• 제목/요약/키워드: Sky-hook Theory

검색결과 10건 처리시간 0.02초

출력귀환과 스카이 훅 제어 방식에 의한 차량 현가 장치의 성능에 관한 연구 (A Study on the Performance of Car Active Suspension System by the output Feedback and Sky-hook Control Method)

  • 김재열
    • 한국생산제조학회지
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    • 제5권4호
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    • pp.7-16
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    • 1996
  • The dynamic model of the suspension system is developed by using both sky-hook control and output feedback control techniques. based on the performance sensitivity index, Many vehicles use sky-hook control theory operated with only one sensor, due to relatively low cost and easy implementation. On the other hand, output feedback control implemented with state variables has difficulties in measuring such as tire deflection, etc.

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스카이훅 시스템에의 능동 서스펜션 제어 이론 적용에 관한 연구 (A Study on Adopting Active Suspension Control in Sky Hook System)

  • 박중현;장승재
    • 한국정보통신학회논문지
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    • 제10권5호
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    • pp.950-955
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    • 2006
  • 본 논문에서는 스카이훅댐퍼 시스템의 해석 및 설계에 능동 서스펜션 제어 이론을 적용하여 현가장치설계에 응용 할 수 있는 이론 및 실험 적 제어장치 적용에 관한 연구를 수행하였다. 최근의 현가장치설계에서는 강성과 감쇠를 능동적으로 제어하는 기술의 적용이 일반화되고 있으며, 다른 차량안정성 제어장치와의 연계성이 높아짐에 따라, 제어 시스템설계에서 보다 내구성 이 강하고 제어효과의 응답성이 빠르며 정도 또한 높은 제어장치의 필요성이 요구되고 있다. 본 연구는 댐퍼의 위치관계에 따른 스카이훅시스템을 해석하여 위와 같은 빠른 응답성과 높은 정도의 제어가 가능한 제어시스템을 해석, 설계하기 위하여 강인제어시스템의 적용에 관한 고찰을 하였다. 그리고 제어대상시스템에 대한 강인제어시스템을 설계하기 위한 모델링 및 적용방법을 수식적으로 해석하였으며, 스카이훅현가장치의 제어시 스템설계에 중요한 내외란성 향상을 위한 강인제어시스템설계에 적용하는 방법에 관해 고찰하였다.

현가장치의 성능향상을 위한 지능형 제어로직에 관한 연구 (A Study on the Knowledge Based Control Algorithm for Performance Improvement of the Automotive Suspension System)

  • 소상균;변기식
    • 동력기계공학회지
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    • 제5권2호
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    • pp.87-92
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    • 2001
  • Automotive suspension system is a mechanism for isolation of the vibration coming from the road inputs. Recently, the electronically controlled suspension systems which may improve ride and handling performance have been developed. Here, the continuously controlled semi-active suspension system is focused. As a mechanism to control damping forces continuously, a solenoid valve is used. The modeling for the solenoid valve is introduced briefly, a vehicle dynamics modeling is constructed, and then combined system model is completed. To design the efficient control algorithm for the semiactive suspension system the knowledge based fuzzy logic is applied and the technique how to apply the sky-hook theory to the fuzzy logic is developed. Finally, to confirm the improvement of performance the computer simulation is carried out.

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센서위치를 고려한 능동 서스펜션 강인제어에 관한 연구 (A Study on Active Suspension Robust Control with Sensor and Actuator Location)

  • 박중현;장승재
    • 한국정보통신학회논문지
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    • 제10권6호
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    • pp.1147-1152
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    • 2006
  • 본 논문에서는 스카이훅댐퍼 시스템의 해석 및 설계에 능동 서스펜션 강인제어 이론을 적용하여 현가장치설계에 응용 할 수 있는 이론 및 실험적 제어 장치 적용에 관한 연구를 수행하였다. 최근의 현가장치설계에서는 강성과 감쇠를 능동적으로 제어하는 기술의 적용이 일반화되고 있으며, 다른 차량안정성제어장치와의 연계성이 높아짐에 따라, 제어시스템설계에서 보다 내구성이 강하고 제어효과의 응답성이 빠르며 정도 또한 높은 제어장치의 필요성이 요구되고 있다. 본 연구는 센서의 위치 관계에 따른 능동현가시스템을 해석하여 위와 같은 빠른 응답성과 높은 정도의 제어가 가능한 제어시스템을 해석, 설계하기 위하여 강인제어시스템의 적용에 관한 고찰을 하였다. 그리고 제어대상시스템에 대한 강인제어시스템을 설계하기 위한 모델링 및 적용방법을 수식적으로 해석하였으며, 스카이훅현가장치의 제어시스템설계에 중요한 내외란성 향상을 위한 강인제어 시스템설계에 적용하는 방법에 관해 고찰하였다.

