• 제목/요약/키워드: Pitch Controller

검색결과 218건 처리시간 0.032초

개별 블레이드 피치 제어 방식을 이용한 수직축 풍력발전기의 성능 해석 및 시스템 구현 (Aerodynamic Analysis and System Implementation of Vertical Axis Wind Turbine using Individual Blade Pitch Control Method)

  • 정인오;이윤한;황인성;김승조
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2007년도 춘계학술대회B
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    • pp.3347-3352
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    • 2007
  • This paper describes a research for the performance improvement of the straight-bladed vertical axis wind turbine. To improve the performance of VAWT, the individual blade pitch control method is adopted. For the wind turbine, CFD analysis is carried out by changing blade pitch angle according to the change of wind speed and wind direction. By this method, capacity and power efficiency of VAWT are obtained according to the wind speed and rotating of rotor, and could predict the overall performance of VAWT. It was manufactured to verify performance of the experimental system that consists of rotor including four blades and base. Furthermore, torque sensor and power generator were installed. Also, active controller which can change the pitch angle of the individual blade according to the wind speed and direction was used.

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풍력발전시스템 속도제어의 실험적 고찰 (Investigation of a Speed Control for a Wind Turbin Systsem)

  • 임종환;최민호;허종철;김건훈
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 2000년도 제15차 학술회의논문집
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    • pp.36-36
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    • 2000
  • The paper presents a speed control algorithm for a full pitch-controlled wind turbine system. Torque of a blade generated by wind energy is non-linear function of a wind speed, angular velocity, and pitch angle of the blade. The design of a cor_troller, in general, is performed by linearizing the torque in the vicinity of a operating point assuming the angular velocity of the blade is constant. For speed control, however, the angular velocity is no longer a constant, so that linearization of the torque in terms of a wind speed and pitch angle is impossible. In this study, a reference pitch model is derived in terms of a wind speed, angular velocity, and pitch angle, which makes it possible to design a controller without linearizing the non-linear torque model of the blade. The validity of the algorithm is demonstrated with the results produced through sets of experiments.

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라틴 하이퍼큐브 기반 신경망모델을 적용한 풍력발전기 피치제어기 최적화 (Optimization of Wind Turbine Pitch Controller by Neural Network Model Based on Latin Hypercube)

  • 이광기;한승호
    • 대한기계학회논문집A
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    • 제36권9호
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    • pp.1065-1071
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    • 2012
  • 풍력발전기의 안정적인 전력생산은 정격풍속 이상에서 피치제어와 스톨제어와 같은 일정속도제어로 이루어지고 있다. 최근, 효율적인 전력생산을 위하여 정격풍속 이하의 변동풍속 조건에서 최대 출력을 얻기 위한 가변 속도제어가 적용되고 있는 추세이다. 기존의 피치제어기에서는 지글러-니콜스 계단응답법에 의한 제어기 최적화가 이루어지고 있으나, 가변 속도제어의 요구로 보다 정확한 최적화가 필요하게 되었다. 본 연구에서는 기존의 지글러-니콜스 계단응답법을 개선하기 위하여 라틴 하이퍼큐브 샘플링을 통한 신경망모델을 구축하고, 구축된 PID 제어 계수 신경망모델에 유전자 알고리즘을 적용하여 피치제어기를 최적화하였다. 유전자 알고리즘으로 구한 최적해가 지글러-니콜스 계단응답법의 초기해 보다 평균제곱근 오차가 13.4% 향상되었고, 응답특성을 나타내는 상승속도와 정착시간은 각각 15.8% 및 15.3%으로 개선되었다.

비 모델 외바퀴 로봇의 제어 (Control of a Unicycle Robot using a Non-model based Controller)

  • 안재원;김민규;이장명
    • 제어로봇시스템학회논문지
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    • 제20권5호
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    • pp.537-542
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    • 2014
  • This paper proposes a control system to keep the balance of a unicycle robot. The robot consists of the disk and wheel, for balancing and driving respectively, and the tile angle is measured and used for balancing by the IMU sensor. A PID controller is designed based on a non-model based algorithm to prove that it is possible to control the unicycle robot without any approximated linear system model such as the sliding mode control algorithm. The PID controller has the advantage that it is simple to design the controller and it does not require an unnecessary complex formula. In this paper, assuming that the pitch and roll axis are dynamically decoupled, each of the two controllers are designed separately. A reaction wheel pendulum method is used for the control of the roll axis, that is, for balancing and an inverted pendulum concept is used for the control of the pitch axis. To confirm the performance of the proposed controllers using MATLAB Simulink, the dynamic equations of the robot are derived.

무인잠수정의 적분 상태 궤환 제어기 설계 및 경유점 추적 연구 (A Study on an Integral State Feedback Controller for Way-point Tracking of an AUV)

  • 배설봉;신동협;박상홍;주문갑
    • 제어로봇시스템학회논문지
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    • 제19권8호
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    • pp.661-666
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    • 2013
  • A state feedback controller with integration of output error is proposed for way-point tracking of an AUV (Autonomous Underwater Vehicle). For the steering control on the XY plane, the proposed controller uses three state variables (sway velocity, yaw rate, heading angle) and the integral of the steering error, and for the depth control on the XZ plane, it uses four state variables (pitch rate, depth, pitch angle) and the integral of the depth error. From the simulation using Matlab/Simulink, we verify that the performance of the proposed controller is satisfactory within an error range of 1m from the target way-point for arbitrarily chosen sets of consecutive way-points.

