• 제목/요약/키워드: camera vibration

검색결과 239건 처리시간 0.026초

레이저와 고속 CCD 카메라를 이용한 대형구조물의 진동계측 (Vibration Measurements of Large-Scale Structure Using Laser and High-Speed CCD Camera)

  • 이창복;안세호;양성훈;염정원;강동욱;김기두
    • 한국통신학회논문지
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    • 제29권8C호
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    • pp.1104-1112
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    • 2004
  • 본 논문에서는 레이저와 고속 CCD 카메라를 이용하여 대형 구조물의 3차원 거동 계측을 위해 진동 주파수 계측 방식을 확립하였다. 구조물에 부착한 대상판에 변동(fluctuation)이 작은 다이오드 레이저를 투사하고, 고속 CCD 카메라로 촬영한 영상에 고정도 상대측정 알고리즘을 적용하여 구조물의 변위를 측정하였다. 초당 120 프레임의 고속 카메라를 이용하고 변위에 FFT를 취해 진동주파수를 구한 경우, 0에서 40Hz까지 $\pm$0.5% 이내의 진동주파수의 정확도를 얻을 수 있다. 이를 이용하면 대형 구조물에 대해 보다 저렴하고 간단하게 고유진동수의 측정이 가능하다. 또한 GPS를 이용한 상대측위 기법과의 비교를 통해 레이저를 이용한 변위측정의 정확도를 입증함으로써, 제안한 진동주파수 측정 방법의 신뢰도와 경제성을 검증하였다.

모바일 카메라 모듈용 볼베어링 방식 OIS 액추에이터 설계 (Design of Ball Bearing Type OIS Actuator for Mobile Camera Module)

  • 송명규;손동훈;박노철;박경수;박영필;임수철
    • 한국소음진동공학회논문집
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    • 제20권4호
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    • pp.361-372
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    • 2010
  • Optical image stabilization is a technique to compensate the image blurring caused by some vibrations of camera at the exposure time. Pitching and yawing of camera are sensitive to the image quality so they are usually compensated by optical image stabilization. Corresponding pitching and yawing of a camera, a lens or the image sensor is translated in two-axis direction and then the optical path of camera is adjusted. In this paper, two-axis OIS actuator for mobile camera module is suggested and designed. The actuator is a voice-coil actuator that uses the electromagnetic force of voice-coil to make compensation motions. And ball bearing is used to reduce friction force. Magnetic attractive force between magnets and yokes acts as a preload and magnet springs. Prototype actuator is fabricated to measure the friction force and to verify the feasibility of the OIS actuator with ball bearing. At last, the actuator is improved in consideration of driving force and friction force. Design of experiments is used for designing the actuator.

승용차 연료탱크의 유량변화에 따른 진동 소음 특성 (Characteristics of Vibration and Noise due to Various Fuel Quantity in Vehicle Fuel Tank)

  • 안성덕;김찬묵;강태원;사종성;권요섭;임동민
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2007년도 추계학술대회논문집
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    • pp.626-629
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    • 2007
  • Vibration originated from the fuel pump is transmitted to the fuel pump module and fuel tank. Fuel tank transmits it to chassis of vehicle. Also, noise perturbed through fuel and fuel tank is radiated out. Dynamic characteristics of fuel tank are composed of tank structure and containing fuel quantity. Therefore, this study is focused at fuel tank with various quantity. As a result, characteristics of vibration for various fuel quantity in a tank are identified as the more mass of fuel is, the less the 1st resonance frequency decrease. Also, between acoustic camera and mode shape of modal analysis are used for searching the positions of radiated noise and are found to be in accordance with each other.

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고무와 압전작동기를 이용한 무인항공기 EO/IR 센서 마운트의 설계 및 능동 진동 제어 (Design and Active Vibration Control of UAV EO/IR Sensor Mount Using Rubber Element and Piezoelectric Actuator)

  • 박동현;최승복
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2008년도 추계학술대회논문집
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    • pp.743-748
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    • 2008
  • This paper presents an inertia type of piezostack based active mount for unmanned aero vehicle (UAV) camera system. After identifying the stiffness and damping properties of the rubber element and piezostack a mechanical model of the active mount system is established. The governing equation of mount is them derived and expressed in a state space farm. Subsequently, a sliding mode controller which is robust to uncertain parameters is designed in order to reduce the vibration imposed according to the military specification associated with UAV camera mount system operation. Control performances such as acceleration and transmitted force are evaluated through both computer simulation and experimental implementation.

