| 1. | Moment gyroscope is implement institution of the satellite attitude control system . the dynamics equation of single gimbal control moment gyroscope is set up , the control law of moment gycroscope is designed and the distribute matrix is confirmed reasonly 选择力矩陀螺作为该卫星控制系统的执行机构,建立单框力矩陀螺的动力学方程,在此基础上进行力矩陀螺控制律设计,合理地确定力矩陀螺的分配矩阵。 |