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A Study on the Vibration Characteristics of Camera Module for Aerial Reconnaissance Considering Vibration Isolator

방진을 고려한 항공 정찰용 카메라 모듈부의 진동특성에 관한 연구

  • Lee, Sang-Eun (EO/IR R&D Lab., LIG NEX1 Co., Ltd.) ;
  • Lee, Tae-Won (Department of Mechanical Design Engineering, Kumoh National Institute of Technology)
  • 이상은 (LIG 넥스원 연구개발본부 전자광학센터) ;
  • 이태원 (금오공과대학교 기계설계공학과)
  • Received : 2012.01.03
  • Accepted : 2012.02.01
  • Published : 2012.05.01

Abstract

A Gimbal structure system in observation reconnaissance aircraft is made up of camera module and stabilization drive device supporting camera module. During flight for image recording, the aircraft undergoes serious accelerations with wide frequencies due to several factors. Though base excitation of stabilization drive device induces vibration of camera module, it must get the stable and clean images. To achieve this aim, acceleration of camera module must be reduced. Hence, vibration isolators were installed to stabilization drive device. Considering isolators and bearings in the stabilization drive device, vibration characteristics of gimbal structure system were analyzed by finite element method. For three translational direction, acceleration transmissibility of camera module was calculated by harmonic responses analysis in the frequency range of 5 ~ 500 Hz. In addition to, sine-sweep experiment were performed to prove correctness of present analysis.

Keywords

References

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