• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 2001년도 ICCAS
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• pp.170.4-170
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• 2001

Safety and confidence of the communications network is the main purpose for the unmanned control systems, in terms of appling a satellite communications network to the water treatment and supply plant communication system. Since the unmanned control systems were applied in the industrial site, the lack of confidence on the communications network has been presented continuously as a main problem for the unmanned and automation systems. Therefore, satellite communications network was presented as one of the methods to solve this problem, supporting the wire used telecommunication. In addition to the safety of a communications network, there is the retrenchment of expenditure. This dual communications network has ...

• International journal of advanced smart convergence
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• 제9권3호
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• pp.207-214
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• 2020

Currently, the operation of unmanned aerial vehicle (UAV) is regulated to be able to fly only within the visible range, but in recent years, the needs for operation in the invisible area, in the urban area and at night have increased. In order to operate UAVs in the invisible area, at night, and in the urban area, a flight path for UAVs must be prepared like those operated by manned aircraft, and for this, it is necessary to establish an unmanned aircraft system traffic management (UTM). In order to establish the UTM, information on the minimum separation distance to prevent collisions with UAVs and buildings is required, and accordingly, information on the navigation performance of UAVs is required. In order to analyze the navigation performance of an UAV, total system error (TSE), which is the difference between the planned flight path and the actual location of the UAV, is required. If the collected data are insufficient and classification according to integrity, independence, and direction is not performed, accurate navigation performance is not derived. In this paper, propose a navigation performance analysis method of UAV that is derived TSE using flight data and modeled with normal distribution, analyze performance.

• 한국군사과학기술학회지
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• 제24권1호
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• pp.61-69
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• 2021

Recently, autonomous navigation technology is actively being developed due to the increasing demand of an unmanned surface vehicle(USV). Local planning is essential for the USV to safely reach its destination along paths. the dynamic window approach(DWA) algorithm is a well-known navigation scheme as a local path planning. However, the existing DWA algorithm does not consider path line tracking, and the fixed weight coefficient of the evaluation function, which is a core part, cannot provide flexible path planning for all situations. Therefore, in this paper, we propose a new DWA algorithm that can follow path lines in all situations. Fixed weight coefficients were trained using reinforcement learning(RL) which has been actively studied recently. We implemented the simulation and compared the existing DWA algorithm with the DWA algorithm proposed in this paper. As a result, we confirmed the effectiveness of the proposed algorithm.

• 한국국방기술학회 논문지
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• 제5권2호
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• pp.17-22
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• 2023

4차 산업혁명 기반의 무인화 및 인공지능 기술의 발전 속에 대한민국 육군은 미래첨단과학기술이 집약된 지상전투체계 ARMY TIGER 4.0을 추진 중이다. 이 체계는 AI 기반 초연결 지상전투체계를 중심으로 발전해나가고 있으며, 기동화, 지능화, 네트워크화를 핵심개념으로 한다. 이중 드론봇 전투체계는 기존의 드론과 로봇의 합성어로 무인전투체계를 포괄적으로 지칭한다. 이러한 추세 속에, 미래 전장은 무인화 및 인공지능 기반의 무기체계 활용이 증대될 것으로 예상된다. 특히 무인화로 전환하는 과도기에는 개별 무인체계 혹은 유·무인체계간 연결성을 보장하는 것이 상당히 중요한 문제이다. 본 논문에서는 효과적인 지휘통제 및 통신을 위한 Multiplexer 할당문제(MAP)를 소개하고, 수학적 모형을 제시함과 동시에 즉응적으로 모형의 해를 도출해줄 수 있는 휴리스틱 알고리즘을 제안한다. 또한, 해당 MAP 모형의 최적해를 도출하여, 본 논문에서 제안한 휴리스틱 알고리즘의 해의 품질과 계산시간을 제시한다. 추가적으로, MAP에 대한 향후 연구방향에 대해서도 논의한다.

