• 한국항해항만학회지
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• 제39권3호
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• pp.149-156
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• 2015

Dynamic Positioning System(DPS)은 동력, DP control 장치, DP 컴퓨터, 위치참조시스템(PRS), 센서, thruster 시스템 및 DP 운용자(DPO) 7가지로 구성되어 있다. DP 선박은 이들 구성요소들에 문제가 발생하면 그 기능을 상실할 수 있는데 이러한 DP 선박의 위치손실사고(Loss of Position, LOP)는 선주가 자발적으로 매년 IMCA에 보고하고 있다. 본 연구에서는 2001~2010년까지 10년 동안 IMCA 보고된 DP 선박 관련사고 612건에 대한 분석을 바탕으로 DPS의 7가지 구성요소와 관련된 사고 원인을 파악하고 이들 중 높은 비율을 차지하는 요인의 정성적, 정량적 분석을 통한 DP 선박의 안전운항 방안을 모색하고자 한다. 10년 평균 가장 높은 비율을 차지한 DPS 사고원인 요소는 PRS였다. 이를 전문가들의 브레인스토밍을 통해 작성된 flowchart를 바탕으로 베이지안 네트워크 분석을 시행한 결과 PRS 각 요소별 조건부 확률을 확인할 수 있었다. DP 선박의 drive off를 발생시키는데 주요한 영향을 미치는 것은 DGPS, microwave radar 및 HPR 이었고 DGPS에 주요한 영향을 미치는 에러 요인은 signal blocked, electric components failure, relative mode error 및 signal weak or fail이라는 것도 확인할 수 있었다.

• 한국항해학회지
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• 제13권2호
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• pp.1-21
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• 1989

The computer can be used to display a continuously updated list or plot of vessel position. The computer that accept input data from a number of different navigation systems, e.g., Loran , Satnav, Radar, Decca, Compass, Sextant with electrical output etc., can compute the position of a vessel relative to prerecorded objects. The celestial navigation system requires the computer to do not much calculation. Calculation are for trigonometeric, linear systems, finding roots of nonlinear equation and least square estimation etc, . In order to computerize the celestrial navigation system, these calculations must be programmed. The purpose of this thesis is to study the formulation, the design and the test of calculations of the coordinates of celestial bodies, the altitude correction and the solution of the navigational triangle processes.

• Journal of Positioning, Navigation, and Timing
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• 제11권3호
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• pp.173-179
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• 2022

The satellite navigation deception technology disturbs the navigation solution of the receiver by generating a deceptive signal simulating the actual satellite for the satellite navigation receiver mounted on the unmanned aerial vehicle, which is the target of deception. A single spoofing technique that creates a single deceptive position and velocity can be divided into a synchronized spoofing signal that matches the code delay, Doppler frequency, and navigation message with the real satellite and an unsynchronized spoofing signal that does not match. In order to generate a signal synchronized with a satellite signal, a very sophisticated and high precision signal generation technology is required. In addition, the current position and speed of the UAV equipped with the receiver must be accurately detected in real time. Considering the detection accuracy of the current radar technology that detects small UAVs, it is difficult to detect UAVs with an accuracy of less than one chip. In this paper, we assume the asynchrony of a single spoofing signal and propose a region defense technique using multiple spoofing signals.

• 한국항행학회논문지
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• 제19권5호
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• pp.403-410
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• 2015

ADS-B는 레이더에 비하여 높은 정확도와 빠른 갱신 주기를 제공하여, 레이더를 대체하거나 보완할 수 있는 기술이다. 최근 증가하는 항공교통량과 이에 따른 정확한 감시의 요구에 의하여 ADS-B가 실제 항공기 운영에 적용되고 있다. 본 논문은 항공기가 운항 중 상시 송신하는 ADS-B 신호를 활용한 공한 인근 지역에서 정밀 감시가 가능한지 확인하기 위한 자료 수집과 일부 데이터에 대한 분석을 수행하였다. 이를 위하여 정밀계기 착륙 접근하는 항공기의 ADS-B 항적을 수집하고, 최종접근 구간에서 항적의 분포 특성에 관한 분석을 수행하였다. 분석결과 ADS-B 항적은 활주로 중심선 연장선에 대하여 평균 이격 거리 -0.04 m, 표준편차 6.71 m이고, 또한 비교적 정확한 감시정보의 제공이 가능함을 확인하였다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2008년 영문 학술대회
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• pp.330-339
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• 2008

