• 제목/요약/키워드: Yaw rate

검색결과 192건 처리시간 0.025초

4MW급 풍력발전기용 요 감속기 설계 (Yaw Gearbox Design for 4MW Class Wind Turbine)

  • 이형우;김인환;이재신
    • 융합정보논문지
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    • 제12권2호
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    • pp.142-148
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    • 2022
  • 본 논문은 풍력발전기용 요 감속기를 경량화하여 유한요소해석과 위험속도해석을 통해 안정성검증을 하였다. 제품의 경량화는 엔진의 효율을 높일 수 있으며, 부품의 소재를 절약하여 경제적 이득을 취할 수 있다. IEC 61400-1에서 제시한 풍력발전기 부품의 안전율 1.3이상을 목표로 풍력발전기용 요 감속기를 경량화하였다. 위상 최적화를 수행한 캐리어를 유한요소해석을 수행하여 안전율을 나타냈고, 하우징과 최적화한 캐리어를 MASTA11을 활용하여 작성한 풍력발전용 요 감속기 기어트레인 모델과 부분구조합성법으로 연결하여 고유 모드와 고유진 동수를 파악하여 질량불평형과 치통과 주파수에 대하여 위험속도해석을 수행하였고, 캠벨 선도(Campbell Diagram)를 작성하여 안정성 검증을 하였다.

ROLLOVER INDEX-BASED ROLLOVER MITIGATION CONTROL SYSTEM

  • Yoon, J.;Yi, K.;Kim, D.
    • International Journal of Automotive Technology
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    • 제7권7호
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    • pp.821-826
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    • 2006
  • This paper describes a rollover index (RI)-based rollover mitigation control (RMC) system. A rollover index which indicates an impending rollover has been developed by a roll dynamics phase plane analysis. The rollover index is calculated using the roll angle, the roll rate, the lateral acceleration and time to wheel lift (TTWL). A differential braking control law based on a 2-D bicycle model has been designed using the direct yaw control (DYC) method. An RMC threshold has been determined from the rollover index. The performance of the RMC scheme and the effectiveness of the proposed rollover index are illustrated using a vehicle simulator.

무궁화 방송통신 위성의 3축 자세 안정화 장치에 관한 연구 (A study on the 3-axis attitude stabilization of Koreasat)

  • 진익민;백명진;김진철
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 1993년도 한국자동제어학술회의논문집(국내학술편); Seoul National University, Seoul; 20-22 Oct. 1993
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    • pp.793-798
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    • 1993
  • In this study the attitude control of the KOREASAT is investigated. The KOREASAT is a geostationary satellite and its 3 attitude angles, namely, roll, pitch and yaw angles, are stabilized by using the 3-axis stabilization technique. In the pitch control loop, the pitch attitude angle received from the earth sensor is processed in the attitude processing electronics by using PI type control logic, and the control command is sent to the momentum wheel assembly to generate the control torque by varying the wheel rate. The roll/yaw attitude control is performed by activating a magnetic torquer or by firing appropriate thrusters. The magnetic torquer interacts with the earth magnetic field to produce the control torque, and the thrusters are used to control the larger roll attitude errors. In this study dynamic modelling of the satellite is performed. And the earth sensor, the momentum wheel, and the magnetic torquer are mathematically modelled. The 3-axis attitude control logic is implemented to make the closed-loop system and simulations are carried out to verify the implemented control laws.

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신경망을 이용한 엔진/브레이크 통합 VDC 시스템에 관한 연구 (A Study on the Engine/Brake integrated VDC System using Neural Network)

  • 지강훈;정광영;김성관
    • 제어로봇시스템학회논문지
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    • 제13권5호
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    • pp.414-421
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    • 2007
  • This paper presents a engine/brake integrated VDC(Vehicle Dynamic Control) system using neural network algorithm methods for wheel slip and yaw rate control. For stable performance of vehicle, not only is the lateral motion control(wheel slip control) important but the yaw motion control of the vehicle is crucial. The proposed NNPI(Neural Network Proportional-Integral) controller operates at throttle angle to improve the performance of wheel slip. Also, the suggested NNPID controller performs at brake system to improve steering performance. The proposed controller consists of multi-hidden layer neural network structure and PID control strategy for self-learning of gain scheduling. Computer Simulation have been performed to verify the proposed neural network based control scheme of 17 dof vehicle dynamic model which is implemented in MATLAB Simulink.

Stabilization Loop Design Method on Dynamic Platform

  • Kwon, Young-Shin;Kim, Doh-Hyun;Kim, Lee-Han;Hwang, Hong-Yeon
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 2001년도 ICCAS
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    • pp.156.5-156
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    • 2001
  • Stabilized tracking platform in a missile consisting of a flat planar antenna, pitch/yaw gimbals, gear trains, and current controlled DC drive motors for pitch and yaw gimbal must have a capability to track a target as an inertial sensor in the presence of missile body motion such as maneuvering and vibration. Because of this reason, tracking a target from dynamic platform requires a servo architecture that includes a outer tracking loop(position loop) and inner rate loop that stabilizes the line of sight(LOS). This paper presents a gimbaled platform model including nonlinear phenomena due to viscous and Coulomb friction based on experimental data and torque equilibrium equation, the design concept for the inner tacholoop having P controller structure ...

