• 제목/요약/키워드: Yaw Damping

검색결과 31건 처리시간 0.029초

TDC 제어를 이용한 측면슬립 및 댐핑보상 강성제어 (Robust Steering Control with Side Slip and Yaw Damping Compensation Using Time Delay Control)

  • 이선봉;최해운
    • 한국기계가공학회지
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    • 제18권4호
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    • pp.10-15
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    • 2019
  • In this paper, we report a robust steering control using time delay control for the vehicle dynamics variation due to tire/road contact condition variation, the lateral disturbance force due to the side wind, and the yaw disturbance moment due to the difference between the left and right tires' pneumatic pressure. We controlled the side slip and yaw damping compensation for rapid steering at the high velocity of the vehicle. Based on the developed control, the driver can only consider the desired path without concerning on the vehicle dynamics variation, disturbances, and undesired side slip and yaw oscillations. Simulation results show that robustness from the vehicle dynamics variation and disturbances was achieved by using the developed time delay control. We evaluated the side slip and yaw damping compensation capability for the rapid steering at the high velocity of the vehicle in the cases of three control methods.

차량 횡방향 안정성 향상을 위한 통합섀시 제어 (Unified Chassis Control for Improvement of Vehicle Lateral Stability)

  • 조완기;이경수;윤장열
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2007년도 춘계학술대회A
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    • pp.1126-1131
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    • 2007
  • This paper presents unified chassis control (UCC) to improve the vehicle lateral stability. The unified chassis control implies combined control of active front steering (AFS), electronic stability control (ESC) and continuous damping control (CDC). A direct yaw moment controller based on a 2-D bicycle model is designed by using sliding mode control law. A direct roll moment controller based on a 2-D roll model is designed. The computed direct yaw moment and the direct roll moment are generated by AFS, ESP and CDC control modules respectively. A control authority of the AFS and the ESC is determined by tire slip angle. Computer simulation is conducted to evaluate the proposed integrated chassis controller by using the Matlab, simulink and the validated vehicle simulator. From the simulation results, it is shown that the proposed unified chassis control can provide with improved performance over the modular chassis control.

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파랑중 부선의 침로안정성에 관한 연구 (Study on the Course Stability of a Barge in Waves)

  • 이상민
    • 해양환경안전학회지
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    • 제24권4호
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    • pp.430-437
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    • 2018
  • 파랑중을 항행하는 선박에는 저항증가와 함께 파랑에 의한 횡력 및 회두모멘트가 정수중과 다르게 작용하여 선박의 조종성능에 영향을 미치게 된다. 따라서 파랑에 의해 발생하는 횡력 및 회두모멘트를 추정하는 것이 중요하므로 본 연구에서는 이와 같은 문제를 해결할 수 있는 수치계산을 이행하였다. 본 연구에서는 CFD를 이용하여 정수중 및 파랑중에서 부선에 작용하는 유체력 계산을 위한 수치시뮬레이션을 수행하였으며, 이 결과를 토대로 최종적으로 파랑중 부선의 침로안정성 특성에 대하여 조사 및 분석하였다. 정수중보다는 파랑중에서 부선에 작용하는 유체력이 강해지고 있으며, 파랑중에서도 파장이 길어질수록 유체력이 커지고 있는 모습을 확인할 수 있다. 장파장 영역에서는 yaw damping lever의 (-) 값이 정수중보다 커지고 있으나, 단파장 영역과 파장이 선박길이와 일치하는 영역에서는 각각 작아지고 있어서 이 영역에서는 침로안정성이 향상되고 있다고 추정할 수 있다. 즉 장파장 영역에서는 침로안정성이 정수중 및 단파장 영역보다 상대적으로 나빠지고 있으므로 항행시 주의가 필요하다고 할 수 있다.