Ground-based interceptors(GBI) comprise a major element of the strategic defense against hostile targets like Intercontinental Ballistic Missiles(ICBM) and reentry vehicles(RV) dispersed from them. An optimum design of the subsystems is required to increase the performance and reliability of these GBI. Propulsion subsystem design and optimization is the motivation for this effort. This paper describes an effort in which an entire GBI missile system, including a multi-stage solid rocket booster, is considered simultaneously in a Genetic Algorithm(GA) performance optimization process. Single goal, constrained optimization is performed. For specified payload and miss distance, time of flight, the most important component in the optimization process is the booster, for its takeoff weight, time of flight, or a combination of the two. The GBI is assumed to be a multistage missile that uses target location data provided by two ground based RF radar sensors and two low earth orbit(LEO) IR sensors. 3Dimensional model is developed for a multistage target with a boost phase acceleration profile that depends on total mass, propellant mass and the specific impulse in the gravity field. The monostatic radar cross section (RCS) data of a three stage ICBM is used. For preliminary design, GBI is assumed to have a fixed initial position from the target launch point and zero launch delay. GBI carries the Kill Vehicle(KV) to an optimal position in space to allow it to complete the intercept. The objective is to design and optimize the propulsion system for the GBI that will fulfill mission requirements and objectives. The KV weight and volume requirements are specified in the problem definition before the optimization is computed. We have considered only continuous design variables, while considering discrete variables as input. Though the number of stages should also be one of the design variables, however, in this paper it is fixed as three. The elite solution from GA is passed on to(Sequential Quadratic Programming) SQP as near optimal guess. The SQP then performs local convergence to identify the minimum mass of the GBI. The performance of the three staged GBI is validated using a ballistic missile intercept scenario modeled in Matlab/SIMULINK.

• International Journal of Control, Automation, and Systems
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• 제3권1호
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• pp.130-136
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• 2005

A new optical digitizing system for determining the position of a cursor in three dimensions(3D) and an experimental device for its measurement are presented. A semi-passive system using light intensity modulation, a technology that is well known in radar ranging, is employed in order to overcome precision limitations imposed by background light. This system consists of a charge-coupled device camera placed before a rotating mirror and a light-emitting diode whose intensity is modulated. Using a Fresnel pattern for light modulation, it is verified that a substantial improvement of the signal to noise ratio is realized for the background noise and that a resolution of less than a single pixel can be achieved. This opens the doorway to the realization of high precision 3D digitized measurement. We further propose that a 3D position measurement with a monocular optical system can be realized by a numerical experiment if a linear-period modulated waveform is adopted as the light-modulating one.

• 한국항행학회논문지
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• 제21권2호
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• pp.163-170
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• 2017

독립 협동형 감시시스템인 이차감시레이더(SSR)의 위치 정보의 해상도를 높이기 위해 다변측정감시시스템(MLAT)이 항공 감시시스템에 적용되고 있다. 다변측정감시시스템은 쌍곡선(hyperbola) 또는 쌍곡면(hyperboloid) 위치 측정법을 이용하는 시스템으로 4개 이상의 지상 수신기에서 TOA (time of arrival)값을 측정하고 이를 중앙처리장치에서 각 수신기 상호간의 수신시각차 (TDOA; time difference of arrival)를 이용하여 항공기의 위치를 계산한다. TDOA (time difference of arrival) 알고리즘을 이용하는 다변측정감시시스템의 위치 측정 해상도를 높이기 위해서는 먼저 항공기에 탑재된 트랜스폰더에서 송출된 신호가 수신기에 수신되는 시간인 TOA(time of arrival)를 정밀하게 측정하여야 한다. 본 논문에서는 다변측정감시시스템의 구성에 대해 간략히 설명하였으며 TOA를 측정하기 위한 방법 중 하나인 ATD (adaptive threshold detector)에 대하여 간략히 설명하였다. ATD는 동일 신호에 대한 수신기간 수신한 신호의 진폭 차에 의해 발생하는 펄스 위치 편차 문제를 해결하는 방식이다. 본 논문에서는 ATD의 종류 중 LAS (level adjuster System)과 CDS (constant-fraction discriminator system)에 대한 시뮬레이션 결과와 기본적인 임계값을 적용한 펄스 위치 계산 시뮬레이션 결과를 비교하여 ATD의 성능을 분석하였다.

