摘要
建立了双框架磁悬浮力矩陀螺(DGMSCMG)内外框架伺服系统耦合动力学模型,并针对未知扰动影响的非线性不确定系统,用基于扩张状态观测器(ESO)的扰动力矩估计器获取补偿力矩,在常规的比例积分微分(PID)控制器中通过前馈方式对内外框架进行前馈力矩补偿。仿真结果表明:干扰补偿控制能有效抑制航天器及框架对磁悬浮转子的耦合干扰,并提高了磁悬浮转子系统的稳定性。
The coupling dynamics modeling for double gimbal magnetically suspended control moment gyroscope of inside and outside gimbal servo system was established in this paper.Aim to the nonlinear system under uncertain disturbance,the compensate moment estimate was obtained based on expand state observation and it was used as the forward moment compensate for inside and outside gimbal by routine PID controller.The simulation results for forward moment compensate of inside gimbal showed that the disturb compensate control could restrain the coupling disturb between spaceflight and magnetically suspended rotor in effect and also improve the system stability of magnetically suspended rotor system.
引文
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