• 제목/요약/키워드: Open-loop Control

검색결과 459건 처리시간 0.046초

터보펌프-가스발생기 개회로 연계시험 연구 (Study on Turbopump-Gas Generator Open-Loop Coupled Test)

  • 김승한;남창호;김철웅;문윤완;설우석
    • 대한기계학회논문집B
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    • 제34권5호
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    • pp.563-568
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    • 2010
  • 30톤급 액체산소/케로신 액체로켓엔진개발의 중간단계로 터보펌프-가스발생기 개회로 연계시험이 수행되었다. 터보펌프-가스발생기 개회로 연계시험은 엔진시스템 작동 모사 환경 시험으로서 가스발생기로의 추진제는 터보펌프 출구를 통해 공급되지만, 가스발생기 출구 가스는 터빈 구동에 이용되지 않고 외부로 배출된다. 터보펌프-가스발생기 개회로 연계시험 목적, 시험설비 구성, 제어시스템의 작동 조건, 시험 수행 절차, 연계시험기의 구성 형태, 개회로 연계시험 결과가 제시되었다. 터보펌프-가스발생기 개회로 연계시험 결과, 연계시험기의 예냉 절차와 시동 특성, 정격 작동성 및 안정적인 종료 특성이 액체로켓 엔진시스템 작동 환경 모사 조건에서 확인되었다.

HDD 스핀들 모터의 초기 구동 제어에 관한 연구 (A Study on the Start-up Control for HDD Spindle Motors)

  • 정준
    • 한국소음진동공학회논문집
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    • 제18권10호
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    • pp.1065-1072
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    • 2008
  • A HDD adopts a sensorless brushless DC (BLDC) motor as a spindle motor. Because there is no direct sensor measuring rotor position. open loop commutations with inductive sensing are used to increase the rotor speed up to a certain speed where the zero crossings of the back electromotive force (EMF) voltage are measurable. Therefore, successful open loop commutations are necessary for the stable start-up control of the spindle motors. In this paper, the time scale and the number of the open loop commutations are employed for design parameters to guarantee robustness to torque constant variation and initial rotor position. The design results are verified by experiments on a very low current start-up of the spindle motor with various environment. The experimental results show that the design results can decrease the start-up failure rate considerably.

역최적 문제를 통한 충돌각 제어 최적유도법칙의 개루프 비행궤적 특성 및 Time-to-go 예측 (The Characteristics of Open-loop Trajectory and Time-to-go Estimation for Impact Angle Control Optimal Guidance through Inverse Optimal Problem)

  • 이용인;이진익
    • 한국군사과학기술학회지
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    • 제11권3호
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    • pp.5-12
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    • 2008
  • This paper presents the features of an impact angle constrained open-loop optimal trajectory which is given by a function of initial conditions and optimal guidance gains. Using missile motion described by linearized kinematic equations and a proper form of performance index, an inverse optimal problem is suggested to investigate the gains related to the performance index. The flight trajectory and time-to-go can be shaped in terms of the optimal guidance gains. The results are evaluated by 3-DOF simulation.

냉각수 순환 형태의 파이프 쿨링 공법을 이용한 매스콘크리트 수화열 제어 (Hydartion Heat Control with Closed Loop Pipe Cooling System)

  • 박찬규;손상현;이승훈;장기욱;정재홍;김명식
    • 한국콘크리트학회:학술대회논문집
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    • 한국콘크리트학회 2001년도 가을 학술발표회 논문집
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    • pp.403-408
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    • 2001
  • In order to control hydration heat in mass concrete, pipe cooling method has been widely used. However, open pipe cooling system cannot be applied to the mass concrete structures when cooling water supply is difficult. To control hydration heat of high strength mass foundation, closed loop pipe cooling system was developed to solve the cooling water supply. This paper reports the performance result of hydration heat control with closed loop pipe cooling system.

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도립진자 시스템의 $H_{\infty}$ 제어기 설계 (Design of $H_{\infty}$Controller for the inverted pendulum system)

  • 서강면;강문성
    • 한국정보통신학회논문지
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    • 제10권10호
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    • pp.1796-1803
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    • 2006
  • 본 연구에서는 비선형성이 강한 대표적인 불안정한 시스템으로 새로운 제어 이론의 유효성을 실증하고 평가하기에 적합한 도립 진자 시스템의 강인 안정 및 강인 제어 성능을 확보하기 위하여 $H_{\infty}$ 제어 이론을 도입하여 최적 제어기를 설계하였다. 그리고, 저역통과 필터를 제어 대상 시스템과 종속으로 결합시켜 개루프 전달함수의 형성(loop shaping)을 시도함으로서, 감도함수 및 상보감도함수가 바람직 한 주파수 특성을 갖도록 하였다. 먼저, 설계한 $H_{\infty}$제어기를 도립진자 제어시스템에 적용하여 시뮬레이션 하였고, 그 결과를 전통적인 기법으로 산업현장에서 널리 사용하고 있는 PID제어기를 채용한 시스템의 출력과 비교하여 그 가능성을 확인하였다. 그런 다음, 설계 한 제어기를 실제 시스템에 적용하여 실험하였다. 시뮬레이션 및 실험 결과를 통해, $H_{\infty}$ 제어기는 모델링 오차, 외란 및 노이즈의 영향을 줄이면서 제어목표를 잘 추종하는 것으로 나타나 안정도 및 제어성능이 우수함을 확인할 수 있었다.

