• Journal of the Korea Academia-Industrial cooperation Society
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• v.16 no.3
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• pp.1677-1683
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• 2015

To cope with exhaust gas regulation, Diesel engine applied to electronic control system. As it accurately regulated the injected fuel mass and the fuel efficiency and the output are increased but the noise and the vibration are decreased. In order to keep the performance of Electronic Diesel Control System, it is important to accurately control the fuel pressure. However, when the regulator of fuel pressure is not controlled properly, the failure phenomenons(starting failure, staring delay, accelerated failure, engine mismatch et al.) occur because the fuel pressure is not stabilize. In this study, effects on a fuel pressure, engine rotating speed according to the control rate of fuel-pressure regulator are investigated in order to analyzed the performance variation with failure of fuel-pressure regulator. As a result, when the control rate of a fuel-pressure regulator is 4%~6% lower than that of standard condition, the variation of engine's rpm and return fuel flow is increased, and the abnormal condition was occurred. Besides, it is possible to diagnose the failures on fuel-pressure regulator under these conditions.

• Proceedings of the Korea Society for Energy Engineering kosee Conference
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• 1993.11a
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• pp.73-77
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• 1993

박막모델을 사용하여 연료전지 성능에 영향을 주는 여러 인자들에 대해 전압과 전류의 관계를 모사 하여 비교하였다. 또한 단위전지에 대해 제어루프를 구성함으로서 전극성능 모델식을 이용한 연료전지의 제어 가능성을 확인하였다. 확산계수가 증가할수록 그리고 전극두께가 얇고 전극의 세공반경이 클수록 전극성능은 증가하였다. 단위전지의 제어를 위해서 양극과 음극의 반응기체 유속을 조절할 수 있는 압력에 대해 설정치 변화와 외란의 변화에 대한 제어모사를 행한 결과 각 전극의 압력이 설정점에 빠르게 수령하여 연료전지의 효과적인 제어가 가능함을 검증하였다.

• Proceedings of the KIPE Conference
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• 2000.07a
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• pp.682-684
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• 2000

에너지 절약과 환경 공해분제 그리고 최근에 부각되고 있는 지구온난화 문제 등을 해결하기 위해 고효율 발전시스템인 연료전지가 주목을 받고 있다 연료전지는 연소과정 없이 화학에너지를 전기 화학적으로 직접 전기로 변환시키는 시스템으로 효율이 높고 공해 물질의 배출이 거의 없기 때문에 매우 이상적인 발전장치이다. 연료전지 발전시스템의 철거 제어기 설계를 위해 필요한 운전 조건 즉 운전온도 압력 등의 운전조건과 연료 농도 공급량이 전지의 성능에 미치는 영향에 대한 특성을분석하였고 이들을 정리하여 최적제어를 위한 기본방식을 얻기 위해 이용하였다 실재 스택에 적용하기 위한 관련 측정시스템과 제어기는 dSPACE-1103과 ControlDesk를 사용하여 구성하였다.

• Journal of the Korean Electrochemical Society
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• v.6 no.1
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• pp.48-52
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• 2003

A mathematical dynamic model of fuel cell was formulated in order to design the control system which will meet the control object. The control objective is set to regulate the airflow in the load change by utilization of airflow and the pressure difference between anode and cathode is maintained below a limit range. Simulation result of 10kW polymer electrolyte membrane fuel cell (PEMFC) clearly demonstrates that response time need to be less. than 1 seconds for the control requirements. Besides, pressure difference was allowed in pressure range less than 0.01 atm.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.12 no.12
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• pp.5997-6003
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• 2011

To increase the driving distance of a natural gas vehicle, the high pressure of fuel charge is necessary and the development of the device reducing the pressure to suitable pressure for fuel of high pressure. In this study, Pressure characteristics at the pressure regulator, which is very important for gas supply systems for vehicles, are investigated. Numerical simulations are carried out to quantify pressures at regulators for several flow rates and to investigate pressure drop, hysteresis losses at some parts in the pressure regulator. Moreover, this paper presents a new kind of hydraulic simulation which is composed of CNG regulator. Lastly, experiments are carried out to verify the effectiveness of the prosed mathematical simulation with various regulator components as in real working condition.

