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NTIS 바로가기한국항공우주학회지 = Journal of the Korean Society for Aeronautical & Space Sciences, v.32 no.5, 2004년, pp.65 - 73
방효충 (한국과학기술원, 항공우주공학전공) , 박영웅 (한국항공우주연구원)
CMG(Control Momentum Gyro) is a control device being used for spacecraft attitude control constructing relatively large amount of torque compared to conventional body-fixed reaction wheels. The CMG produces gyroscopic control torque by continuously varying the angular momentum vector direction with ...
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