• 제목/요약/키워드: Embedded Power Control

검색결과 277건 처리시간 0.032초

휴대 가능한 Lonworks 네트워크 설치 장비의 설계 (Design of portable Lonworks Network Installation Tool)

  • 이희찬;김명균
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 2006년 학술대회 논문집 정보 및 제어부문
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    • pp.127-129
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    • 2006
  • The distributed control system is used in wide control fields. Factory automation, home network and building automation are good examples. Lonworks that Echelon company has been developing and providing since 1991 is one of popular distributed control systems. Lonwork system is support various communication media, especially it has a feature that supports communication through the power line. When Constructing Lonworks network in a construction field, the experts, who can treat Lonworks bring laptops that LNS and Lonmaker installed, install the network. However this way takes long time to construct the network and needs the experts. To resolve this problem, this paper suggests that a design of Lonworks network installation machine that is easy to use for everyone and portable. Non-experts can install Lonworks network by using this machine so they can reduce fare for installation of network and time to install.

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고속 영상 검지기 시스템 개발에 관한 연구 (Study On Development of Fast Image Detector System)

  • 임태현;이종민;김용득
    • 대한전자공학회:학술대회논문집
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    • 대한전자공학회 2003년도 신호처리소사이어티 추계학술대회 논문집
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    • pp.241-244
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    • 2003
  • Nowadays image processing is very useful for some field of traffic applications. The one reason is we can construct the system in a low price, the other is the improvement of hardware processing power, it can be more fast to processing the data. In this study, I propose the traffic monitoring system that implement on the embedded system environment. The whole system consists of two main part, one is host controller board, the other is image processing board. The part of host controller board take charge of control the total system, interface of external environment. and OSD(On screen display). The part of image processing board takes charge of image input and output using video encoder and decoder, image classification and memory control of using FPGA, control of mouse signal. And finally, fer stable operation of host controller board, uC/OS-II operating system is ported on the board.

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광대역 OFDMA 무선통신시스템의 호 접속제어에 관한 연구 (Study on the Call Admission Control in the Broadband OFDMA Wireless Communication Systems)

  • 백천현
    • 대한산업공학회지
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    • 제34권4호
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    • pp.445-459
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    • 2008
  • This paper addresses a call admission control(CAC) scheme giving handoff calls a priority over new calls for OFDMA wireless communication systems. The characteristics of OFDMA system and a variety of user QoS (Quality of Service) requirements are incorporated into the proposed CAC scheme which consists of several optimization modules for the system resource(subcarriers and power) allocations. The mathematical models and its solution methods for the embedded resource allocation problems are proposed. Some extensive computational experiments are conducted to illustrate the superiority of our CAC.

Herschel-Bulkley 모델을 이용한 MR 댐퍼 승용차의 제어 성능 고찰 (Control Performance Investigation of MR Fluid Damper using Herschel-Bulkley Shear Model)

  • 이덕영;황우석
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2002년도 춘계학술대회논문집
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    • pp.323-328
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    • 2002
  • The control performance of a vehicle installed with an MR(magnetorheological) fluid-based damper is investigated on the basis of Herschel-Bulkley shear model. Generally, most of MR fluid damper has been analyzed based on a simple Bingham-plastic shear model. However, the Bingham-plastic shear model can not well describe the behavior of the damper on the condition of high velocity and high current field input. Therefore, in this study, the Herschel-Bulkley shear model in which the constant post-yield plastic viscosity in Bingham model is replaced with a power law model dependent on shear rate is used to assess control performance of a vehicle with MR fluid damper suspension system. This study deals with a two-degree-of-freedom suspension using the MR fluid damper for a quarter car model. The response for the bump input to identify the fastness of MR fluid damper embedded skyhook controller and requested magnetic field are investigated.

