• 제어로봇시스템학회논문지
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• 제14권9호
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• pp.873-880
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• 2008

This paper deals with the peer-to-peer data communication to connect each distributed levels of developed unmanned system according to the JAUS. The JAUS is to support the acquisition of unmanned system by providing a mechanism for reducing system life-cycle costs. Each of distributed levels of the JAUS protocol divides into a system, some of subsystems, nodes and components/instances, each of which may be independent or interdependence. We have to distribute each of the levels because high performance is supported in order to create several sub-processor computing data in one processor with high CPU speed performance. To complement such disadvantage, we must think the concept that a distributed processing agrees with separating each of levels from the JAUS protocol. Therefore, each of distributed independent levels send data to another level and then it has to be able to process the received data in other levels. So, peer-to-peer communication has to control a data flow of distributed levels. In this research, we explain each of levels of the JAUS and peer-to-peer communication structure among the levels using our developed unmanned ground vehicle.

• 한국항행학회논문지
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• 제19권1호
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• pp.41-47
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• 2015

최근 국내에서 A-SMGCS (advance surface movement ground control systems) 레벨 IV단계를 구현하기 위한 연구가 활발히 진행 중에 있다. 전체 A-SMGCS 시스템의 안전을 확보하기 위하여 안전성 평가가 필요하며, 유로컨트롤에서는 A-SMGCS의 안전성 평가를 위하여 기능별 위험요소 평가, 예비시스템 안전성 평가, 그리고 시스템 안전성 평가를 수행하도록 권고하고 있다. 본 논문에서는 기능별 위험요소 평가 방법을 통하여 전체 A-SGMCS의 위험요소를 식별한다. 따라서 A-SMGCS레벨 IV시스템에 대하여 29가지 위험 요소를 식별하고 각 위험요소의 심각도를 평가하는 자료로 활용할 것이다.

• 대한전기학회:학술대회논문집
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• 대한전기학회 2003년도 추계학술대회 논문집 전기기기 및 에너지변환시스템부문
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• pp.206-208
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• 2003

PWM AC/DC 컨버터에서 입력 전원측에서 제어보드까지 거리가 상당히 멀리 떨어져 있는 경우, 입력 전압의 신호케이블은 매우 길고 복잡하게 설치되며 외부 노이즈에 노출되기 쉽다. 본 논문에서는 이러한 문제를 해결하기 위하여 무선 전압 센서를 제안한다. 무선 전압 센서는 전압 센서에서 측정된 신호를 제어보드까지 유선 케이블로 전송하지 않고, 무선 신호로 전송한다. 따라서 입력전원측이 원거리에 있더라도 쉽게 설치할 수 있고 외부 노이즈에 대한 면역성이 강한 PWM AC/DC 컨버터를 제공한다.

• Smart Structures and Systems
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• 제12권6호
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• pp.595-617
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• 2013

Semi-active control equipments are used to effectually enhance the seismic behavior of structures. Magneto-rheological (MR) dampers are semi-active devices that can be utilized to control the response of structures during seismic loads and have received voracious attention for response suppression. They supply the adaptability of active devices and stability and reliability of passive devices. This paper presents an optimal fuzzy logic control scheme for vibration mitigation of buildings using magneto-rheological dampers subjected to near-fault ground motions. Near-fault features including a directivity pulse in the fault-normal direction and a fling step in the fault-parallel direction are considered in the requisite ground motion records. The membership functions and fuzzy rules of fuzzy controller were optimized by genetic algorithm (GA). Numerical study is performed to analyze the influences of near-fault ground motions on a building that is equipped with MR dampers. Considering the uncontrolled system response as the base line, the proposed method is scrutinized by analogy with that of a conventional maximum dissipation energy (MED) controller to accentuate the effectiveness of the fuzzy logic algorithm. Results reveal that the fuzzy logic controllers can efficiently improve the structural responses and MR dampers are quite promising for reducing seismic responses during near-fault earthquakes.

• 한국전산유체공학회지
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• 제15권4호
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• pp.53-59
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• 2010

Preliminary design of a ground plate, a device installed close to the aircraft model for wind tunnel test to simulate the ground effect, was performed by a numerical simulation. A two-dimensional numerical study was performed initially to decide the optimal leading edge and flap configurations. Then, three-dimensional studies were conducted to decide the optimal flap deflection angle for pressure distribution reduction since the plate and the plate supporting system generate static pressure difference between the upper and lower flow regions. Three-dimensional simulation additionally studied the effect of the clearance between the plate and the wind tunnel side wall. For the efficiency of computation, half model was simulated and a symmetric boundary condition was applied on the center plane. Based on the preliminary design, a ground plate was designed, manufactured and tested at the Korea Aerospace Research Institute(KARI) wind tunnel. The measured pressure differences versus flap deflection angle agreed well with the predicted results.