• 한국정보통신학회논문지
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• 제25권1호
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• pp.160-163
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• 2021

In this paper, we present a path search scheme for the safe movement of the swarm of unmanned systems in unknown dangerous areas. Some of the swarm searches for the primary and secondary paths before the majority of swarm move through dangerous areas. In terms of rapid movement from the dangerous area and preparation for an accident, the primary path is searched first in the destination's direction. The secondary path is searched by considering the distance between the paths to guarantee a safe distance. The computer simulations show that the proposed scheme is suitable for the swarm of unmanned systems.

• 제어로봇시스템학회논문지
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• 제10권2호
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• pp.139-144
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• 2004

The flight control system designed for an unmanned airship, which is under development by KARI, is in reduced. First, the dynamic characteristics of the airship are addressed, which are fairly different from those of the nominal aircraft. In order to implement autonomous flight for the unmanned airship, flight control logic is designed including autopilot and guidance law. The autopilot is designed under consideration of the velocity region of the unmanned airship. The guidance laws are implemented in main operational modes such as point navigation, station keeping and spiral up/down for emergency return. Their simulation results are also presented in order to validate performances of the flight control system.

• 한국해양공학회지
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• 제33권6호
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• pp.510-517
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• 2019

Efficient path planning is essential for unmanned surface vehicle (USV) navigation. The A^* algorithm is an effective algorithm for identifying a safe path with optimal distance cost. In this study, a modified version of the A^* algorithm is applied for planning the path of a USV in a static and dynamic obstacle environment. The current study adopts the A^* approach while maintaining a safe distance between the USV and obstacles. Two important parameters-path length and computational time-are considered at various start times. The results demonstrate that the modified approach is effective for obstacle avoidance by a USV that is compliant with the International Regulations for Preventing Collision at Sea (COLREGs).

• 제어로봇시스템학회논문지
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• 제13권2호
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• pp.133-139
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• 2007

An unmanned ground vehicle can perform its mission automatically without human control in unknown environment. To move up to a destination in various surrounding situation, navigational information is indispensible. In order to be adopted for an unmanned vehicle, the navigation box is small, light weight and low power consumption. This paper suggests navigation system using a low grade MEMS IMU for supplying position, velocity, and attitude of an unmanned ground vehicle. This system consists of low cost and light weight MEMS sensors and a GPS receiver to meet unmanned vehicle requirements. The sensors are basically integrated by loosely coupled method using Kalman filter and internal algorithms are divided into initial alignment, sensor error compensation, and complex navigation algorithm. The performance of the designed navigation system has been analyzed by real time field test and compared to commercial tactical grade GPS/INS system.

• 제어로봇시스템학회논문지
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• 제14권12호
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• pp.1253-1259
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• 2008

This paper presents a landing controller and guidance law for net-recovery of fixed-wing unmanned aerial vehicles. A linear quadratic controller was designed using the system identification result of the unmanned aerial vehicle. A pursuit guidance law is applied to guide the vehicle to a recovery net with imaginary landing points on the desired approach path. The landing performance of a pure pursuit guidance, a constant pseudo pursuit guidance, and a variable pseudo pursuit guidance is compared. Numerical simulation using an unmanned aerial vehicle model was performed to verify the performance of the proposed landing guidance law.

• 한국지능시스템학회논문지
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• 제19권3호
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• pp.375-380
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• 2009

본 논문에서는 자계기반 무인주행 차량을 위한 조향장치를 설계하고 개발하였다. 자계기반 무인주행 시스템에서 가장 중요한 것은 자계도로를 따라 주행할 때 차량의 방향을 제어하는 조향장치이다. 본 논문에서는 조향각 제어를 위해 조향제어장치의 메커니즘을 설계하고 스텝모터의 속도 제어를 위해 새로운 속도 추종 주파수 제어 방법을 적용하였다. 개발된 조향장치의 실용성을 입증하기 위하여 개발된 시스템을 자계기반 무인주행 차량에 적용하고 주행실험을 수행하고 분석하였다.