• 제목/요약/키워드: Accelerometer Array Method

검색결과 4건 처리시간 0.022초

감쇠 단을 갖는 보의 면내 진동인텐시티 측정에 관한 연구 (Study on Measurements of the In-Plane Vibration Intensity In a Beam With a Damped End)

  • 김창열;길현권;홍석윤
    • 한국음향학회지
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    • 제24권7호
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    • pp.371-378
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    • 2005
  • 본 연구에서는 면내 진동하는 감쇠 단을 갖는 보에서 진동파워의 크기와 방향을 나타내는 면내 진동인텐시티를 측정하였다. 보의 면내 진동인텐시티 측정 방법으로서 3가지 다양한 방법을 적용하였다. 이러한 방법들은 2개의 가속도계 선형 배열을 이용하는 가속도계배열법과 하나의 가속도계를 갖고 주파수응답함수를 이용하는 주파수응답함수법 그리고 기준 가속도를 고정시키고 다른 하나의 가속도계를 이용하는 기준가속도계법 들이다. 본 연구에서는 이러한 방법들을 적용하여 보의 진동인텐시티 공간 분포를 측정하여 비교하였으며, 또한 가진 점에서 주어지는 입력 파워와 비교를 통하여 적용 가능성을 확인하였다. 이러한 결과들로부터 보의 면내 진동인텐시티를 측정하기 위하여 가속도계배열법뿐만이 아니라 주파수응답함수법과 기준가속도계법 또한 효과적으로 사용될 수 있음을 보였다.

기준 가속도계를 이용한 보의 면내 진동인텐시티 측정 (Measurements of the In-Plane Vibration Intensity of a Beam Using an Reference Accelerometer)

  • 김창렬;길현권;전진숙;홍석윤
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2002년도 추계학술대회논문집
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    • pp.848-851
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    • 2002
  • In this paper, an experimental method using a reference accelerometer has been developed to measure the in-plane vibration intensity of a beam. It has the advantages of reducing accelerometer phase error comparing with the cross spectral intensity measurement technique using an accelerometer array. It needs no measurement of the input force required in the frequency response method using the only one accelerometer This method has been used to measure the in-plane vibration intensity over the beam. The result has been compared with an input power and the vibration intensity obtained with other methods. It showed that the present experimental method can be effectively used to measure the structural in-plane vibration intensity.

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Structural Intensity 법을 이용한 구조체의 진동전달량 측정 (Measurements of the Vibrational Power Flow in Structure Beam by Using the Structural Intensity Method)

  • 김흥식
    • 소음진동
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    • 제4권2호
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    • pp.231-238
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    • 1994
  • This paper presents an experimental method to find the vibrational transmission characteristics of structures by using the structural intensity method which is used as the important techniques of active vibration control method. Experimental results are obtained from measurements performed on a structure beam by 2, 3 and 4 position linear accelerometr array (2, 3 and 4 structural intensity : 2, 3 and 4 S.I.) methods at near and farfield conditions. These results are compared with the measurement values of conventional power flow measurement method called input power measurement in order to verify the accuracy of structural intensity methods. To minimize the errors associated with 2, 3 and 4 S.I. methods, the measurement locations were selected by the result of modal analysis and the averaged data by the inter-change of accelerometer array was utilized. In 3 and 4 S.I. methods measured wavenumber instead of theoretical wavenumber was used. This paper shows that measurements of bending wave power flow by using 2, 3 and 4 S.I. methods can give accurate values under general field conditions in structural beam and the accuracy of 2, 3 S.I. methods is higher than 4 S.I. methods. Finally, 2 position linear accelerometer array method is suggested as the practical structural intensity technique.

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A method for image processing by use of inertial data of camera

  • Kaba, K.;Kashiwagi, H.
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 1998년도 제13차 학술회의논문집
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    • pp.221-225
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    • 1998
  • This paper is to present a method for recognizing an image of a tracking object by processing the image from a camera, whose attitude is controlled in inertial space with inertial co-ordinate system. In order to recognize an object, a pseudo-random M-array is attached on the object and it is observed by the camera which is controlled on inertial coordinate basis by inertial stabilization unit. When the attitude of the camera is changed, the observed image of M-array is transformed by use of affine transformation to the image in inertial coordinate system. Taking the cross-correlation function between the affine-transformed image and the original image, we can recognize the object. As parameters of the attitude of the camera, we used the azimuth angle of camera, which is de-fected by gyroscope of an inertial sensor, and elevation an91e of camera which is calculated from the gravitational acceleration detected by servo accelerometer.

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