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Writer Identification using Wii Remote Controller

  • Watanabe, Takashi;Shin, Jung-Pil;Chong, Ui-Pil
    • 융합신호처리학회논문지
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    • 제14권1호
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    • pp.21-26
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    • 2013
  • The objective of this study was to develop a system for handwriting recognition in three dimensions (3D) to authenticate users. While previous studies have used a stylus pen for two-dimensional input on a tablet, this study uses the Wii Remote controller because it can capture 3D human motion and could therefore be more effective means of recognition. The information obtained from a Wii Remote controller included x and y coordinates, acceleration (x, y, z), angular velocity (pitch, yaw, roll), twelve input buttons, and time. The proposed system calculates distances using six features extracted after preprocessing the data. In an experiment where 15 subjects wrote "AIZU" 10 times, we obtained a 94.8% identification rate using a combination of writing velocity, the peak value of pitch, and the peak value of yaw. This suggests that this system holds promise for handwriting-based authentication in the future.

선수동요 동유체마력 추정을 위한 시운전 (A Study on Sea Trial Test Scenario for Estimation of Hydrodynamic Rotary Derivatives)

  • 윤현규
    • 대한조선학회논문집
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    • 제43권1호
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    • pp.50-58
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    • 2006
  • Free running model tests gives us only maneuvering indices not hydrodynamic derivatives. For this reason, system identification method has been applied to the measured data to identify mathematical model describing hydrodynamic force. However It is difficult to obtain complete set of maneuvering derivatives because of strong correlation of sway velocity and yaw rate. Therefore, in this paper, we assumed that sway velocity related coefficients would be obtained by oblique towing test. and then proposed new procedure to estimate yaw related coefficients. To do this, correlation and regression analyses were carried out to establish modified model and estimate maneuvering derivatives. Also D-optimal rudder input scenario was found based on the modified model and confirmed the validity of its sufficient richness as a input scenario.

현가장치의 유연성과 차체의 탄성효과가 조종안정성에 미치는 영향 분석 (Effects of Suspension Compliance and Chassis Flexibility in Handling Performance)

  • 강동권;유완석
    • 한국정밀공학회지
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    • 제14권7호
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    • pp.137-143
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    • 1997
  • In this study, handling simulation of a passenger car is carried out to see the effects of suspension compliance, roll stabilizef bar and chassis flexibility. The front suspension of the car is a MacPherson strut type and the rear suspension is a multi-link type. The following five DADS models are constructed and compared to verify the effects of suspension compliance and chassis flexibility during lane change. (1) Vdhicle model without hard point compliance and stabilizer, (2) Vehicle model with hard point compoiance, (3) Vehicle model with hard point compliance and stabilizer, (4) Vehicle model with hard point compoiance, stabilizer, and one vibration mode of the chaxxis. (5) Vehicle model with hard point compliance, stabilizer, and three vibration modes of the chassis. The result shows that hard point compliance and stabilizer are significant in roll angle, and the flexibility of the chassis affects the yaw angle and yaw rate.

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대형 트럭의 선회 주행특성 해석을 위한 컴퓨터 모델의 개발 (Development of a Computer Model for the Turning Maneuver Analysis of a Heavy Truck)

  • 문일동;권혁조;오재윤
    • 한국자동차공학회논문집
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    • 제8권4호
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    • pp.121-129
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    • 2000
  • this paper develops a computational model for the turning maneuver analysis of a cabover type heavy truck. The model having 42 degree-of-freedom is developed using ADAMS. Leaf springs used in the front and rear suspension systems are modeled by dividing it three links and joining them with joints. Force and displacement relationship showing nonlinear hysteric characteristics of the leaf spring is measured and modeled with an exponential function. A velocity and force relationship of a shock absorber is measured and modeled with a spline function. And a stabilizer bar is modeled using ADAMS beam element to consider a twisting and bending effect. To verify the developed model an actual vehicle test is performed in the double lane change course with 50kph and 60kph vehicle velocity. In the actual vehicle test lateral acceleration roll angle and yaw rate are measured, The tendency and peak-to-peak values of the actual vehicle test and simultion results are compared each other.

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프레임을 유연체로 고려한 대형트럭 컴퓨터 모델의 개발 (Development of a Computer Model of a Large-sized Truck Considering the Frame as a Flexible Body)

  • 문일동;오재윤
    • 한국자동차공학회논문집
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    • 제11권6호
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    • pp.197-204
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    • 2003
  • This paper develops a computer model for estimating the handling of a cabover type large-sized truck. The truck is composed of front and rear suspension systems, a frame, a cab, and ten tires. The computer model is developed using ADAMS. A shock absorber, a rubber bush, and a leaf spring aunt a lot on the dynamic characteristic of the vehicle. Their stiffness and damping coefficient are measured and used as input data of the computer model. Leaf springs in the front and rear suspension systems are modeled by dividing them three links and joining them with joints. To improve the reliability of the developed computer model, the frame is considered as a flexible body. Thus, the frame is modeled by finite elements using MSC/PATRAN. A mode analysis is performed with the frame model using MSC/NASTRAN in order to link the frame model to the computer model. To verify the reliability of the developed computer model, a double lane change test is performed with an actual vehicle. In the double lane change, lateral acceleration, yaw rate, and roll angle are measured. Those test results are compared with the simulation results.