MR 댐퍼를 이용한 철도 차량 조향 장치의 진동제어 (Vibration Control of Railway Vehicle Steering Mechanism Using Magnetorheological Damper)

  • 하성훈;최승복;유원희
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2007년도 추계학술대회논문집
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    • pp.369-374
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    • 2007
  • This paper presents yaw vibration control performances of railway vehicle featuring controllable magnetorheological damper. A cylindrical type of MR damper is devised and its damping force is evaluated by considering fluid resistance and MR effect. Design parameters are determined to achieve desired damping force level. The MR damper model is then incorporated with the governing equations of motion of the railway vehicle which includes vehicle body, bogie and wheel-set. Subsequently, computer simulation of vibration control via proportional-integral-derivative (PID) controller is performed using Matlab. Various control performances are demonstrated under external excitation by creep force between wheel and rail.

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MR댐퍼를 이용한 철도 차량의 진동제어 및 조향성능 고찰 (Vibration Control and Steering Performance Evaluation of Railway Vehicle Using Magnetorheological Damper)

  • 하성훈;최승복;유원희
    • 한국소음진동공학회논문집
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    • 제18권5호
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    • pp.524-532
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    • 2008
  • This paper presents yaw vibration control performances of railway vehicle featuring controllable magnetorheological damper. A cylindrical type of MR damper is devised and its damping force is evaluated by considering fluid resistance and MR effect. Design parameters are determined to achieve desired damping force level. The MR damper model is then incorporated with the governing equations of motion of the railway vehicle which includes vehicle body, bogie and wheel-set. Subsequently, computer simulation of vibration control via proportional-integral-derivative(PID) controller is performed using Matlab. Various control performances are demonstrated under external excitation by creep force between wheel and rail.

Effect of the Turret's Rotational Damping on the Heading Stability of a Turret-Moored FPSO

  • Min, Soo Young;Park, Sung Boo;Shin, Seong Yun;Shin, Da Gyun;Jung, Kwang Hyo;Lee, Jaeyong;Lee, Seung Jae;Han, Solyoung;Chun, Yun Suk
    • 한국해양공학회지
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    • 제34권5호
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    • pp.304-315
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    • 2020
  • The main features of offshore turret platforms are station-keeping and weathervaning functions. Due to the complexity of the yaw motion, abundant research is being done to verify the factors that affect the heading stability. Simulations are used for studies that are not possible with experiments, but the conditions must be verified using experimental results. This study presents methods to estimate turret-related parameters such as the rotational stiffness and rotational damping. A time series analysis was performed, and the results showed that the calculation using the obtained parameters agreed well with experimental results.

차세대 분산형 고속열차의 후미진동 저감에 관한 연구 (A Study on Tail Vibration Reduction for the Next Generation High Speed EMU)

  • 전창성;김영국;김석원;김상수;최성훈;박태원
    • 한국철도학회논문집
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    • 제15권6호
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    • pp.543-549
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    • 2012
  • 본 연구는 차세대 분산형 고속전철 시제차량(HEMU-430X)의 후미진동저감에 관한것이다. VAMPIRE 해석을 통한 주행거동 관찰에서 HEMU-430X는 전두부 유선형 형상유지를 위하여 설치된 한방향 요댐퍼 때문에 후미차량에서 횡방향 진동이 예상되었으며, 430km/h에서 기준치를 초과하는 경우가 있었다. 이 후미진동을 감소시키기 위하여 차륜답면 형상변경, 횡댐퍼 댐핑계수조정, 요댐퍼 계수조정 등 다양한 방법을 시도하였으나 후미진동이 없어지지 않았다. 최종적으로 요댐퍼를 양방향으로 바꾸었을 때 횡방향 진동이 사라졌다. 실제 시운전에서는 150km/h로 주행하였을 때 횡방향 후미진동이 나타났으며, 요댐퍼를 양방향으로 바꾸어 300km/h 주행 시에도 후미진동이 나타나지 않았다. 추후 430km/h까지 최고속도시험을 수행할 예정인데 높은 속도에서 후미진동이 다시 발생한다면 본 연구에서 제시한 차륜답면 형상변화, 횡댐퍼 계수 조정 등의 방법을 이용해서 진동을 저감시킬 수 있을 것이다.