• Journal of Positioning, Navigation, and Timing
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• 제6권4호
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• pp.159-166
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• 2017

The position of autonomous driving vehicle is basically acquired through the global positioning system (GPS). However, GPS signals cannot be received in tunnels. Due to this limitation, localization of autonomous driving vehicles can be made through sensors mounted on them. In particular, a 3D Light Detection and Ranging (LIDAR) system is used for longitudinal position error correction. Few feature points and structures that can be used for localization of vehicles are available in tunnels. Since lanes in the road are normally marked by solid line, it cannot be used to recognize a longitudinal position. In addition, only a small number of structures that are separated from the tunnel walls such as sign boards or jet fans are available. Thus, it is necessary to extract usable information from tunnels to recognize a longitudinal position. In this paper, fire hydrants and evacuation guide lights attached at both sides of tunnel walls were used to recognize a longitudinal position. These structures have highly distinctive reflectivity from the surrounding walls, which can be distinguished using LIDAR reflectivity data. Furthermore, reflectivity information of tunnel walls was fused with the road surface reflectivity map to generate a synthetic reflectivity map. When the synthetic reflectivity map was used, localization of vehicles was able through correlation matching with the local maps generated from the current LIDAR data. The experiments were conducted at an expressway including Maseong Tunnel (approximately 1.5 km long). The experiment results showed that the root mean square (RMS) position errors in lateral and longitudinal directions were 0.19 m and 0.35 m, respectively, exhibiting precise localization accuracy.

• 대한전자공학회논문지TC
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• 제45권11호
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• pp.61-68
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• 2008

본 논문은 차량용 UWB 레이더 시스템의 RF front-end 개발에 그 목적이 있다. UWB 시스템은 1ns 이하의 매우 좁은 펄스폭을 갖는 임펄스를 전송한다. 따라서 수 GHz에 이르는 매우 낮은 전력의 초광대역 특성을 갖게 되어 기존의 무선 통신 시스템과의 공존이 불가피하다. UWB의 장점은 높은 채널 용량과 데이터 전송률을 가지며, 다중 경로에 대한 세밀한 분해가 용이하여 위치 예측과 Rake 수신이 가능하다는 점이다. 또한 UWB는 저전력의 초광대역 특성을 나타내므로 낮은 간섭 특성을 가지며, 초단거리의 정밀함에 의해 위치 추적이 가능하며, 시스템 구현 비용을 절감할 수 있다. RF front-end 모듈은 DCR(Direct ConveRsion) 방식을 사용하여 설계하였으며, 저가의 차량용 RF단에 적합하게 구성을 하였다.

• 한국멀티미디어학회논문지
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• 제23권11호
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• pp.1372-1382
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• 2020

This paper proposes a core technology for a micro river monitoring terminal device suitable for flood monitoring in small rivers and valleys. Our proposed device is basically equipped with a 77GHz radar, gyro and accelerometer sensors. To measure the flow velocity and water level, we proposed a signal processing technique that extracts pure water energy components from the observed Doppler velocity and reflection intensity from the radar. And to determine the stability of the river structure equipped with our device, we constantly monitor the displacement of the measured values of the gyro and accelerometer sensors. Experimental result verified that our method detects pure water energy in various river environments and distinguishes between flow velocity and water level well. And we verified that vibration and position change of structures can be determined through a gyro sensor. In future research, we will work to build a secure digital twin river network by lowering the cost of supplying RF-WAV devices. Also we expect our device to contribute to securing a preventive golden time in rivers.