• Title/Summary/Keyword: Firing Control System

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A Study on firing control of generator control system (발전기 제어시스템의 점호제어에 관한 연구)

  • Lee, Joo-Hyun;Lim, Ick-Hun;Ryu, Ho-Sun;Jeong, Tae-Won
    • Proceedings of the KIPE Conference
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    • 2007.07a
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    • pp.488-490
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    • 2007
  • 발전기 제어시스템은 동기발전기의 무효전력 또는 단자전압의 변화에 제어기의 출력신호에 따른 점호제어를 통하여 발전기 계자에 흐르는 전류를 자동조정 함으로써 발전기 단자전압을 목표 값으로 신속하고 안정하게 유지하게 된다. 본 논문에서는 발전기 제어시스템의 위상제어 정류기에서 점호제어 방식에 대하여 살펴보고 점호제어 회로의 특성분석과 실제 발전기 제어시스템에 적용된 결과를 기술하고자 한다.

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Design of FPGA in Power Control Unit for Control Rod Control System (원자로 제어봉 구동장치 제어시스템용 전력제어기 FPGA 설계)

  • Lee, Jong-Moo;Shin, Jong-Ryeol;Kim, Choon-Kyung;Park, Min-Kook;Kwon, Soon-Man
    • Proceedings of the KIEE Conference
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    • 2003.11c
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    • pp.563-566
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    • 2003
  • We have designed the power control unit which belongs to the power cabinet and controls the power supplied to Control Rod Drive Mechanism(CRDM) as a digital system based on Digital Signal Processor(DSP). The power control unit dualized as the form of Master/Slave has had its increased reality. The Central Process Unit(CPU) board of a power control unit possesses two Digital Signal Processors(DSPs) of the control DSP for performing the tasks of power control and system monitoring and the communication of the Control DSP and the Communication DSP. To accomplish the functions requested in the power control unit effectively, we have installed Field Programmable Gate Arrays(FPGAS) on the CPU board and have FPGAs perform the memory mapping, the generation of each chip selection signal, the giving and receiving of the signals between the power controllers dualized, the fault detection and the generation of the firing signals.

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Noise Control of an Air Intake system for a Four-Cylinder Engine (4기통 엔진의 흡기계 소음제어)

  • 김태정;홍상범
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 1996.10a
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    • pp.77-83
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    • 1996
  • Noise control process of an air intake system for a four-cylinder automotive engine is described. The objective of the process is reduction of induction noise without losing engine performance and changing package layout. The theory and feasibility for noise control elements are also discussed. In general, four-cylinder engines generate a lower frequency induction noise around 80-150 Hz (2400-4500 rpm) and firing frequency, valve impact noise are the main sources. In this paper, the most problematic noise source is identified first and better position of air inlet is selected between inside-fender and out-of-fender layouts. Secondly, the possible noise control approach and CAE analysis results are compared to those from speaker excitation tests. Finally, the effect of the controlled intake system after the installation to an automobile is presented.

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A Study on the High Performance Slip Power Recovery System in Induction Motor (유도전동기의 고성능 슬립전력 회수방식에 대한 연구)

  • Park, Han-Ung;Park, Seong-Jin;An, Jin-U;Park, Jin-Gil;Kim, Cheol-U;Hwang, Myeong-Mun
    • The Transactions of the Korean Institute of Electrical Engineers B
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    • v.48 no.8
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    • pp.431-439
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    • 1999
  • Among the variable-speed AC motor drive systems, the static slip power recovery system has been widely adopted in large power drives because a high efficiency drive can be obtained by recovering the slip power to the AC line. Although many improvements have been made in this system, several problems also remain such as the need of transformer in inverter AC side, which results in limiting speed control range and increasing the losses, production of reactive power by the control of inverter firing angle, harmonics in line currents, and so on. This paper presents the novel high performance slip power recovery system using the boost converter and small size filter in the rotor circuit, which recovers slip power of a wound rotor induction machine to AC supply efficiently with the aid of the boost converter, in which most of the problems in conventional system can be solved. The speed can be controlled by the duty ratio of the converter switch, not by inverter firing angle. As a results, the proposed system can operate in high power factor and the harmonic currents caused by the inverter and rectifier can be considerably suppressed. The validity of the proposed system verified by demonstrating the good agreement in the simulation and experimental results.

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Behavior Control of Autonomous Mobile Robots using ECANS1 (진화하는 셀룰라 오토마타를 이용한 자율이동로봇군의 행동제어)

  • Lee, Dong-Wook;Chung, Young-June;Sim, Kwee-Bo
    • Proceedings of the KIEE Conference
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    • 1998.07g
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    • pp.2183-2185
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    • 1998
  • In this paper, we propose a method of designing neural networks using biological inspired developmental and evolutionary concept. The living things are best information processing system in themselves. One individual is developed from a generative cell. And a species of this individual have adapted itself to the environment by evolution. Ontogeny of organism is embodied in cellular automata and phylogeny of species is realized by evolutionary algorithms. The connection among cells is determined by a rule of cellular automata. In order to obtain the best neural networks in the environment, we evolve the arrangement of initial cells. The cell, that is neuron of neural networks, is modeled on chaotic neuron with firing or rest state like biological neuron. A final output of network is measured by frequency of firing state. The effectiveness of the proposed scheme is verified by applying it to navigation problem of robot.

