• 펄프종이기술
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• 제35권5호
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• pp.46-52
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• 2003

In this work we developed the closed-loop model of a paper machine during grade change with the intention to provide a reliable dynamic model to be used in the model-based grade change control scheme. During the grade change, chemical and physical characteristics of paper process change with time. It is very difficult to represent these characteristics on-line by using physical process models. In this work, the wet circulation part and the drying section were considered as a single process and closed-loop identification technique was used to develop the grade change model. Comparison of the results of numerical simulations with mill operation data demonstrates the effectiveness of the model identified.

• 제어로봇시스템학회논문지
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• 제3권3호
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• pp.280-288
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• 1997

In this paper, we will show that the torque ripple in closed-loop drives of permanent magnet stepping motors is reduced as properly selected lead angle control method. We propose an instantaneous torque equation, which is the function of lead angle, to estimate the influence on torque ripple. We design a closed-loop lead angle control system based on the proposed instantaneous torque equation and measure the instantaneous torque in various excitation modes. It is shown that torque ripple is greatly reduced, as seen from the experimental results as well as from the computer simulation results. For example, torque ripple reduced from 78.25% to 46.82% in the case of 50 PPS single-phase excitation mode operation.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 1989년도 한국자동제어학술회의논문집; Seoul, Korea; 27-28 Oct. 1989
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• pp.109-112
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• 1989

Gun system operation is represented as a first-order Markov process, and an optimum linear filter is derived for closed-loop control of mean square error. Potential improvement is then estimated by contrasting the variance in performance and the auto correlation for open-loop system with that for the optimum linearly corrected process.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 2003년도 ICCAS
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• pp.1537-1541
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• 2003

In this paper, presented is a feedback control performance of vibratory gyroscope at various vacuum levels. Micro gyroscope, whose operation is based on the vibrating motion at the vacuum conditions, is highly influenced by the vacuum level of the operating circumstances. In general, we apply the feedback control scheme to the gyroscope in order to improve the performances of the sensor. And control performances of the gyroscope are related to those vacuum levels. So we need investigate the performances of the closed loop control at various vacuum conditions comparing with those of the open loop. The experimental results show that the sensitivity of the closed loop is less than that of the open loop especially in low vacuum conditions. Therefore, there should be trade-off between sensitivity and other sensor performances such as linearity, bandwidth when we apply feedback control to the gyroscope.

• 신재생에너지
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• 제17권3호
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• pp.32-41
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• 2021

A groundwater source heat pump (GWHP) was developed in this study by adapting a borehole heat exchanger with closed-loop and open-loop systems in a new building. In the pilot test building, the air-conditioning on the second floor was designed to employ a closed-loop system and that on the third floor had an open-loop system. The GWHP design is based on the feasibility of groundwater resources at the installation site. For the hydrogeological survey of the study site, pumping and injection tests were conducted, and the feasibility of GWHP installation was evaluated based on the air-conditioning load demand of the building. The site was found to be satisfactory for the design capacity of the thermal load and water quality. In addition, the effect of groundwater movement on the performance of the closed-loop system was tested under three different operational scenarios of groundwater pumping. The performance of the system was sustainable with groundwater flow but declined without appropriate groundwater flow. From long-term observations of the operation, the aquifer temperature change was less than 2℃ at the observation well and 5℃ at the injection well with respect to the initial groundwater temperature. This pilot study is expected to be of guidance for developing GWHPs at fractured rock aquifers.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2009년도 제33회 추계학술대회논문집
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• pp.38-41
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• 2009

액체산소/케로신 추진제 액체로켓엔진 개발기술 확보를 위해, 연소기를 제외한 터보펌프, 가스발생기 등의 30톤급 엔진 주요 구성품을 이용한 터보펌프+가스발생기 폐회로 연계시험을 수행하였다. 연소기를 유량제어 요소로 모사한, 엔진시스템 모사조건에서 터보펌프+가스발생기 폐회로 연계시험기의 예냉 절차, 시동 특성, 정격조건 작동 및 정지가 성공적으로 수행되었다. 터보펌프와 가스발생기의 작동성을 검증하였다. 연계시험기의 터보펌프 회전수 및 혼합비 피드백 제어를 위한 제어시스템도 검증되었다. 본 폐회로 연계시험 결과는 액체로켓엔진 선행 기술 개발에 활용될 것이다.