• Coupled systems mechanics
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• 제7권3호
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• pp.269-280
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• 2018

Post-earthquake damages investigation in past and recent earthquakes has illustrated that the ground motion spatial variation plays an important role in the structural response of long span bridges. For the structural control of seismic-induced vibrations of cable-stayed bridges, it is extremely important to include the effects of the ground motion spatial variation in the analysis for design of an effective control system. The feasibility and efficiency of different vibration control strategies for the cable-stayed bridge under multiple support excitations have been examined to enhance a structure's ability to withstand earthquake excitations. Comparison of the response due to non-uniform input ground motion with that due to uniform input demonstrates the importance of accounting for spatial variability of excitations. The performance of the optimized designed control systems for uniform input excitations gets worse dramatically over almost all of the evaluation criteria under multiple-support excitations.

• Journal of Biosystems Engineering
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• 제29권5호
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• pp.425-432
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• 2004

In harvesting rice and barley using combine, the inclination of the body caused by the irregular surface condition of the field and the soil sinking from the unbalanced weight during the grain collection used to make harvesting operation difficult and even impossible. To overcome such a problem hydraulic system far automatic and manual leveling control of a combine has been developed. The system was composed of the combine body and the hydraulic level control system mounted on it. The maximum height of ground clearance was set up to be 290mm. And the limit angle of the leveling control was set up to be $\pm7^{\circ}$. The proposed controller and hydraulic system was implemented to the prototype combine. The prototype combine was designed and built as a separable structure with the body and the track of it. This paper shows results of a specification and design testing with the hydraulic level control system far body of combine.

• International Journal of Aeronautical and Space Sciences
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• 제12권3호
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• pp.283-287
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• 2011

Science and Technology Satellite-3 (STSAT-3) is a 150 kg class micro satellite based with the national space program. The STSAT-3 system consists of a space segment, ground segment, launch service segment, and various external interfaces including additional ground stations to support launch and early operation phases. The major ground segment is the ground station at the Satellite Technology Research Center, Korea Advanced Institute of Science and Technology site. The ground station provides the capability to monitor and control STSAT-3, conduct STSAT-3 mission planning, and receive, process, and distribute STSAT-3 payload data to satisfy the overall missions of STSAT-3. The ground station consists of the mission control element and the data receiving element. This ground station is designed with the concept of low cost and high efficiency. In this paper, the requirements and design of the ground station that has been developed are examined.

• Journal of Astronomy and Space Sciences
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• 제25권2호
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• pp.227-238
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• 2008

위성항법 지상국 기술은 위성으로부터 위성항법신호를 받아 위성항법신호를 감시하고 분석하며 위성에 보정정보를 업로드하는 기술로써 위성항법 인프라 구축에 매우 중요한 기술이며 여러 응용분야에 적용할 수 있는 핵심 기술이다. 이 중 한국전자통신연구원에서 개발하고 있는 감시제어시스템은 GPS 및 갈릴레오 항법 위성으로부터 신호 감시 데이터를 수집하여 위성항법 제어센터로 제공하는 기능을 수행하는 소프트웨어 시스템이다. 이 논문에서는 위성항법 지상국의 구성과 감시제어시스템의 목적 및 형상을 소개한 다음, 감시제어시스템의 적용 알고리즘을 소개하고 감시제어시스템의 예비설계를 기술하였다. 감시제어시스템은 데이터 수집, 데이터 포맷팅 및 저장, 데이터 오차 보정, 항법해 결정, 독립 품질 감시, 시스템 운용 및 유지 등의 모듈로 구성되어 있다. 감시제어시스템의 예비설계는 유스케이스 모델, 도메인 설계, 소프트웨어 구조설계, 사용자 인터페이스 구조 설계 과정을 통하여 이루어진다. 각 단계별 설계과정은 UML(Unified Modeling Language) 표준 방식에 따라 이루어졌다. 이 연구에서 설계된 감시제어시스템은 지상국의 운용 능력을 향상시킬 뿐만 아니라 상세설계의 기초자료로 이용될 것이다.

• 항공우주기술
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• 제7권1호
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• pp.40-48
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• 2008

공기 혼합시스템은 초음속 지상추진시험설비의 축열식 가열기로부터 공급되는 $1000^{\circ}C$, 3.5MPa의 공기와 고압공기 공급원으로부터 공급되는 상온, 동일 압력의 공기를 혼합시켜서 시험부로 공급하기 위한 설비로 32MPa로 압축되어 있는 고압공기 공급원을 3.5MPa로 감압하는 고압/저온 유동제어부, 축열식 가열기의 고온밸브에서부터 공기 혼합기로 고온의 공기를 공급하기 위한 고온 배관, 축열식 가열기로부터 공급되는 고온 유동과 고압공기 공급원으로부터 공급되는 상온 유동을 혼합하기 위한 공기 혼합기로 구성된다. 공기 혼합 시스템을 통하여 완전히 혼합된 공기의 유량은 25kg/s, 온도는 약 $400^{\circ}C$로 이를 통하여 초음속 지상추진시험설비의 구동 영역을 저 마하수, 저 고도 영역까지 확장할 수 있다.