시뮬레이터를 이용한 가변속 풍력발전기 제어시스템 검증 (Verification of The Variable-Speed Wind Turbine Control System by Using the Simulator)

  • 차삼곤;한상열;차종환;최원호;이승구
    • 한국신재생에너지학회:학술대회논문집
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    • 한국신재생에너지학회 2007년도 춘계학술대회
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    • pp.370-373
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    • 2007
  • For the development of wind turbine, generally simulator is used. Simulator include wind turbine components. e.g blades, pitch and pitching method, rotor, yaw system, tower, drive train and so on. Few the more, it include a external circumstance. e.g wind speed, wind direction, air density. these basic parameters be used for the control of wind turbine by wind turbine controller in wind turbine simulator. The wind turbine controller can be designed in the wind turbine simulator. But a developer must make the real control system that will be made using PLC or PC or other processor. The developer must verify the function of control system. that is control algorithm , I/O function, communication, sequence and so on. This verification is possible if we substitute the real wind turbine control system for wind turbine controller in the simulator.

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이중 프로세서를 이용한 고장허용 제어기의 설계 및 실현 (Design and implementation of fault tolerant controller using duplex processors)

  • 최성규;홍일선;권오규
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 1993년도 한국자동제어학술회의논문집(국내학술편); Seoul National University, Seoul; 20-22 Oct. 1993
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    • pp.239-243
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    • 1993
  • In this paper, a fault-tolerant controller using duplex processors has been designed and implemented. The PI controller is adopted as the control algorithm and the fault-tolerant control system is implemented by two single chip processors(MCS-96). Performances of the control system designed here have been shown via a simulation with application to a pitch channel autopilot.

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과학로켓 탑재부 자세제어를 위한 펄스 진폭 변조 제어기 설계 (Design of Pulse Amplitude Modulation Controller for the Attitude Control of the Payload of a Sounding Rocket)

  • 공현철;전상운
    • 제어로봇시스템학회논문지
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    • 제6권11호
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    • pp.981-986
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    • 2000
  • A pulse amplitude modulation(PAM) controller is designed for the 3 axis attitude control of a sounding rocket. a certain number of fixed level of thrust are used for the pulse amplitude modulation and the nonlinearity of the controller is considered to examine the existence of the limit cycles and the stability analysis is carried out with the aid of Nyquist plot.

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예측 제어기를 이용한 2바퀴 로봇의 실시간 균형제어 (Real Time Balancing Control of 2 Wheel Robot Using a Predictive Controller)

  • 강진구
    • 한국컴퓨터정보학회논문지
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    • 제19권3호
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    • pp.11-16
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    • 2014
  • 본 논문은 예측제어기를 이용하여 2휠 로봇의 실시간 균형을 유지할 수 있는 자세 제어에 대해 연구하였다. 또한 역방향 진자 제어는 로봇이 진행하는 동안 균형을 유지하기 위하여 도입되었다. 본 논문에서 구현에 사용한 프로세서는 dsPIC30F4013 임베디드 프로세서이며 자체 균형 알고리즘을 설계하고 구현 하는 것이다. 본 연구에서 ARS는 2축의 자이로 각(roll, pitch)과 3축의 가속도계 값(x, y, z)값으로 자세를 계산하도록 하였다. 따라서 본 연구에서는 외란에 대한 자세의 불균형을 극복하기 위한 예측제어기를 제안했으며 이를 원격 시스템의 제어문제에 도입하여 2바퀴 로봇의 선형 제어기와 예측제어기를 결합한 시스템의 시뮬레이션을 수행하였다. 또한 강인한 특성을 실현하기 위해 목표 필터루프를 설계하고 강인도-안정성을 만족하는 제어기를 설계하므로 제어시스템의 안정성을 향상시키고 시스템의 성능의 저하를 최소화함을 확인하였다.

초기 추력편향제어를 위한 자세각제어 구조에 대한 연구 (A Research of Attitude Angle Control Structure for Thrust Vector Control of Missiles at Initial Boosting Phase)

  • 김부민;황익호
    • 전기학회논문지
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    • 제66권10호
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    • pp.1523-1531
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    • 2017
  • In general, the thrust vector control should be fast and stable in the initial launch phase. Two types of conventional controllers, one is for pitch angle control and the other is for pitch rate control, are designed based on the equation of motion without aerodynamics and are compared in the viewpoints of the stability margin and the time response performance. Also analyzed are the rejection capabilities to cope with high aerodynamic disturbances caused by high angle of attacks in initial booting phase. Additionally, time response features at actuator saturation are investigated. Based on those results, we suggest a controller structure which is more suitable for thrust vector control of missiles at initial booting phase.