Satellite roll-yaw angles stable control using magnetically suspended momentum wheel(MBMW) with vernier gimballing capacity is investigated.
研究基于磁悬浮动量轮的微框架能力进行卫星的滚动-偏航姿态稳定控制问题。
Satellite roll-yaw angles stable control using magnetically suspended momentum wheel(MBMW) with vernier gimballing capacity is investigated.
研究基于磁悬浮动量轮的微框架能力进行卫星的滚动-偏航姿态稳定控制问题。
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