Earticle

초록

영어

In the present study, the inertial electromagnetic actuator (IEA) and the FxLMS (filtered-x least mean square) method were applied to study vibration control using the active mount. IEA was designed and manufactured for the experiment, and FxLMS algorithm was developed to evaluate control performance and mount dynamic characteristics. For the vibration control experiment, active mounts were installed at the top and bottom, and the lower active mount controls the force transmitted to the structure by the excitation signal from the upper active mount. The experiment was performed by simultaneously exciting three frequencies in three axes. From the experimental results, it was confirmed that the force measured at the lower active mount when the actuator is off is greatly reduced when the actuator is on, and that vibration reduction in the vertical z-axis is more effective than vibration reduction in the x-y plane.

목차

Abstract
1. 서론
2. 작동기 설계
3. 작동기 실험 및 진동제어 로직
3.1 작동기 및 진동제어 실험 방법
3.2 작동기 진동제어 로직
4. 실험 결과
4.1 작동기 성능실험 결과
4.2 진동제어 실험 결과
5. 결론
References

키워드

저자

• 정규철 [ Kyuchul Jung | Dept. of Mechanical Engineering, Sunmoon University, Graduate student ]
• 이창수 [ Changsoo Lee | Dept. of Mechanical Engineering, Sunmoon University, Graduate student ]
• 권영철 [ Young-Chul Kwon | Dept. of Mechanical Engineering, Sunmoon University ] Corresponding Author

참고문헌

발행기관

간행물

표지보기 관심저널 등록

• 간행물명

  한국기계항공기술학회지(구 한국기계기술학회지) [Journal of the Korean Society of Mechanical and Aviation Technology ]

• 간기

  격월간

• pISSN

  1229-604X

• eISSN

  2508-3805

• 수록기간

  1999~2026

• 등재여부

  KCI 등재

• 십진분류

  KDC 550 DDC 620