가변 이득을 가지는 단상 PFC 디지털 제어기 (The Digital Controller of the Single-Phas Power Factor Correction(PFC) having the Variable Gain)

  • 정창용
    • 전력전자학회:학술대회논문집
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    • 전력전자학회 2000년도 전력전자학술대회 논문집
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    • pp.163-167
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    • 2000
  • This paper presents the digital control of single-phase power factor correction(PFC) converter which has the variable gain according to the condition of inner control loop error. Generally the gain of inner current control loop in single-stage PFC converter has a constant magnitude. This has a bad influence on the power factor because current loop doesn't operate smoothly in the condition that input voltage is low In particular a digital controller has more time delay than an analog controller and degrades This drops the phase margin of the total digital PFC system,. It causes the problem that the gain of current control loop isn't increased enough. In addition the oscillation happens in the peak value of the input voltage open loop PFC system gain changes according to ac input voltage. These aspects make the design of the digital PFC controller difficult The digital PFC controller presented in this paper has a variable gain of current control loop according to input voltage. The 1kW converter was used to verify the efficiency of the digital PFC controller.

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Development, Implementation and Experimentation on a dSPACE DS1104 of a Direct Voltage Control Scheme

  • Hmidet, Ali;Dhifaoui, Rachid;Hasnaoui, Othman
    • Journal of Power Electronics
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    • 제10권5호
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    • pp.468-476
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    • 2010
  • This paper proposes and develops a new direct voltage control (DVC) approach. This method is designed to be applied in various applications for AC drives fed with a three-phase voltage source inverter (VSI) working with a constant switching time interval as in the standard direct torque control (DTC) scheme. Based on a very strong min(max) criterion dedicated to selecting the inverter voltage vector, the developed DVC scheme allows the generation of accurate voltage forms of waves. The DVC algorithm is implemented on a dSPACE DS1104 controller board and then compared with the space vector pulse width modulation technique (SVPWM) in an open loop AC drive circuit. To demonstrate the efficiency of the developed algorithm in real time and in closed loop AC drive applications, a scalar control scheme for induction motors is successfully implemented and experimentally studied. Practical results prove the excellent performance of the proposed control approach.

모멘트쌍 액추에이터가 적용된 PPF에 의한 평판의 능동진동제어 (Positive Position Feedback Control of Plate Vibrations Using Moment Pair Actuators)

  • 신창주;홍진숙;정의봉;유호영
    • 한국소음진동공학회논문집
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    • 제22권4호
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    • pp.383-392
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    • 2012
  • This paper reports the active vibration control of plates using a positive position feedback(PPF) controller with moment pair actuators. The equations of motion of the plates under a force and moment pairs are derived and the equations of PPF controllers are formulated. The numerical active control system is then achieved. The effect of the parameters - gain and damping ratio - of the PPF controllers on the open loop transfer function was investigated mainly in terms of the system stability. Increasing the gain of the PPF controller tuned at a mode, the magnitude of the open loop transfer function is increased at all frequencies without changing the phase behavior. The increase of the damping ratio of the PPF controller leads to decrease the magnitude of the open loop transfer function and to modify its phase characteristics, ie, system stability. Based on the behavior of the gain and the damping ratio of the controller, PPF controller for reduction of the plate vibration can be achieved. Two PPF controllers are designed with their connection in parallel to control the two modes simultaneously. Each PPF controller is tuned at the $1^{st}$ and $2^{nd}$ modes, respectively. Their parameters were determined to remain the system to be stable based on the results of the parametric study. A significant reduction in vibration at the tuned modes can be obtained.

고기동 유도탄 HILS를 위한 비행자세모의기 최적 경로 산출 (Optimal Path Generation of Flight Motion Simulator for Hardware in the Loop Simulation)

  • 김기승;나원상
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 2004년도 하계학술대회 논문집 A
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    • pp.117-119
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    • 2004
  • An optimal flight motion simulator path generation method is proposed for hardware in the loop simulation of high maneuverable missile. The proposed method consists of open loop and closed loop path calculation algorithm based on the energy optimal control strategies. The optimal angle command is able to protect the simulator from high acceleration shock at initial control phase.

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슬라이딩모드를 이용한 자동변속기의 비선형제어 (Nonlinear Control of an Automatic Transmission Using Sliding Mode)

  • 조승호
    • 대한기계학회논문집
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    • 제19권3호
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    • pp.605-614
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    • 1995
  • In the automatic transmission using planetary gear there exists nonlinearities due to the finite difference between gear ratios, which yield torque hole during shift and influence on the ride quality and life of clutch. Based on the reaction carrier and converter turbine speed sliding functions are defined. Nonlinear closed-loop control laws are derived using them. Computer simulation shows that the closed loop design is better than the open loop design and semi-closed loop design.