MR마운트 진동제어 성능 향상을 위한 슬라이딩 모드 제어 (Sliding Mode Control for Improving Performance of Mount with MR(Magneto-Rheological) Fluid)

  • 안영공;김성하;정석권
    • 동력기계공학회지
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    • 제21권4호
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    • pp.18-25
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    • 2017
  • This paper deals with vibration control of a small mount with MR(Magneto-Rheological) fluid as a functional fluid mount for precision equipment of automobiles. Damping and stiffness coefficients of the mount with MR fluid are changed by variations of the applied magnetic field strength. We present the robust control scheme, based on a conventional sliding mode control theory, for the design of a stable controller that is capable of vibration control due to various disturbances such as impact and periodic excitations, and is insensitive to dynamic properties of the mount. We got stable controller by using Lyapunov stability theory. The controller is then realized by using a semi-active control condition in simulations. Chattering problem of the sliding mode control is eliminated by saturation function instead of signum function. The sliding mode control with Lyapunov stability theory is superior to passive and Sky-Hook control in performance.

능동적 점성감쇠를 이용한 차량용 동적 흡진기의 모델링과 제어에 관한 연구 (A Study about Modeling and Control of Dynamic Absorber for Vehicle by Using Active Viscous Damping)

  • 김대원;배준영
    • 소음진동
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    • 제9권1호
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    • pp.121-130
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    • 1999
  • Generally, A Dynamic Absorber by using Active viscous Damping is highlighted for effective suspension system, such as improved ride comfort and handling in the market. Lately, this system based on the Sky-Hook damper theory is introduced by the name of "Active Dynamic Absorber" to us. This system has an excellent performance in contrast to Passive. Adaptive Dynamic Absorber, besides having low cost components of system, low energy consumption. light weight of system. In this viewpoint. most of car-maker will adopt this system in the near future. For this reason, we developed Dynamic Absorber by using Active viscous Damping which is equipped with continuously variable Dynamic Absorber and Control logic consisting Filter and Estimator. control apparatus of Dynamic Absorber operated by 16-bit microprocessor of high performance. variable device of viscous Damping. G-sensor so on. In this paper. several important points of development procedure for realizing this system will be described with results in which is obtained from experiment by simulation and Full car test in Proving ground. respectively.pectively.

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승용차용 능동제어식 현가시스템의 개발(2); 실차 성능실험 및 결과 (Development of an Active Suspension System for Passenger Cars( II ) ; Prototype Car Test Result)

  • 황요하;홍예선;이종민;배준영
    • 한국자동차공학회논문집
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    • 제2권2호
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    • pp.83-94
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    • 1994
  • Performance test result on prototype car equipped with low-band type active suspension system is reported. Control theory is explained first. Simulation for feasibility and parameter tuning, control module test using hydraulic exciter and test run, and performance evaluation of the test car on test track are reported successively. Emphasis was put on modification of control theory which caused many unexpected problems in actual implementation.

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실험적 MR댐퍼 모델을 사용한 1/4차량 진동 시뮬레이션 (1/4 Car Vibration Simulation Using An Empirical MR Damper Model)

  • 백운경;양보석;이종석;강태호;류성원
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2005년도 춘계학술대회논문집
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    • pp.638-643
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    • 2005
  • This study is about a semi-active quarter car simulation method including a MR(magneto-rheological) damper. The MR damper was modeled as Spencer model that can capture nonlinear and hysteretic behavior. The parameters of the Spencer model were extracted from a random excitation test and optimum treatment of the test data. Then, a suspension control algorithm based on Sky-hook theory was applied for the quarter car simulation. Also, an experiment was dong using a quarter car simulator to confirm the simulation results with the Spencer MR damper model

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실험적 MR댐퍼 모델을 사용한 1/4 차량 진동 시뮬레이션 (1/4 Car Vibration Simulation Using an Empirical MR Damper Model)

  • 양보석;이종석;강태호;류성원;백운경
    • 한국소음진동공학회논문집
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    • 제15권9호
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    • pp.1016-1022
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    • 2005
  • This study is about a semi-active quarter car simulation method including a MR(magneto-rheological) damper. The MR damper was modeled as Spencer model that can capture nonlinear and hysteretic behavior. The parameters of the Spencer model were extracted from a random excitation test and optimum treatment of the test data. Then, a suspension control algorithm based on Sky-hook theory was applied for the quarter car simulation. Also, an experiment was done using a quarter car simulator to confirm the simulation results with the Spencer MR damper model.

비행 구조물에 탑재된 정밀 기기의 능동 진동 제어 (Active Vibration Control of a Precision Equipment on Flying Vehicle Structure)

  • 이재홍;유진형;박영필
    • 대한기계학회논문집A
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    • 제23권11호
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    • pp.1912-1921
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    • 1999
  • The equipments mounted on guided-missile undertake heavy vibrational disturbance. Sometimes the equipments mounted on guided-missile go wrong so that the guided-missile flies over unintended place. For the vibration isolation of the equipments mounted on guided-missile, active vibration control was performed. In the case of active vibration technique, the stiffness matrix and the mass matrix are derived based on FEM (ANSYS5.0). Model reduction was carried out and, as a result, we got 7 DOF mass and stiffness matrix. For the sake of FEM model identification, modal experiment was carried out. With the help of Sensitivity Analysis, the natural frequencies of FEM were tuned to those of Experiment. In this work, the Sky Hook and the LQG control theory were adopted for v iteration control using stacked piezoactuator. Experiments were performed with changing excitation frequency from 10 Hz upto 200 Hz and we got frequency response function of guided-missile equipments. The magnitude of 3rd mode of guided-missile equipments is 8.6 % that of Uncontrolled in Skyhook controller and is 3.4 % that of uncontrolled in LQG controller.