The FY-4 satellite arrived at the Xichang Satellite Launch Center on October 23 and prepares for launch scheduled in the mid of December.The FY-4 satellite had completed all testing including integrated satellite micr...The FY-4 satellite arrived at the Xichang Satellite Launch Center on October 23 and prepares for launch scheduled in the mid of December.The FY-4 satellite had completed all testing including integrated satellite micro-vibration test,image navigation and registration test,展开更多
针对欠驱动旋转激励平移振荡器(translational oscillations with a rotational actuator, TORA)系统的控制问题,使用一种自耦PID (self-coupling proportional-integral-differential, SCPID)控制方法.该方法首先利用坐标变换使TORA系...针对欠驱动旋转激励平移振荡器(translational oscillations with a rotational actuator, TORA)系统的控制问题,使用一种自耦PID (self-coupling proportional-integral-differential, SCPID)控制方法.该方法首先利用坐标变换使TORA系统的质心映射为Huygens振动中心,以实现新系统控制输入解耦,避免零动态不稳定问题;然后对Huygens振动中心设计平移位置的SCPID控制器,同时获得小球偏转角度的虚拟指令,进而设计小球偏转角度的SCPID控制器,从而实现TORA系统的平衡点跟踪控制;最后在复频域对闭环控制系统的稳定性进行严格的数学分析和证明.仿真及与其他方法的结果对比表明,所设计的控制算法简单高效,在欠驱动控制系统领域具有实际的应用价值.展开更多
文摘The FY-4 satellite arrived at the Xichang Satellite Launch Center on October 23 and prepares for launch scheduled in the mid of December.The FY-4 satellite had completed all testing including integrated satellite micro-vibration test,image navigation and registration test,
文摘针对欠驱动旋转激励平移振荡器(translational oscillations with a rotational actuator, TORA)系统的控制问题,使用一种自耦PID (self-coupling proportional-integral-differential, SCPID)控制方法.该方法首先利用坐标变换使TORA系统的质心映射为Huygens振动中心,以实现新系统控制输入解耦,避免零动态不稳定问题;然后对Huygens振动中心设计平移位置的SCPID控制器,同时获得小球偏转角度的虚拟指令,进而设计小球偏转角度的SCPID控制器,从而实现TORA系统的平衡点跟踪控制;最后在复频域对闭环控制系统的稳定性进行严格的数学分析和证明.仿真及与其他方法的结果对比表明,所设计的控制算法简单高效,在欠驱动控制系统领域具有实际的应用价值.