介绍了反作用飞轮力矩模式反馈补偿控制系统的设计。
In this paper, the design of a feedback compensation control system for reaction wheel of torque mode is introduced.
给出了实现飞轮力矩伺服控制算法的系统级ASIC结构。
Finally the single-chip flywheel torque servo controller was implemented on a system level ASIC.
这种方法不需要对每个飞轮的力矩控制信号进行积分，减小了计算量。
This method didn't need to integrate the torque control command of every flywheel and reduced calculation amount.
提出了用直流力矩电动机在反作用飞轮控制方式下对气球吊篮的方位控制，从理论上研究了气球吊篮方位控制系统。
The nacelle azimuth control of DC torque motor under the reaction flywheel control mode is presented, and the nacelle azimuth control system is investigated in theory.
实现了用直流力矩电机在反作用飞轮控制方式下对气球吊篮的方位控制。
DC torque motor under the reaction flywheel control mode was used in nacelle azimuth control in this paper.
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。
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.
卫星姿控飞轮是由三相轮流换向无刷直流电动机驱动的，采用力矩控制(电流反馈)模式。
Satellite attitude control flywheel is driven by three-phase alternate commutating brushless DC motor, schema of which is torque control model (current feedback).
主要研究了航天器姿控系统中冗余飞轮构型的力矩分配问题。
This article deals with torque allocation for redundant flywheel configurations in a spacecraft attitude control system.
实验结果表明，该飞轮系统在整个四象限区域内均具有良好的动态和静态力矩控制性能。
Experimental results indicate that the flywheel system can provide satisfactory dynamic and static performances throughout the whole four quadrants.
实现了用直流力矩电机在反作用飞轮控制方式下对气球吊篮的方位控制。
Reaction wheel is one of the main disturbance sources that affect the precision of attitude control system of spacecraft.
变惯量反作用飞轮是一种新型的动量交换装置，不仅可以通过改变飞轮转速输出力矩，还可以通过改变其转动惯量实现大范围的力矩输出。
VIRW is a new momentum exchange device, which can provide attitude control torque not only by adjusting the spin rate, but also by changing the inertia of the wheel.
实现了用直流力矩电机在反作用飞轮控制方式下对气球吊篮的方位控制。
The results of simulation show that the gondola control system achieves the desired results.
对飞轮类转子的电磁轴承的陀螺力矩耦合现象进行分析，并对径向四自由度系统建模，应用软件方法在控制中对其进行速度交叉解耦补偿。
This paper analyzes the flywheel rotor's gyroscopic coupling effect on the electromagnetic bearing and derives the motion equations of radial four-degree-of-freedom rotors.
对飞轮类转子的电磁轴承的陀螺力矩耦合现象进行分析，并对径向四自由度系统建模，应用软件方法在控制中对其进行速度交叉解耦补偿。
This paper analyzes the flywheel rotor's gyroscopic coupling effect on the electromagnetic bearing and derives the motion equations of radial four-degree-of-freedom rotors.
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