reaction-wheels 反作用飞轮
Reaction wheels are widely used in the modern spacecraft attitude control systems.
在现代卫星的姿态控制系统中,反作用轮得到了广泛应用。
In this paper an advanced design concept of zero-bias momentum 3-axes attitude control system consisting of four skew reaction wheels is presented.
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。
The time-optimal control law for motor torques of reaction wheels is designed, and, the calculated formulations of maneuver time and system state are given.
进一步的设计了反作用飞轮电机力矩的快速控制规律。给出了机动时间和系统状态的简单计算公式。
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