According to the characteristic of zero-momentum reaction wheel,the magnetic control laws were improved. The proposed scheme was applied to zero-momentum wheel system to cope with its attitude control problems while non-decoupling.
将偏置动量轮卫星的进动和章动抑制原理引入零动量控制系统,并针对零动量轮卫星自身特性,对磁控制规律进行改进,解决了不解耦情况下零动量轮卫星的进动抑制问题。
参考来源 - 零动量轮卫星姿态控制系统研究·2,447,543篇论文数据，部分数据来源于NoteExpress
在人造卫星的姿态控制中，广泛地采用偏置动量轮控制系统。
A momentum wheel control system is widely used for the attitude control of satellite.
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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