分析了仅靠飞轮控制的零动量轮卫星系统的稳定性。
The stability of zero-momentum wheel satellite, only using wheel as the executive component, was analysed.
本文提出一个与常规不同的零动量——偏置动量三轴姿态控制系统的设计方案。该系统由四个斜装的反作用轮组成。
In this paper an advanced design concept of zero-bias momentum 3-axes attitude control system consisting of four skew reaction wheels is presented.
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