摘要
反作用飞轮是航天空间飞行器姿态控制系统的执行机构,其驱动电动机伺服系统性能优劣对飞行器的姿态有至关重要的作用。详细介绍磁悬浮反作用飞轮驱动用无刷直流电动机伺服控制系统的工作原理和设计方案,并且通过实验证明该控制系统可实现对磁悬浮反作用飞轮的精确控制。
Reaction fly-wheel is the implementary element of the poser control system of the space vehicle. The control system of servo motor plays an important role in spacecraft attitude. The article introduces the principle of control system of servo motor, design process. In the end, the experiment also proves that the control system designed can precisely control the reaction fly-wheel.
出处
《微电机》
北大核心
2008年第1期27-30,共4页
Micromotors