对星载二维转台中反作用轮的控制技术进行了研究。
The control technique of reaction wheel in the two-axis gimbals mechanism on the satellite is researched.
反作用轮微振动是影响卫星姿态控制精度的重要因素。
Reaction wheel is one of the main disturbance sources for the attitude control system accuracy of spacecraft.
在现代卫星的姿态控制系统中，反作用轮得到了广泛应用。
Reaction wheels are widely used in the modern spacecraft attitude control systems.
反作用轮是影响航天器姿态控制系统精度的主要扰动源之一。
Reaction wheel is one of the main disturbance sources for the attitude control system accuracy of spacecraft.
反作用轮系统是影响航天器姿控系统精度的主要扰动源之一。
Reaction wheel is one of the main disturbance sources that affect the precision of attitude control system of spacecraft.
反作用轮系统是影响航天器姿控系统精度的主要扰动源之一。
Reaction wheel assembly is one of the main disturbances affecting the accuracy of attitude control system in the spacecraft.
反作用轮系统是影响航天器姿控系统精度的主要扰动源之一。
Reaction wheel is one of the main disturbance sources for the attitude control system accuracy of spacecraft.
反作用轮是影响航天器姿态控制系统精度的主要扰动源之一。
Reaction wheel is one of the main disturbance sources that affect the precision of attitude control system of spacecraft.
本文首先采用虚功原理建立了反作用轮的扰动解析模型，然后给出了反作用轮的实验模型。
In this paper, an analytical model is firstly set up using virtual work principle, an empirical model is then given.
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.
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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