An inverse LQG/LTR problem applied to the vehicle steering system

  • Park, Yong-Woon;Kim, Dae-Hyun;Scott, Kimbrough
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 1996년도 Proceedings of the Korea Automatic Control Conference, 11th (KACC); Pohang, Korea; 24-26 Oct. 1996
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    • pp.324-327
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    • 1996
  • This paper describes the robust controller design methods applied to the problem of an automatic system for tow-vehicle/trailer combinations. This study followed an inverse Linear Quadratic Regulator(LQR) approach which combines pole assignment methods with conventional LOR methods. It overcomes two concerns associated with these separate methods. It overcomes the robustness problems associated with pole placement methods and trial and error required in the application of the LQR problem. Moreover, a Kalman filter is used as the observer, but is modified by using the loop transfer recovery (LTR) technique with modified transmission zero assignment. The proposed inverse LQG,/LTR controllers enhances the forward motion stability and maneuverability of the combination vehicles. At high speeds, where the inherent yaw damping of the vehicle system decreases, the controller operates to maintain an adequate level of yaw damping. At backward moton, both 4WS (2WS tow-vehicle, 2WS trailer) and 6WS (4WS tow-vehicle, 2WS trailer) control laws are proposed by using inverse LQG/LTR method. To evaluate the stability and robustness of the proposed controllers, simulations for both forward and backward motion were conducted using a detailed nonlinear model. The proposed controllers are significantly more robust than the previous controllers and continues to operate effectively in spite of parameter perturbations that would cause previous controllers to enters limit cycles or to loose stability.

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Aerodynamic coefficients of inclined and yawed circular cylinders with different surface configurations

  • Lin, Siyuan;Li, Mingshui;Liao, Haili
    • Wind and Structures
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    • 제25권5호
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    • pp.475-492
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    • 2017
  • Inclined and yawed circular cylinder is an essential element in the widespread range of structures. As one of the applications, cables on bridges were reported to have the possibility of suffering a kind of large amplitude vibration called dry galloping. In order to have a detailed understanding of the aerodynamics related to dry galloping, this study carried out a set of wind tunnel tests for the inclined and yawed circular cylinders. The aerodynamic coefficients of circular cylinders with three surface configurations, including smooth, dimpled pattern and helical fillet are tested using the force balance under a wide range of inclination and yaw angles in the wind tunnel. The Reynolds number ranges from $2{\times}10^5$ to $7{\times}10^5$ during the test. The influence of turbulence intensity on the drag and lift coefficients is corrected. The effects of inclination angle yaw angle and surface configurations on the aerodynamic coefficients are discussed. Adopting the existed the quasi-steady model, the nondimensional aerodynamic damping parameters for the cylinders with three kinds of surface configurations are evaluated. It is found that surface with helical fillet or dimpled pattern have the potential to suppress the dry galloping, while the latter one is more effective.

이종결합 고속회전 발사 탄의 비행 안정성에 결합력이 미치는 영향성 분석 (Analysis of How the Bonding Force between Two Assemblies Affects the Flight Stability of a High-speed Rotating Projectile)

  • 이상봉;최낙선;이종현;김상민;강병덕
    • 품질경영학회지
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    • 제49권3호
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    • pp.255-268
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    • 2021
  • Purpose: We sought to understand why a high-speed rotating projectile featuring a fuze-and-body assembly sometimes exhibited airburst, and we intended to improve the flight stability by eliminating airburst. Methods: We performed characteristic factor analysis, structural mechanics modeling, and dynamic modeling and simulation; and we scheduled firing tests to discover the cause of airburst. We used a step-by-step procedure to analyze the reliability function for selecting the bonding force standard that prevents airburst. Results: The 00MM high-speed rotating projectile features a fuze bonded to a body assembly; the bonding sometimes can break on firing. The resulting contact force, vibration and roll damping during flight generated yaw. Flight became unstable; fuze operation triggered an airburst. Our reliability test improved the bonding force standard (the force was increased). When the bonding force was at least the minimum required, a firing test revealed that airburst/flight instability disappeared. Conclusion: Analysis and identification of the causes of flight instability and airburst render military training safer and enhance combat power. Ammunition must perform as designed. Our method can be used to set standards that improve the performances of similar types of ammunition.