STSAT RWA Micro-Vibration Test and Analysis

과학기술위성 반작용휠의 미소진동 측정 및 분석

  • 오시환 (한국항공우주연구원 위성제어그룹) ;
  • 남명용 (한국과학기술원 인공위성연구센터) ;
  • 박연묵 (한국과학기술원 인공위성연구센터) ;
  • 임조령 (한국항공우주연구원 위성제어그룹) ;
  • 금정훈 (한국항공우주연구원 위성제어그룹) ;
  • 이승우 (한국항공우주연구원 위성제어그룹)
  • Published : 2004.11.01

Abstract

STSAT RWA (Reaction Wheel Assembly) micro-vibration is measured using KISTLER dynamic plate that can provide the time signals of three orthogonal forces and torques simultaneously up to 400Hz. In the post-processing, measured data are evaluated with respect to the wheel spin rate in both time and frequency domains, and the static/dynamic unbalances are evaluated from the extracted first harmonic component. Also the friction torque profile at each wheel speed is estimated from the measured data. Several higher order harmonic components are observed, that comes from its rotor shape as well as the wheel bearing characteristics. One of the most peculiar characteristics of this wheel is that the dynamic properties of two radial unbalance components are much different from each other as the RWA mounting configuration on a spacecraft is different from conventional RWA mounting configuration. Rocking mode is not appeared below 400Hz for all operating speed because the wheel size is very small. The post-processed results will be used for jitter analysis of STSAT due to RWA micro-vibration.

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