• 대한환경공학회지
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• 제34권12호
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• pp.821-827
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• 2012

슬러지 공기건조장치는 외기로부터 공기를 흡입/송풍하여 이젝터(Ejector) 및 다단 사이클론(Multi-Cyclone)에서 슬러지를 건조하는 시스템이다. 즉 공기건조장치는 외기의 조건에 따라 시스템 성능 변화가 클 뿐 아니라 개루프(Open-Loop) 구조로 되어 있어 에너지 소모량이 큰 단점이 있다. 이를 해결하기 위한 방안으로 공기건조장치의 분리기 후단에 응축기(Condenser), 냉각기(Cooler), 압축기(Compressor)로 구성된 제습기를 장착하여 송풍-건조-제습-송풍으로 순환하는 폐루프(Closed-Loop) 공기건조 기술을 개발하였다. 기존의 공기건조와 비교하여 본 기술의 특성을 비교 분석한 결과, 본 시스템의 공기는 외기에 비하여 약 50% 이상의 에너지를 더 많이 함유하고 있었다. 또한 공기가 시스템 내에서 순환하기 때문에 슬러지 건조에 공급하는 공기의 질을 일정하게 유지할 수 있어 시스템을 안정적으로 운용할 수 있을 것으로 분석되었다. 그리고 경제성을 분석한 결과, 폐루프 공기건조장치를 이용하여 슬러지 1톤을 건조하는데 소요되는 비용은 기존의 건조장치에 비하여 약 35% 절감되는 것으로 파악되었다. 따라서 본 기술은 에너지 소모량이 적고, 일정한 품질의 공기를 송풍할 수 있어 시스템의 안정적으로 운전할 수 있는 기술로 평가된다.

• Industrial Engineering and Management Systems
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• 제8권3호
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• pp.162-170
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• 2009

This paper deals with a closed-loop remanufacturing system with one manufacturer and one remanufacturer. The manufacturer sells new products bearing the 'Extended Producer Responsibility (EPR).' It is assumed that the manufacturer's collection rate of used products depends only on the buy-back cost, while that of the remanufacturer depends on the minimum allowed quality level of used products in addition to the buy-back cost. Through the development of mathematical models with the objective function of maximizing profit, we study an efficient operation policy of each party. The decision variables are the unit selling price of new products and remanufactured products, the unit buy-back cost of the used products of the manufacturer and remanufacturer, and the minimum allowed quality level. The validity of the model is examined through numerical examples and sensitivity analysis.

• 제어로봇시스템학회논문지
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• 제10권10호
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• pp.956-960
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• 2004

The Vehicle Dynamic Simulator(VDS) is a key equipment of the performance verification of attitude control subsystem and it simulates the real dynamic environment that spacecraft undergoes during mission operation. All the software models and hardware interfaces necessary for the closed-loop simulation of the spacecraft dynamics are implemented. Using VDS, KOMPAT-2 attitude control logic functions and performance was verified. In this paper, the hardware and software configurations of KOMPSAT-2 VDS was described briefly and the information flow and exchanges between software models and actual hardwares during close loop simulation was described in the systematic point of view.

• 대한전기학회논문지
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• 제41권6호
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• pp.615-624
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• 1992

For the operation of the resonant DC link inverters, only limited number of modulation techniques such as the delta modulation and instantaneous current control techniques have been suggested. However, these modulation techniques have some limitations in practical operation. In this paper, the application of conventional inverter modulation techniques is suggested for the control of the resonant DC link inverter. The harmonic analysis results are presented. The results show that these modulation techniques offer good output characteristics similar to conventional inverter PWM techniques for the operation of the resonant DC link inverter. This implies that not only the delta modulation technique and instantaneous current control techniques but also various other modulation techniques can be applied to the operation of the resonant DC link inverter. This also indicates that open loop control as well as closed loop control can be used for the operation of the resonant inverter. The resonant DC link inverter with various modulation strategies is implemented using V-40 microprocessors.