• 한국항해항만학회지
• /
• 제35권8호
• /
• pp.657-665
• /
• 2011

본 연구는 수직 배치형 컨테이너 터미널에서 반입되는 수출 컨테이너의 작업순서와 장치위치를 결정하는 통합 문제를 다루었다. 수출 컨테이너에 대한 선호 장치위치는 대응하는 본선작업의 우선순위와 밀접하고 외부 트럭들의 대기시간은 장치 소요시간에 좌우된다. 본 연구는 외부 트럭들의 예정도착시간과 예정완료시간 그리고 적하작업의 선호 장치위치를 고려한 혼합정수모형을 제시하였다. 그리고 현장 적용을 위해 시뮬레이티드 어닐링에 기반한 휴리스틱 알고리즘을 개발하였다. 목적 함수값과 계산시간의 관점에서 최적 모형과 휴리스틱 알고리즘을 비교하였고 수치실행을 통해 휴리스틱 알고리즘의 수행도를 분석하였다.

• 대한조선학회논문집
• /
• 제58권2호
• /
• pp.121-128
• /
• 2021

According to the increasing interest and demand for the Autonomous Surface Vessels (ASV), the autonomous navigation system is being developed such as obstacle detection, avoidance, and path planning. In general, autonomous navigation algorithm controls the ship by detecting the obstacles with various sensors and planning path for collision avoidance. This study aims to construct and prove autonomous algorithm with integrated various sensor using the Robot Operating System (ROS). In this study, the safety zone technique was used to avoid obstacles. The safety zone was selected by an algorithm to determine an obstacle-free area using 2D LiDAR. Then, drift angle of the ship was controlled by the propulsion difference of the port and starboard side that based on PID control. The algorithm performance was verified by participating in the 2020 Korea Autonomous BOAT (KABOAT).

• 한국항행학회논문지
• /
• 제24권1호
• /
• pp.16-27
• /
• 2020

본 논문에서는 위성항법 불용 환경에서의 무인비행체 항법을 위한 광류 정보 활용에 관한 연구 내용을 기술한다. 광류 정보는 위성항법 불용 환경에서 수평 위치 및 속도 추정을 위해 중요한 측정값이므로 정확한 광류 정보의 획득은 필수적이다. 이에 광류 정보에 포함될 수 있는 바이어스를 추정하여 상쇄함으로써 추정 성능을 향상시킬 수 있는 항법 알고리즘을 제안한다. 제안된 알고리즘을 적용하여 검증하기 위해 유도, 항법, 제어 시스템을 설계하여 통합 시뮬레이션 환경을 구축한다. 이를 기반으로 수치 시뮬레이션을 수행하여 제안된 알고리즘을 분석한다.

• 제어로봇시스템학회논문지
• /
• 제7권5호
• /
• pp.454-464
• /
• 2001

In this paper, a personal navigation system is developed using GPS and dead reckoning sensors. This personal navigation system can be used to track a person inside a building, on an urban street, and in the mountain area. GPS can provide accurate absolute position information, but it cant be used without receiving enough satellite signals. Although the inertial sensors such as gyro an accelerometer and be used without this diggiculty, the inertial sensors severely suffer from their drift errors and the magne-tometer can be easily distorted by surrounding electromagnetic field. GPS and DR sensors can be inte-grated together to overcome these problems. A new personal navigation system that can be carried wit person is developed. A pedometer. actually vertically mounted accelerometer, detects ones footstep and gyro detects heading angle. These DR sensors are integrated with GPS and the humans walking pattern provides additional navigation information for compensating the DR sensors. The field testes are performed to evaluated the proposed navigation algorithm.

• 한국시뮬레이션학회논문지
• /
• 제14권2호
• /
• pp.93-103
• /
• 2005

This paper presents characteristics of a virtual human's navigation using a limited perception-based mapping. Previous approaches to virtual human navigation have used an omniscient perception requiring full layout of a virtual environment in advance. However, these approaches have a limitation on being a fundamental solution for a human-likeness of a virtual human, because behaviors of humans are basically based on their limited perception instead of omniscient perception. In this paper, we integrated Hill's mapping algorithm with a virtual human to experiment virtual human's navigation with the limited perception. This approach does not require full layout of the virtual environment, 360-degree's field of view, and vision through walls. In addition to static objects such as buildings, we consider enemy emergence that can affect an virtual human's navigation. The enemy emergence is used as the variable on the experiment of this present research. As the number of enemies varies, the changes in arrival rate and time taken to reach the goal position were observed. The virtual human navigates by two conditions. One is to take the shortest path to the goal position, and the other is to avoid enemies when the virtual human encounters them. The acquired result indicates that the virtual human's navigation corresponds to a human cognitive process, and thus this research can be a framework for human-likeness of virtual humans.

