• Title/Summary/Keyword: 피치 제어

Search Result 220, Processing Time 0.035 seconds

Passive Maglev Carrier Control with Consideration of Pitch Motion (피치 운동을 고려한 자기부상 수동형 이송자 제어)

  • Lee, Younghak;Kim, Chang-Hyun;Ha, Chang-Wan;Park, Doh-Young;Yang, Seok-Jo;Lim, Jaewon
    • Transactions of the Korean Society of Mechanical Engineers A
    • /
    • v.40 no.2
    • /
    • pp.213-220
    • /
    • 2016
  • This research aims to develop core technologies for passive carrier (no power in carrier itself) transfer system. The technologies are passive levitation, propulsion, and guidance, which can be great benefits for semiconductor and display manufacturing industries. Passive maglev carrier is necessary to precise position control for quiet and stable transfer operation. However, the structural characteristics of carrier and the installation errors of gap sensors cause the pitch motion. Hence, the controller design in consideration of pitch motion is required. This study deals with the reduction control of carrier pitch motion. PDA controller and PDA controller with pitch control are proposed to compare the pitch angle analysis. The pitch angle and the levitation precision are measured by experiment. Finally, the optimized design of pitch controller is presented and the effects are discussed.

Pitch-axis Maneuver of UAVs by Adaptive Control Approach (무인항공기의 적응제어 법칙을 이용한 피치 기동 연구)

  • Bang, Hyo-Choong
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.38 no.12
    • /
    • pp.1170-1176
    • /
    • 2010
  • This study addresses adaptive control of UAVs(Unmanned Aerial Vehicles) pitch-axis maneuver. The MRAC(Model Referenced Adaptive Control) approach is employed to accommodate uncertainties which are introduced by feedback linearization of pitch attitude control by elevator input. The model uncertainty is handled by adaptation laws which update model parameters while the UAV is under control by the feedback control law. Steady-state pitch attitude achieved by the stabilizing control law is derived to provide insight on the closed-loop behavior of the controlled system. The proposed idea is free of linearization, gain-scheduling procedures, so that one can design high maneuverability of UAVs for pitching motion in the presence of significant model uncertainty.

Dynamic Stability Analysis of Wind Turbines Considering Periodic Blade Pitch Actions (블레이드의 주기적 피치운동을 고려한 풍력 터빈의 동적 안정성 해석)

  • Kim, Kyungtaek;Lee, Chongwon
    • 한국신재생에너지학회:학술대회논문집
    • /
    • 2010.11a
    • /
    • pp.186-186
    • /
    • 2010
  • 개별 블레이드 피치 제어(individual blade pitch control)는 각각의 로터 블레이드의 피치각을 독립적으로 조정함으로써 블레이드에 작용하는 공력을 변화시키는 원리로 풍력 터빈 구조물에 발생하는 동적 피로하중을 저감시키기 위한 제어기법이다. 그러나 개별 피치 제어에 의해 발생하는 각 블레이드의 독립적인 피치 운동은 풍력 터빈 회전자에 비대칭성을 야기하고 구조물의 동적 불안정 현상을 발생시킬 수 있기 때문에 이에 대한 정확한 동적 해석이 선행되어야 한다. 하지만 블레이드의 피치 운동이 반영된 풍력 터빈은 시변계로 간주되어 기존의 시불변계 해석기법을 직접 적용할 수 없기 때문에 동적 해석에 어려움이 있다. 이 논문에서는 각각의 블레이드 피치운동을 주기함수로 근사화 함으로써 풍력 터빈을 주기 시변계로 모형화한다. 그리고 효율적으로 주기 시변계의 근사해를 구하기 위한 변조 좌표 변환(modulated coordinate transformation)기법을 적용하여 블레이드의 피치운동이 반영된 풍력 터빈의 동적 안정성 해석을 수행하였다. 그리고 현재 풍력 터빈의 동적 해석에 활용되는 대표적인 해석 기법인 다중 블레이드 좌표변환(multi-blade coordinate transformation)기법을 이용한 해석보다 정확한 결과를 얻을 수 있음을 보였다.

