• 제목/요약/키워드: 스카이훅 제어

검색결과 53건 처리시간 0.014초

불완전 발달 유체 유동을 고려한 MR댐퍼 착륙장치 모델링 (Modeling of MR Damper Landing Gear Considering Incompletely Developed Fluid Flow)

  • 이효상;장대성;황재혁
    • 항공우주시스템공학회지
    • /
    • 제15권1호
    • /
    • pp.7-18
    • /
    • 2021
  • 반능동형 MR댐퍼 착륙장치는 MR유체가 환형 유로를 지날 때 유체감쇠력 및 자장 제어 감쇠력을 발생시키는 댐퍼이다. 환형 유로를 지나는 MR 유체의 경우 필연적으로 불완전 발달 유동이 발생하게 되어, 이는 유체 감쇠력을 포함하는 댐퍼 내력 계산에 오차를 발생시키는 원인이 된다. 이로 인해 댐퍼 구조적 파라미터 설계 및 제어 이득 선정이 부정확해지며, 착륙장치의 동특성 및 충격흡수성능 저하를 초래하게 된다. 본 논문에서는 MR댐퍼 환형 유로의 입구영역에서 발생하는 추가적인 감쇠력을 고려한 MR댐퍼 착륙장치의 수학적 모델을 유도하였다. 본 논문에서 유도한 수학적 모델링을 MR댐퍼 착륙장치의 설계 및 최적화 과정에 적용한다면 좀 더 정확한 내력 예측으로 우수한 성능의 MR댐퍼 착륙장치를 설계할 수 있을 것으로 판단된다.

복합 모드형 ER엔진마운트의 성능평가 (II) - HILL를 통한 성능 평가 - (Performance Evaluation of a Mixed-Mode Type ER Engine Mount(II)-Performance Evaluation Via HILS-)

  • 최영태;최승복
    • 대한기계학회논문집A
    • /
    • 제24권9호
    • /
    • pp.2151-2158
    • /
    • 2000
  • This paper presents vibration control performance of a passenger vehicle installed with the mixed-mode type ER engine mounts. The performance is evaluated via hardware-in-the-loop-simulation(HILS) method. As a first step, a dynamic model of a vehicle featuring the ER engine mounts is formulated by taking into account the engine excitation forces. A new type of the fuzzy skyhook controller is then established in order to control both engine and body vibrations. This is accomplished by adopting a weighting parameter between two performance criteria which is to be determined from the fuzzy algorithm. Vertical displacement and acceleration of the engine mount obtained from the HILS method are provided in the frequency domain. In addition, vibration control performance between the conventional hydraulic engine mount and the proposed engine mount is compared in the time and frequency domains.

HILS를 활용한 전투차량의 반능동 현수장치 적용에 관한 연구 (A Study on the Appication of Semi-Active Supension Units for a Combat Vehicle by Using HILS)

  • 김지웅;김문준;이은준;이경훈;우관제
    • 한국군사과학기술학회지
    • /
    • 제13권6호
    • /
    • pp.967-975
    • /
    • 2010
  • There have been a lot of efforts on the improvement for the ride comfort and handling stability of the combat vehicles. Especially most of vehicles for military purpose have bad inertial condition and severe operating condition such as the rough road driving, and need a high mobility in the emergency status. It is necessary to apply the controlled suspension system in order to improve the vehicle mobile stability and ride comfort ability of crews. A feasibility study is performed on the application of the semi-active suspension system with a magneto-rheological controlled shock absorber for a $6{\times}6$ combat vehicle. First, the dynamic simulation model of the vehicle including the control model for the semi-active suspension system was executed. Based on this model, a hardware-in-the-loop simulation(HILS) system which has a semi-active suspension controller hardware was constructed. After full vehicle simulations were performed in virtual proving courses with this system, the semi-active suspension system was proven to give better ride comfort and handling stability in comparison with the conventional passive suspension system.