• 한국항해항만학회지
• /
• 제48권2호
• /
• pp.125-136
• /
• 2024

This research presents an innovative integrated ethanol solid oxide fuel cell (SOFC) system designed for applications in marine vessels. The system incorporates an exhaust gas heat recovery mechanism. The high-temperature exhaust gas produced by the SOFC is efficiently recovered through a sequential process involving a gas turbine (GT), a regenerative system, steam Rankine cycles, and a waste heat boiler (WHB). A comprehensive thermodynamic analysis of this integrated SOFC-GT-SRC-WHB system was performed. A simulation of this proposed system was conducted using Aspen Hysys V12.1, and a genetic algorithm was employed to optimize the system parameters. Thermodynamic equations based on the first and second laws of thermodynamics were utilized to assess the system's performance. Additionally, the exergy destruction within the crucial system components was examined. The system is projected to achieve an energy efficiency of 58.44% and an exergy efficiency of 29.43%. Notably, the integrated high-temperature exhaust gas recovery systems contribute significantly, generating 1129.1 kW, which accounts for 22.9% of the total power generated. Furthermore, the waste heat boiler was designed to produce 900.8 kg/h of superheated vapor at 170 ℃ and 405 kP a, serving various onboard ship purposes, such as heating fuel oil and accommodations for seafarers and equipment.

• 한국항행학회논문지
• /
• 제25권4호
• /
• pp.293-298
• /
• 2021

일반적으로 유도무기의 탐색기와 유도조종장치는 유도탄의 상태를 나타내기 위해 표적, 탐색, 인지, 포착정보를 처리하여 유도무기의 운용 및 제어를 담당하는 역할을 한다. 유도에 필요한 신호는 시선 변화율 신호, 시각 신호, 종말 단계 동체 지향 신호이며, 발사 통제에 필요한 신호는 표적, 감지 신호가 필요하다. 최근 유도탄의 복잡하고 처리하기 어려운 유도탄 신호를 실시간으로 처리하기 위해 유도탄의 데이터 처리 속도를 높여야 한다. 본 연구는 PLINQ(Parallel Language-Integrated Query)의 병렬 알고리즘 방법 중 스톱앤고와 역 열거형 알고리즘을 적용한 후 유도탄 점검 프로그램을 이용하여 실시간으로 유도탄 필요 신호 데이터 처리속도를 비교 후 처리결과를 나타내었다. 도출된 데이터 처리결과 기준으로 다중코어 처리방식과 단독코어 처리방식 CPU(Central Processing Unit) 처리속도 비교, CPU 코어 이용률을 비교하고 병렬처리 알고리즘 적용 시 유도탄 데이터 처리에 효과적 방법을 제안한다.

• 제어로봇시스템학회논문지
• /
• 제9권9호
• /
• pp.736-744
• /
• 2003

The GPS attitude output or carrier phase observables can be effectively utilized to compensate the attitude error of the strapdown inertial navigation system. However, when the integer ambiguity is not correctly resolved and/or a cycle slip occurs, an erroneous GPS output can be obtained. If the erroneous GPS information is directly applied to the AGPS/INS integration system, the performance of the system can be rapidly degraded. This paper proposes an AGPS/INS integration system using the triple difference carrier phase observables. The proposed integration system contains a cycle slip detection algorithm, in which inertial information is combined. Computer simulations and van test were performed to verify the proposed integration system. The results show that the proposed system gives an accurate and reliable navigation solution even when the integer ambiguity is not correct and the cycle slip occurs.

• 한국우주과학회:학술대회논문집(한국우주과학회보)
• /
• 한국우주과학회 2008년도 한국우주과학회보 제17권2호
• /
• pp.26.3-26.3
• /
• 2008

This research develops a GPS-based formation-flying testbed (FFTB) for formation navigation and control. The FFTB is a simulator in which spacecraft simulation and modeling software and loop test capabilities are integrated for test and evaluation of spacecraft navigation and formation control technologies. The FFTB is composed of a GPS measurement simulation computer, flight computer, environmental computer for providing true environment data and 3D visualization computer. The testbed can be simulated with one to two spacecraft, thus enabling a variety of navigation and control algorithms to be evaluated. In a formation flying simulation, GPS measurement are generated by a GPS measurement simulator to produce pseudorange, carrier phase measurements, which are collected and exchanged by the flight processors and subsequently processed in a navigation filter to generate relative and/or absolute state estimates. These state estimates are the fed into control algorithm, which are used to generate maneuvers required to maintain the formation. In this manner, the flight processor also serves as a test platform for candidate formation control algorithm. Such maneuvers are fed back through the controller and applied to the modeled truth trajectories to close simulation loop. Currently, The FFTB has a closed-loop capability of simulating a satellite navigation solution using software based GPS measurement, we move forward to improve using SPIRENT GPS RF signal simulator and space-based GPS receiver

• 대한전기학회:학술대회논문집
• /
• 대한전기학회 2008년도 심포지엄 논문집 정보 및 제어부문
• /
• pp.197-198
• /
• 2008

A software platform which is able to evaluate the performances of a GPS/INS integrated system has been developed in this paper. And it consists of four parts including GUI(Graphic User Interface) part, GPS part, INS part and integrated filter part. It basically offers the loosely, tightly and deeply coupled GPS/INS algorithms, and many design parameters can be changed by users via GUI. Each functions of the platform has been confirmed with GPS signals and IMU data from commercial simulators.