  • PDF

Optimal Aerodynamic Design and Performance Analysis for Pitch-Controlled HAWT (가변 피치형 수평축 풍력 터빈의 공력 최적설계 및 피치제어 성능 연구)

  • Ryu, Ki-Wahn
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.35 no.10
    • /
    • pp.891-898
    • /
    • 2007
  • Optimal aerodynamic design for the pitch-controlled horizontal axis wind turbine and its aerodynamic performance for various pitch angles are performed numerically by using the blade element momentum theory. The numerical calculation includes effects such as Prandtl‘s tip loss, airfoil distribution, and wake rotation. Six different airfoils are distributed along the blade span, and the special airfoil i.e. airfoil of 40% thickness ratio is adopted at the hub side to have structural integrity. The nonlinear chord obtained from the optimal design procedure is linearized to decrease the weight and to increase the productivity with very little change of the aerodynamic performance. From the comparisons of the power, thrust, and torque coefficients with corresponding values of different pitch angles, the aerodynamic performance shows delicate changes for just $3^{\circ}$ increase or decrease of the pitch angle. For precisive pitch control, it requires the pitch control algorithm and its drive mechanism below $3^{\circ}$ increment of pitch angle. The maximum torque is generated when the speed ratio is smaller than the designed one.

Pitch-based Intensity Control Models Considering Phonetic Environments (음운환경을 고려한 피치 기반 세기 제어 모델)

  • 김기중;김진영;진달복
    • The Journal of the Acoustical Society of Korea
    • /
    • v.17 no.1
    • /
    • pp.80-85
    • /
    • 1998
  • 본 논문에서는 음성합성기에서 합성음의 자연성을 향상시키기 위한 한 방법으로 운 율 제어요소중 세기 제어 모델을 통계적인 방법을 이용하여 제안하였다. 세기 제어 모델을 구성하기 위하여, 음성의 세기는 피치에 비례한다는 사실에 기반하여, 녹음된 음성 데이터에 서 음절의 각 모음에 대한 평균파워와 평균피치를 구하고, 피치를 종속변수로 하는 모음의 세기 예측식을 만들었다. 예측식에 의하여 얻어진 세기값과 실제 측정된 세기값과의 상관도 는 전체모음에 대하여 약 0.63으로 나타났다. 본 논문에서는 예측 세기와 실제 세기와의 상 관도를 향상시키기 위하여 피치만을 고려하여 예측된 세기값을 음운환경을 고려하여 선형 오차를 보정하는 방법을 제안하였고, 이 방법을 이용하여 얻어진 세기값은 전체모음에 대하 여 실제 세기값과 0.71의 상관도로 향상시킬 수 있었다.

  • PDF

A Study on the Wind Turbine Blade Optimization and Pitch Control Using the Hybrid Genetic Algorithm (혼합형 유전 알고리즘을 이용한 풍력발전기용 블레이드 최적설계 및 피치제어에 관한 연구)

  • Kang, Shin-Jae;Kim, Ki-Wan;Ryu, Ki-Wahn;Song, Ki-Jung
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.30 no.6
    • /
    • pp.7-13
    • /
    • 2002
  • This paper introduced a new hybrid genetic algorithm, verified its performance, and applied it to the optimization of blade design and pitch control for 30kW pitch-controlled variable-speed horizontal-axis wind turbine system to determine the optimum blade chord and twist distributions that maximize the energy production for a given Weibull wind distribution and the optimum blade pitch angles that maintain constant power output.

