• 제목/요약/키워드: Closed loop control

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순환형 공급체인 환경에서 시설 통합에 의한 물류원가 절감 및 재고관리시스템 모델구축에 관한 연구 (Study on Reducing Logistics Costs and Inventory Control System according to facilities integration in the Closed-Loop Supply Chain Environment)

  • 이정은
    • 한국산업정보학회논문지
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    • 제19권5호
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    • pp.81-90
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    • 2014
  • 순방향물류와 역방향물류의 두 물류 체인을 통합해서 자원 순환형 공급체인 (CLSC: closed-loop supply chain) 을 구성하는 것은 기업의 비용절감을 위해서 반드시 필요한 요소이다. 본 연구에서는 순환형 공급체인의 환경에서 순방향물류의 도매점과 역방향물류의 처리센터의 재고를 통합하는 재고관리를 제안한다. JIT(Just-in-Time)배송이 고려된 새로운 CLSC 재고관리모델은, 회수센터에서 처리센터로 배송된 사용이 끝난 제품이 도매업자의 수요에 미치지 못할 때 제조사에게 필요한 제품을 재발주 할 것이지 사용이 끝난 제품의 회수를 기다릴 것이지를 선택함으로써 비용을 절감한다. 제안 모델의 유효성을 검증하기 위하여 최적화 기법중 하나인 유전자 알고리즘(Genetic Algorithm: GA)을 이용하였다. 파라미터가 해에 미치는 영향을 알아보기 위해서 세 가지 파라미터 조건에서 우선 순위형 GA (priority-based GA: priGA)와, 각 세대마다 파라미터가 조정되는 개량형 하이브리드 GA (modified Hybrid Genetic Algorithm: mhGA)를 사이즈가 다른 4가지 수치 예에 적용하여 시뮬레이션을 실시하였다.

Closed-loop predictive control using periodic gain

  • Lee, Young-Il
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 1994년도 Proceedings of the Korea Automatic Control Conference, 9th (KACC) ; Taejeon, Korea; 17-20 Oct. 1994
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    • pp.173-176
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    • 1994
  • In this paper a closed-form predictive control which takes the intervalwise receding horizon strategy is presented and its stability properties are investigated. A slate-space form output predictor is derived which is composed of the one-step ahead optimal output prediction, input and output data of the system. A set of feedback gains are obtained using the dynamic programming algorithm so that they minimize a multi-stage quadratic cost function and they are used periodically.

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HUMAN-IN-THE-LOOP EVALUATION OF A VEHICLE STABILITY CONTROLLER USING A VEHICLE SIMULATOR

  • Chung, T.;Kim, J.;Yi, K.
    • International Journal of Automotive Technology
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    • 제5권2호
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    • pp.109-114
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    • 2004
  • This paper presents a closed-loop evaluation of the Vehicle Stability Control (VSC) system using a vehicle simulator. Human driver-VSC interactions have been investigated under realistic operating conditions in the laboratory. Braking control inputs for vehicle stability enhancement have been directly derived from the sliding control law based on vehicle planar motion equations with differential braking. A driving simulator has been validated using actual vehicle driving test data. Real-time human-in-the loop simulation results in realistic driving situations have shown that the proposed controller reduces driving effort and enhances vehicle stability.

Optimal Bandwidth Allocation and QoS-adaptive Control Co-design for Networked Control Systems

  • Ji, Kun;Kim, Won-Jong
    • International Journal of Control, Automation, and Systems
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    • 제6권4호
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    • pp.596-606
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    • 2008
  • In this paper, we present a co-design methodology of dynamic optimal network-bandwidth allocation (ONBA) and adaptive control for networked control systems (NCSs) to optimize overall control performance and reduce total network-bandwidth usage. The proposed dynamic co-design strategy integrates adaptive feedback control with real-time scheduling. As part of this co-design methodology, a "closed-loop" ONBA algorithm for NCSs with communication constraints is presented. Network-bandwidth is dynamically assigned to each control loop according to the quality of performance (QoP) information of each control loop. As another part of the co-design methodology, a network quality of service (QoS)-adaptive control design approach is also presented. The idea is based on calculating new control values with reference to the network QoS parameters such as time delays and packet losses measured online. Simulation results show that this co-design approach significantly improves overall control performance and utilizes less bandwidth compared to static strategies.

Absolute Stability Margins in Missile Guidance Loop

  • Kim, Jong-Ju;Lyou, Joon
    • International Journal of Control, Automation, and Systems
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    • 제6권3호
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    • pp.460-466
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    • 2008
  • This paper deals with the stability analysis of a missile guidance loop employing an integrated proportional navigation guidance law. The missile guidance loop is formulated as a closed-loop control system consisting of a linear time-invariant feed-forward block and a time-varying feedback gain. Based on the circle criterion, we have defined the concept of absolute stability margins and obtained the gain and phase margins for the system assuming 1 st order missile/autopilot dynamics. The correlation between the absolute stability margins and the margins derived from the frozen system analysis is also discussed.

