Analytical & Experimental Study on Microvibration Effects of Satellite

인공위성의 미소 진동 영향성에 관한 해석 및 실험적 연구

  • 박지용 (KAIST 대학원 항공우주공학 전공) ;
  • 이대은 (KAIST 대학원 항공우주공학 전공) ;
  • 윤재산 (KAIST 대학원 항공우주공학 전공) ;
  • 한재흥 (KAIST 항공우주공학 전공)
  • Published : 2013.04.24

Abstract

Number of components and payload systems installed in satellites were found to be exposed to various disturbance sources such as the reaction wheel assembly, the control moment gyro, coolers, and others. A micro-level of vibration can introduce jitter problems into an optical payload system and cause significant degradation of the image quality. Moreover, the prediction of on-orbit vibration effects on the performance of optical payloads during the development process is always important. However, analyzing interactions between subsystems and predicting the vibration level of the payloads is extremely difficult. Therefore, this paper describes the analytical and experimental approach to microvibration effects on satellite optical payload performance with integrated jitter analysis framework, micro vibration emulator and satellite structure testbed.

Keywords

Acknowledgement

Supported by : 한국연구재단