Aerodynamic Characteristics of Several Airfoils for Design of Passive Pitch Control Module of 10 kW Class (10kW 급 풍력 블레이드의 수동형 피치제어 모듈의 설계를 위한 여러가지 익형의 공력 특성에 관한 연구)

  • Kang, Sang Kyun;Lee, Ji Hyun;Lee, Jang-Ho
    • Transactions of the Korean Society of Mechanical Engineers A
    • /
    • v.38 no.6
    • /
    • pp.609-617
    • /
    • 2014
  • Even though the variable pitch control of a wind turbine blade is known as an effective component for power control over the rated wind speed, it has limited applicability to small wind turbines because of its relatively high cost on the price of small wind turbine. Instead, stall control is generally applied in the blade design without any additional cost. However, stall delay can frequently be caused by high turbulence around the turbine blade, and it can produce control failures through excessive rotational speed and overpowering the electrical generator. Therefore, a passive pitch control module should be considered, where the pitch moves with the aerodynamic forces of the blade and returns by the elastic restoring force. In this study, a method to calculate the pitch moment, torque, and thrust based on the lift and drag of the rotating blade wing was demonstrated, and several effective wing shapes were reviewed based on these forces. Their characteristics will be estimated with variable wind speed and be utilized as basic data for the design of the passive pitch control module.

Power Control of Variable and Constant Speed Wind Power System (가변속과 일정속 풍력발전시스템의 출력제어)

  • 김철호;공정식;오철수
    • Journal of Energy Engineering
    • /
    • v.9 no.2
    • /
    • pp.117-122
    • /
    • 2000
  • 풍력발전시스템은 일정속과 가변속 풍력발전시스템으로 나누어진다. 일정속 풍력발전시스템은 유도발전기를 이용한 시스템이 주종을 이루고, 가변속 풍력발전시스템은 동기발전기-인버터로 이루어진다. 본 논문에서는 피치컨트롤이 장착된 두 시스템을 분석하여, 피치컨트롤의 제어 알고리즘을 유도하고 공기역학적 출력제어 국면에서 두 시스템의 출력제어를 비교 분석하고자 한다.

  • PDF

Roll/Yaw Momentum Management Method of Pitch Momentum Biased Spacecraft (피치 모멘텀 바이어스 위성시스템의 롤/요축 모멘텀 제어방식)

  • Rhee, Seung-Wu;Ko, Hyun-Chul;Jang, Woo-Young;Son, Jun-Won
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.37 no.7
    • /
    • pp.669-677
    • /
    • 2009
  • In general, the pitch momentum biased system that induces inherently nutational motion in roll/yaw plane, has been adapted for geosynchronous communications satellites. This paper discusses the method of roll attitude control using yaw axis momentum management method for a low earth orbit(LEO) satellite which is a pitch momentum biased system equipped with only two reaction wheels. The robustness of wheel momentum management method with PI-controller is investigated comparing with wheel torque control method. The transfer function of roll/yaw axis momentum management system that is useful for attitude controller design is derived. The disturbance effect of roll/yaw axis momentum management system for attitude control is investigated to identify design parameters such as magnitude of momentum bias and to get the insight for controller design. As an example, the PID controller design result of momentum management system for roll/yaw axis control is provided and the simulation results are presented to provide further physical insight into the momentum management system.

Neural Network Pitch Controller of Wind Turbine using Changing Rate of Generator Speed (발전기 속도 변화율을 이용한 신경망피치제어기)

  • Hong, Min-Ho;Kim, Ho-Chan;Huh, Jong-Chul;Kang, Min-Jae
    • Journal of the Korean Institute of Intelligent Systems
    • /
    • v.24 no.4
    • /
    • pp.366-371
    • /
    • 2014
  • The neural network pitch controller using changing rate of generator speed has been suggested in this paper to regulate wind turbine power above the rated wind speed. The changing rate of generator speed is used in the suggested pitch controller as well as the difference between the rated and current generator speed. Matlab/simulink has been used for simulations and it has been shown that the suggested pitch controller regulates generator speed as the rated speed of 122.9[rad/s].