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지게차 마스트 작동내구를 위한 실차 기반 무인시험장치 개발 (Development of an Unmanned Test System Based on Forklift for Mast Operation Durability)

  • 조재홍;나선준;김민석;박명관
    • 드라이브 ㆍ 컨트롤
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    • 제19권4호
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    • pp.70-76
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    • 2022
  • In this paper, we develops an unmanned test system for the purpose of realizing an actual forklift-based test-bed for the operation durability of the forklift mast. First, two robot actuators were applied to the lever to replace lever manipulation of the operator. For detecting the height of the fork and the tilt angle of the mast, the laser displacement sensor and the inclinometer were installed to the forklift. Next, the embedded control system was used to control the robot actuator with reference to test mode. Experimental evaluation verified that developed test system was effective and practical for the viewpoint of the repeatability of the test mode.

Hierarchical Power Management Architecture and Optimal Local Control Policy for Energy Efficient Networks

  • Wei, Yifei;Wang, Xiaojun;Fialho, Leonardo;Bruschi, Roberto;Ormond, Olga;Collier, Martin
    • Journal of Communications and Networks
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    • 제18권4호
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    • pp.540-550
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    • 2016
  • Since energy efficiency has become a significant concern for network infrastructure, next-generation network devices are expected to have embedded advanced power management capabilities. However, how to effectively exploit the green capabilities is still a big challenge, especially given the high heterogeneity of devices and their internal architectures. In this paper, we introduce a hierarchical power management architecture (HPMA) which represents physical components whose power can be monitored and controlled at various levels of a device as entities. We use energy aware state (EAS) as the power management setting mode of each device entity. The power policy controller is capable of getting information on how many EASes of the entity are manageable inside a device, and setting a certain EAS configuration for the entity. We propose the optimal local control policy which aims to minimize the router power consumption while meeting the performance constraints. A first-order Markov chain is used to model the statistical features of the network traffic load. The dynamic EAS configuration problem is formulated as a Markov decision process and solved using a dynamic programming algorithm. In addition, we demonstrate a reference implementation of the HPMA and EAS concept in a NetFPGA frequency scaled router which has the ability of toggling among five operating frequency options and/or turning off unused Ethernet ports.

일체형 방사선 피폭 방호 소방관 인명구조 경보기의 임베디드 보드 개발 (Development of Embedded Board for Integrated Radiation Exposure Protection Fireman's Life-saving Alarm)

  • 이영지;이주현;이승호
    • 전기전자학회논문지
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    • 제23권4호
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    • pp.1461-1464
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    • 2019
  • 본 논문에서는 위치추적과 방사선 측정이 가능한 일체형 방사선 피폭 방호 소방관 인명구조 경보기를 위한 임베디드 보드 개발을 제안한다. 제안하는 방사선 피폭 방호 소방관 인명구조 경보기의 임베디드 보드는 신호 처리부, 통신부, 전원부, 메인 제어부 등으로 구성된다. 신호 처리부에서는 차폐설계, 노이즈 저감 기술 및 전자파 차감 기술 등을 적용한다. 통신부에서는 WiFi 방식을 사용하여 통신하도록 설계한다. 메인 제어부에서는 전력 소모를 최소한으로 줄이고 작고 밀도가 높으면서도 낮은 발열성을 통하여 높은 고성능 시스템을 구성한다. 일체형 방사선 피폭 방호 소방관 인명구조 경보기를 위한 임베디드 보드는 재난 및 화재현장 등 열악한 환경에 노출되어 운영하는 장비이므로 방수와 내열성을 고려한 외형도 설계 및 제작을 한다. 제안된 일체형 방사선 피폭 방호 소방관 인명구조 경보기를 위한 임베디드 보드의 효율을 판단하기 위하여 공인시험기관에서 실험하였다. 방수 등급은 소방관용 장비의 특성 상 재해 현장에서 물에 의한 침수 시에도 안정적인 성능을 유지할 수 있는 IP67 등급을 달성하였다, 동작 온도는 재해현장에서의 폭넓은 환경변화에 대응할 수 있는 -10℃~50℃의 범위에서 측정이 되었다. 배터리 수명은 붕괴사고 등의 비상 재난 상황에 대처할 수 있는 1회 충전 후 144시간 사용 가능함이 측정되었다. PCB를 포함한 최대 통신 거리는 재난 상황 시 지휘통제 차량과의 직선거리에서 기존의 50m보다 넓은 범위인 54.2m에서 작동하는 것이 측정되었다. 따라서 일체형 방사선 피폭 방호 소방관 인명구조 경보기를 위한 임베디드 보드의 그 효용성이 입증되었다.