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Novel Third Harmonic Current Injection Technique for Harmonic Reduction of Controlled Converters

  • Eltamaly, Ali M.
    • Journal of Power Electronics
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    • v.12 no.6
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    • pp.925-934
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    • 2012
  • Three-phase controlled converters have many applications in the utility interfacing of renewable energy sources and adjustable speed drives as a rectifier or inverter. The utility line currents of these converters have a high harmonic distortion, which is more than the harmonic standards. This paper introduces a new technique for circulating the third harmonic currents from the dc-link to the line currents to reduce their harmonic contents. The proposed system uses a single-phase PWM converter to control the angle and amplitude of the injection current for each of the firing angle of a three-phase converter. A detailed analysis is introduced to achieve a relationship between the firing angle of the three-phase controlled converter and the power angle of the PWM converter. In addition, a detailed design for the other injection path components is introduced. A simulation and experimental work is introduced to prove the mathematical derivations. Analysis, simulation and experimental results prove the superiority of the proposed technique.

Development of Combustion Test Facility for Liquid Locket Engine (액체로켓엔진 성능 및 냉각특성 연구를 위한 연소시험 장치 개발)

  • Lee Sung-Woong;Kim Dong-Hwan;Kim Young-Soo
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2004.10a
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    • pp.189-192
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    • 2004
  • Test Facility for hot firing test of small size liquid rocket engine has been developed to research the cooing characteristics of kerosene for cylinder part especially. Propellants for the tests are kerosene and liquid oxygen as fuel and oxidizer respectively and they are fed by gaseous nitrogen. The engine components used hot firing test except for cylinder are cooled by tap-water. Valves for supply of propellants and coolants are controlled by pneumatically. System control and data recording are conducted automatically.

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HVDC System Design for AC Network Reactive Power Control (AC 계통 무효전력 제어를 위한 HVDC 시스템 설계)

  • Choi, Soon-Ho;Choi, Jang-Hum;Kim, Chan-Ki
    • The Transactions of The Korean Institute of Electrical Engineers
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    • v.62 no.1
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    • pp.8-20
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    • 2013
  • This paper deals with the concept design of HVDC system for controlling AC network reactive power. HVDC system can control active power and reactive power and the control concept of reactive power is similar to SVC(Static Var Compensator). Reactive power is controlled by adjusting firing angle of HVDC system under the condition that AC filters are switched. Reactive power depends on AC voltage condition, considering the steady-state and transient state to maintain the stable operation of AC network in the viewpoint of voltage stability. Therefore, in the design stage of HVDC, the reactive power required in the AC network must be considered. For the calculation of operation angle in HVDC system, the expected reactive power demand and supply status is examined at each AC system bus. The required reactive power affects the determination of the operation angle of HVDC. That is, the range of "control deadband" of operation angle should have the capability supplying the required reactive power. Finally, the reactive power control concepts is applied to 1GW BTB Pyeongtaek-Dangjin HVDC system.

EMTDC Modeling of Cheju-Haenam HVDC System (제주-해남 HVDC 시스템의 EMTDC 모델링)

  • 김찬기
    • The Transactions of the Korean Institute of Power Electronics
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    • v.6 no.1
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    • pp.1-12
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    • 2001
  • This paper deals with HVDC simulation. And the purpose of this paper is to reproduce measurements recorded at HVDC site and to verify the control gains and control actions. In this paper, the target of simulation study is Cheju-Haenam HVDC system. Because Cheju-Haenam HVDC system include analogue controller and digital controller, the detailed digital model considered nonlinear characteristics of analogue controllers is development for high accurate firing and control action. Finally the simulation results which is simulated by PSCAD/EMTDC is compared with measurement signals.

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A study on the 3-axis attitude stabilization of Koreasat (무궁화 방송통신 위성의 3축 자세 안정화 장치에 관한 연구)

  • 진익민;백명진;김진철
    • 제어로봇시스템학회:학술대회논문집
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    • 1993.10a
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    • pp.793-798
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    • 1993
  • In this study the attitude control of the KOREASAT is investigated. The KOREASAT is a geostationary satellite and its 3 attitude angles, namely, roll, pitch and yaw angles, are stabilized by using the 3-axis stabilization technique. In the pitch control loop, the pitch attitude angle received from the earth sensor is processed in the attitude processing electronics by using PI type control logic, and the control command is sent to the momentum wheel assembly to generate the control torque by varying the wheel rate. The roll/yaw attitude control is performed by activating a magnetic torquer or by firing appropriate thrusters. The magnetic torquer interacts with the earth magnetic field to produce the control torque, and the thrusters are used to control the larger roll attitude errors. In this study dynamic modelling of the satellite is performed. And the earth sensor, the momentum wheel, and the magnetic torquer are mathematically modelled. The 3-axis attitude control logic is implemented to make the closed-loop system and simulations are carried out to verify the implemented control laws.

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