항공우주시스템공학회지 (Journal of Aerospace System Engineering)
- 제1권3호
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- Pages.32-36
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- 2007
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- 1976-6300(pISSN)
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- 2508-7150(eISSN)
반작용 휠의 외란에 의한 STSAT-3 지터 분석
Analysis of STSAT-3 Jitter due to the Reaction Wheel Disturbance
초록
When the reaction wheel rotates, the disturbance occurs mainly due to the mass imbalance. It is necessary to predict the effect of disturbance on the attitude stability of the satellite. The disturbance forces and torques are identified and the attitude jitter of the satellite is analyzed depending on the configuration of the wheels. On the analysis the equation of the satellite motion is combined with the translational and rotational dynamics of the wheels. The accuracy of analysis is verified by simulation of STSAT-3 satellite.