CAJ | 학술논문

控制力矩陀螺是一种常用的航天器的执行机构。介绍了M o del 750型控制力矩陀螺结构组成，对装置的数学模型进行了推导，以M o del750型控制力矩陀螺为研究对象，分析了陀螺的进动性和章动性原理，设计了实验步骤并进行仿真验证，得到的仿真图形较好地说明了陀螺特性的现象。
공제력구타라시일충상용적항천기적집행궤구。개소료M o del 750형공제력구타라결구조성，대장치적수학모형진행료추도，이M o del750형공제력구타라위연구대상，분석료타라적진동성화장동성원리，설계료실험보취병진행방진험증，득도적방진도형교호지설명료타라특성적현상。
The control moment gyroscopes (CMG) are widely used in spacecrafts such as satellites and space stations as actuators of attitude control .In order to grasp the principle of control moment gyroscope ,the structure of Model 750 is introduced in the first part and the mathematical model of the device has been deduced in the second part .Based on Model 750 ,the gyroscopes characteristics are analyzed firstly ,and tested by using steps of experiments which are designed in the third part ,and then the phenomenon of gyro characteristics can be shown through simulation graphs .