Development of Hardware-in-the-loop Simulator for Spacecraft Attitude Control using thrusters

  • Koh, Dong-Wook;Park, Sang-Young;Choi, Kyu-Hong
    • 한국우주과학회:학술대회논문집(한국우주과학회보)
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    • 한국우주과학회 2008년도 한국우주과학회보 제17권2호
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    • pp.35.3-36
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    • 2008
  • The ground-based spacecraft simulator is a useful tool to realize various space missions and satellite formation flying in the future. Also, the spacecraft simulator can be used to develop and verify new control laws required by modern spacecraft applications. In this research, therefore, Hardware-in-the-loop (HIL) simulator which can be demonstrated the experimental validation of the theoretical results is designed and developed. The main components of the HIL simulator which we focused on are the thruster system to attitude control and automatic mass-balancing for elimination of gravity torques. To control the attitude of the spacecraft simulator, 8 thrusters which using the cold gas (N2) are aligned with roll, pitch and yaw axis. Also Linear actuators are applied to the HIL simulator for automatic mass balancing system to compensate for the center of mass offset from the center of rotation. Addition to the thruster control system and Linear actuators, the HIL simulator for spacecraft attitude control includes an embedded computer (Onboard PC) for simulator system control, Host PC for simulator health monitoring, command and post analysis, wireless adapter for wireless network, rate gyro sensor to measure 3-axis attitude of the simulator, inclinometer to measure horizontality and battery sets to independently supply power only for the simulator. Finally, we present some experimental results from the application of the controller on the spacecraft simulator.

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냉각탑 수질관리를 위한 자동화 시스템 개발 (Water Quality Control System Development for Cooling Towers)

  • 이기건;송무준;이영재;성상경;강태삼
    • 제어로봇시스템학회논문지
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    • 제14권1호
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    • pp.36-41
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    • 2008
  • Cooling tower is an important equipment of the cooling systems for large buildings like factory and department store. Water used for cooling in cooling tower is reused continuously. If the water is polluted, corrosion and scale can happen at equipments and pipes. In order to prevent this problem, it is necessary to control the water quality using chemicals. To control the water quality, an automatic control system is designed, fabricated, and experimented. The control system is based on an imbedded microcontroller. Relays are used for power driving, an LCD and LED for display, and RS485 for remote data acquisition. Monitoring program is also developed for easy man-machine interface and extraction of data stored in the imbedded processor and EEPROM. The control system calculates amounts of chemicals necessary using sensor data and injects the chemicals into the cooling tower on proper time. The developed water quality control system is expected to reduce cost of maintenance and extend the lifetime of the cooling systems with low cost.

Development of a Hardware-in-the-loop Simulator for Spacecraft Attitude Control Using Thrusters

  • Koh, Dong-Wook;Park, Sang-Young;Kim, Do-Hee;Choi, Kyu-Hong
    • Journal of Astronomy and Space Sciences
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    • 제26권1호
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    • pp.47-58
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    • 2009
  • In this study, a Hardware-In-the-Loop (HIL) simulator using thrusters is developed to validate the spacecraft attitude system. To control the attitude of the simulator, eight cold gas thrusters are aligned with roll, pitch and yaw axis. Also linear actuators are applied to the HIL simulator for automatic mass balancing to compensate the center of mass offset from the center of rotation. The HIL simulator consists of an embedded computer (Onboard PC) for simulator system control, a wireless adapter for wireless network, a rate gyro sensor to measure 3-axis attitude of the simulator, an inclinometer to measure horizontal attitude, and a battery set to supply power for the simulator independently. For the performance test of the HIL simulator, a bang-bang controller and Pulse-Width Pulse-Frequency (PWPF) modulator are evaluated successfully. The maneuver of 68 deg. in yaw axis is tested for the comparison of the both controllers. The settling time of the bang -bang controller is faster than that of the PWPF modulator by six seconds in the experiment. The required fuel of the PWPF modulator is used as much as 51% of bang-bang controller in the experiment. Overall, the HIL simulator is appropriately developed to validate the control algorithms using thrusters.