ZVT 풀 브리지 DC/DC 컨버터의 병렬 운전 및 제어기 설계에 관한 연구 (A Study on the Parallel Operation and Control Loop Design of ZVT-Full Bridge DC/DC Converter)

  • 배진용;김용;윤석호;장성원;이규훈
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 2001년도 춘계학술대회 논문집 전기기기 및 에너지변환시스템부문
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    • pp.324-328
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    • 2001
  • This paper presents parallel operation and control loop design of ZVT(Zero Voltage Transition) Full Bridge DC/DC Converter. At parallel operation of ZVT Full Bridge Converter, dynamic current shared inductor devides the same current of unit converter and ZVT circuit and aids to high efficiency in the system. Base on the modeling of ZVT. Full Bridge Converter, the control loop is designed using a simple two-pole, one-zero compensation circuit. To show the validity of the design procedures, the small signal analysis of the closed loop system and open loop system is carried out and the superiority of the dynamic characteristics is verified through the experiment with a 2kW, 50kHz prototype converter.

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주파수 선택적 Rayleigh 페이딩 채널에서 cdma2000 순방향링크의 고속 폐루프 전력제어에 대한 성능 평가 (Performance Evaluation for Fast Closed-Loop Power Control of cdma2000 Forward Link in frequency-Selective Rayleigh Fading Channel)

  • 강법주;남윤석
    • 한국통신학회논문지
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    • 제26권11B호
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    • pp.1522-1533
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    • 2001
  • 본 논문에서는 cdma2000 시스템에서 순방향 폐루프전력제어를 위해 수신 E$_{b}$/I$_{o}$ 를 추정하는 방법을 다루고 있다. 이동국 수신 b//I$_{o}$ 의 추정은 순방향 전력제어 부채널(forward power control subchannel) 전송 심벌을 이용하고 있다. 수신비트에너지와 잡음분산의 추정은 주파수 선택적 Rayleigh 페이딩 채널에서 해석되었다. 특히, 수신비트에너지의 추정은 SIR(signal-to-interference ratio)을 향상시키기 위해서 rake 핑거들과 1/Q 수신심벌들웨 대하여 코히런트 결합에 의해 수행되었다. 그리고 본 논문에서는 차량속도와 전력조정스텝크기에 따른 순방향 폐루프 전력제어의 성능을 비트오율과 전력제어에러 측면에서 평가하고 있다. 시뮬레이션 결과로는 차량속도에 따른 최적의 전력조정스텝크기를 제시하고 있다.

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강압형 스위치드-커패시터 DC-DC 컨버터의 동특성해석 및 제어회로 설계 (Dynamic Analysis and Control Design of a Step-Down Switched-Capapcitor Dc-Dc Converter)

  • 최병조
    • 전력전자학회:학술대회논문집
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    • 전력전자학회 2000년도 전력전자학술대회 논문집
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    • pp.485-488
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    • 2000
  • In this paper dynamic analyses and control design of a step-down switched-capacitor dc-dc converter are presented. Open-loop dynamics of the converter are analyzed using the stage-space averaging technique. A systmatic control design method that offers excellent closed-loop performance for the converter is proposed, The analysis results and dynamic performance of the converter are verified using 18 W experimental converter that delivers a 5V/3.5V output from a 11-16V input source.

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극점배치기능을 갖는 LQ제어기 설계 및 자동차 능동 현가장치 제어에의 응용 (Linear Quadratic Control with Pole Placement for an Automotive Active Suspension System)

  • 최재원;서영봉;유완석
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 1995년도 추계학술대회 논문집
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    • pp.513-517
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    • 1995
  • In this paper, a relation of matrix Q in cost function to distances between the closed-loop and open-loop poles of a multi input controllable systems is studied. Futhmore, the state feedback gain with exact desired eigenvalues in the LQR is computed. The proposed scheme is applied to designing automotive active suspension control system for a half-car model and its performance is compared with the existing LQR control system design methodology.

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2자유도 $H_{\infty}$제어기를 이용한 비행체 자동조종장치 설계 (Autopilot Design with Two Degree of Freedom $H_{\infty}$ Control Method)

  • 최광진;황준하;권오규
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 1996년도 한국자동제어학술회의논문집(국내학술편); 포항공과대학교, 포항; 24-26 Oct. 1996
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    • pp.1304-1307
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    • 1996
  • In this paper, we present a robust Two Degree of Freedom (TDF) $H_{\infty}$ controllers for a missile system. The feedback controller is designed to meet robust stability and disturbance rejection specifications while the prefilter is used to improve the robust model matching properties of the closed loop system. As the perturbed model, we use the normalized coprim factor perturbations. These controllers are designed using $H_{\infty}$ optimization procedures, and applied to a missile model via simulation.

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