• Transactions of the Korean Society of Automotive Engineers
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• v.21 no.2
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• pp.114-121
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• 2013

High efficiency operation is required for motors of vehicle to increase fuel efficiency due to the regulation of exhaust gas. This paper presents a control method of fuel pressure to increase fuel efficiency and a sensorless control method of BLDC motor to get higher efficiency than conventional brushed DC motor. Initial rotor position of BLDC motor is detected from current value that is occurred by test voltage pulse and rotor is accelerated by defined sequence to enter sensorless operation mode. The algorithm to control flow rate of fuel pump uses PI controller that is control motor speed to maintain the target fuel pressure commanded by ECU.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.38 no.2
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• pp.107-114
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• 2014

This paper proposes a common rail pressure control algorithm for passenger car diesel engines. For handling the parameter-varying characteristics of common rail systems, the quantitative feedback theory (QFT) is applied to the design of a robust rail pressure control algorithm. The driving current of the pressure control valve and the common rail pressure are used as the input/output variables for the common rail system model. The model parameter uncertainty ranges are identified through experiments. Rail pressure controller requirements in terms of tracking performance, robust stability, and disturbance rejection are defined on a Nichols chart, and these requirements are fulfilled by designing a compensator and a prefilter in the QFT framework. The proposed common rail pressure control algorithm is validated through engine experiments. The experimental results show that the proposed rail pressure controller has a good degree of consistency under various operating conditions, and it successfully satisfies the requirements for reference tracking and disturbance rejection.

• Aerospace Engineering and Technology
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• v.1 no.2
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• pp.51-56
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• 2002

Satellite propulsion system is employed for orbit transfer, orbit correction, and attitude control. The monopropellant feeding system in the low-earth-orbit satellite blowdowns fuel to the thrust chamber. The thrust produced by the thruster depends on fuel amount flowed into the combustion chamber. If the thruster valve be given on-off signal from on-board commander in the satellite, valve will be opened or closed. When the thrusters fire fuel flows through opened thruster valve, instantaneous stoppage of flow in according to valve actuation produces transient pressure due to pressure wave. This paper describes transient pressure predictions of the KOMPSAT-2 propulsion system resulting from latching valve and thrust control valve operations. The time-dependent set of the fluid mass and momentum equations are calculated by MOC.

• Proceedings of the KIPE Conference
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• 2006.06a
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• pp.216-218
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• 2006

본 논문에서는 연료전지용 듀얼 부스트 컨버터의 전압제어루프의 피드백 루프에 디지털 필터를 도입하여 부하에 의해 발생하는 출력전압의 저고조파 리플성분을 제거한 측정값을 사용함으로써 입력전류의 저고조파 리플을 제거하고, 전류제어루프에 predictive deadbeat 제어기법을 적용하여 제어주기와 제어알고리듬 계산에 의한 시간적 지연에 의해 발생되는 동적응답특성의 저하를 최소화한다. 센서를 사용하는 대신 연료전지 스택에 공급되는 수소와 공기의 압력과 스택의 출력전류에 결정되는 연료전지의 전압-전류 특성곡선을 이용하여 부스터 컨버터의 입력전압을 계산하고 전류를 제어함으로써 연료전지 시스템의 성능을 최적화한다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2000.11a
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• pp.8-8
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• 2000

하이드라진 단기액체엔진을 장착하고 궤도에서 임무를 수행하고 있는 다목적실용 위성 추진시스템 궤도비행 초기운용 자료에 근거하여 추진제 소모율을 산정 한다. 추진시스템은 위성의 궤도각과 비행고도 조정을 위한 속도증분($\Delta$V) 및 자세제어를 위한 추력을 발생시킨다. 단기액체 추진시스템에서 추진제 소모량은 추력기 밸브의 개폐시간에 비례하고 추력 생성 효율은 추진제의 연소기 유입압력에 종속한다. 일정질량의 가압 기체 압력에 의해 연료를 공급하는 추진시스템에서 잔류 추진제 량의 감소는 연소기 유입압력의 감소를 유발하고 추진기관의 효율을 저하시키는 요인으로 작용하여 임무말기로 진행함에 따라 동일한 운동량 생성에 보다 많은 연료소모가 이루어진다.(중략)