hz이며, 이 주파수 대역은 삽입층의 두께가 증가할수록 넓어진다. 1차 고차모드의 저주파 차단주파수 바로 위의 주파수 구간을 제외하면, 모든 모델에서 기본모드의 스펙트럼 진폭이 1차 고f차모드보다 크다.

The Thomsen-Haskell method was used to determine sensitivities of the Rayleigh-wave phase velocities and spectral amplitude of vertical ground motion to insertion of a single velocity-anomaly layer into overburden underlain by a basement. The reference model comprised a 9-m thick overburden with shear-wave velocity (${\nu}_s$ of 300 m/s above a half-space with ${\nu}_s$ = 1000 m/s. The inserted layer, with a velocity of 150, 225, 375, or 450 m/s and a thickness of 1, 2, or 3 m, was placed at depths increasing from the surface in increments of 1 m. Phase velocities were computed for frequencies of 4 to 30 Hz. For inserted layer models, we placed an anomalous layer with thickness of 1 ~ 3 m, shear-wave velocity of 150 ~ 450 m/s, and at depths of 0 ~ 8 m in the overburden. The frequency range of 8 ~ 20 Hz were the most sensitive to the difference of $C_R$ between the inserted and reference models (${\Delta}C_R$) for h = 1 m and the frequency range got wide as h increased. For all of the models, the spectral amplitudes of the fundamental mode exceeded those of the $1^{st}$-higher mode except at frequencies just above the low-frequency cutoff of the $1^{st}$-higher mode.