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압전작동기를 이용한 무인항공기 EO/IR 센서 마운트의 능동 진동 제어 (Active Vibration Control of UAV EO/IR Sensor Mount Using Piezoelectric Actuator)

  • 박동현;최승복
    • 한국소음진동공학회논문집
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    • 제18권12호
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    • pp.1278-1285
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    • 2008
  • This paper presents an inertia type of piezostack based active mount fur unmanned aero vehicle (UAV) camera system. After identifying the stiffness and damping properties of the rubber element and piezostack a mechanical model of the active mount system is established. The governing equation of mount is then derived and expressed in a state space form. Subsequently, a sliding mode controller which is robust to uncertain parameters is designed in order to reduce the vibration imposed according to the military specification associated with UAV camera mount system operation. Control performances such as acceleration and transmitted force are evaluated through both computer simulation and experimental implementation.

Non-contact monitoring of 3-dimensional vibrations of bodies using a neural network

  • Ha, Sung Chul;Cho, Gyeong Rae;Doh, Deog-Hee
    • Journal of Advanced Marine Engineering and Technology
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    • 제39권10호
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    • pp.1011-1016
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    • 2015
  • Gas piping systems in power plants and factories are always influenced by the mechanical vibrations of rotational machines such as pumps, blowers, and compressors. Unusual vibrations in a gas piping system influence possible leakages of liquids or gases, which can lead to large explosive accidents. Real-time measurements of unusual vibrations in piping systems in situ prohibit them from being possible leakages owing to the repeated fatigue of vibrations. In this paper, a non-contact 3-dimensional measurement system that can detect the vibrations of a solid body and monitor its vibrational modes is introduced. To detect the displacements of a body, a stereoscopic camera system is used, through which the major vibration types of solid bodies (such as X-axis-major, Y-axis-major, and Z-axis-major vibrations) can be monitored. In order to judge the vibration types, an artificial neural network is used. The measurement system consists of a host computer, stereoscopic camera system (two-camera system, high-speed high-resolution camera), and a measurement target. Through practical application on a flat plate, the measured data from the non-contact measurement system showed good agreement with those from the original vibration mode produced by an accelerator.

노치 대역을 개선한 이미지 흔들림 보정 장치의 동특성 향상과 이미지 분석 (Improvement of Dynamic Characteristics of OIS System using Improved Band Notch and Analysis of Images)

  • 손동훈;박노철;박영필;박경수
    • 정보저장시스템학회논문집
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    • 제7권2호
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    • pp.70-74
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    • 2011
  • The mobile camera module is a device to be inserted in the digital device for camera feature. The mobile camera module is being shaken by vibrations such as handshake during the exposure time. The clarity is compromised by these vibrations, thus the vibration is considered as an external disturbance. Moreover the use of mobile camera module has been being expanded for automotive vibration should be considered. These external disturbances can cause image blurring, thus optical image stabilization should be applied for image compensation. The compensator is fulfilled mechanically by movable lens group or image sensor that adjusts the optical path to the camera movement. Open loop control is useful for well-defined systems like compliant mechanism. Notch filter and lead compensator are designed and applied to improve the stability and bandwidth. The final level of image compensating is confirmed by image processing with MATLAB and CODE V to verify the better performance.

HILS를 통한 무인항공기 카메라 지지 능동 마운트 시스템의 진동제어 성능 평가 (Performance Evaluation on an Active Camera Mount System for UAV via Hardware-in-the-loop-simulation)

  • 오종석;최승복;조한준;이철희;조명우
    • 한국소음진동공학회논문집
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    • 제20권8호
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    • pp.767-773
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    • 2010
  • In the present work, vibration control performance of piezoactuator-based active mount system for unmanned aero vehicle(UAV) equipment is evaluated via hardware in the loop simulation(HILS). At first, the vibration level of UAV is measured and from this vibration data, the proper piezostack actuator is selected. Then, the dynamic model of active mount system including four active mounts and UAV camera equipment is derived. In order to evaluate vibration control performance, the HILS system is constructed. The proposed mount is prepared as hardware part and the other mounts are considered in software part. A sliding mode controller is designed and implemented to the HILS system. Effective vibration control results are presented in both time and frequency domains.

스테레오 영상을 이용한 비행 중인 항공기 날개의 변위 및 진동 측정 (Measurement of Aircraft Wing Deformation and Vibration Using Stereo Pattern Recognition Method)

  • 김호영;윤종민;한재흥;권혁준
    • 한국소음진동공학회논문집
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    • 제25권8호
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    • pp.568-574
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    • 2015
  • The present study was conducted by using stereo pattern recognition method(SPR method) to measure the displacement and vibration of an airplane wing in flight condition. A SPR based measurement system was developed using two visible light stereo cameras. The visible light stereo images were processed to obtain marker points by adaptive threshold method and marker filtering technique. The marker points were used to reconstruct 3D point, displacement, and vibration data. The SPR system was installed on F-16 fighter. The wing displacement and vibration were measured in flight condition. Therefore, this paper presents a possibility that SPR based measurement system using visible light stereo camera can be very useful for measuring displacement and vibration of an airplane in flight condition.