TAMAM RWA Micro-Vibration Test and Analysis

TAMAM 반작용휠의 미소진동 측정 및 분석

  • 오시환 (한국항공우주연구원 위성제어그룹) ;
  • 이승우 (한국항공우주연구원 위성제어그) ;
  • 최홍택 (한국항공우주연구원 위성제어그) ;
  • 이선호 (한국항공우주연구원 위성제어그) ;
  • 용기력 (한국항공우주연구원 위성제어그룹)
  • Published : 2003.11.01

Abstract

In this paper, we briefly introduce the test bench and test method of RWA micro-vibration. TAMAM RWA (Reaction Wheel Assembly) micro-vibration was measured on a KISTLER dynamic plate which can measure time signals of three orthogonal forces and torques simultaneously up to 400Hz, and test data was analyzed. Measured data were evaluated with respect to the wheel spin rate and the static/dynamic unbalances were estimated from the extracted first harmonic component. The estimated static and dynamic unbalances were 0.79gㆍcm and 17.4gㆍ$\textrm{cm}^2$ respectively. The resonance mode and two rocking modes were observed as a results of its frequency analysis. Several higher order harmonic components were observed, which comes from its rotor shape as well as the wheel bearing.

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