飞轮控制系统是个多回路系统，内回路为电压稳定回路，外回路在不同的工作模式下分别为电流回路和转速回路。
Flywheel control system has two closed loops, the inner is voltage stabilization loop, other is current loop or is speed loop in different mode.
设计了由PW M脉宽调制技术构建的工作在速率控制模式下的反作用飞轮控制系统，并对其硬件电路进行了具体实现。
The reaction flywheel control system was designed by using PWM technology under the velocity control mode, and the hardware circuit was also set up.
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.
作为一种高精度的执行机构，反作用飞轮已广泛应用于卫星姿态控制系统中。
As a kind of high accuracy executive machine, reaction wheel has been extensively applied to the attitude control system (ACS) of satellites.
反作用飞轮是卫星姿态控制系统的重要执行元件，提高飞轮系统的性能对卫星姿态控制系统具有重要意义。
Reaction wheel is an important executive component of satellite attitude control system, and the improvement of flywheel system is spurred by high performance satellite attitude control system.
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.
目前空间飞行器的高精度姿态控制系统大多采用飞轮系统。
Now, flywheels systems are elected as the actuators of attitude control system with high precision for most spacecrafts.
设计了基于永磁无刷直流电机的飞轮储能单元的能量转换控制系统。
In this paper, an energy converter system for flywheel energy storage system (FESS) using permanent magnet brushless DC motor (BLDCM) is designed.
最后，针对实验中的问题，分析了零部件加工误差、磁悬浮飞轮的悬浮气隙、控制系统的PID参数等因素对磁悬浮飞轮稳定悬浮的影响。
At last, in allusion to the problems in experiment, the processing tolerance of components and parts, the gas gap of maglev flywheel, the PID parameters of control system are analyzed.
反作用飞轮是卫星姿态控制系统的重要执行元件，提高飞轮系统的性能对卫星姿态控制系统具有重要意义。
Reaction wheel is one of the main disturbance sources that affect the precision of attitude control system of spacecraft.
研究航天器集成能量与姿态控制系统中飞轮的控制律。
Research on Distributed Interactive Simulation Method of Missiles Attitude Control System;
研究航天器集成能量与姿态控制系统中飞轮的控制律。
Research on Distributed Interactive Simulation Method of Missiles Attitude Control System;
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