A dynamic controller is presented for rest - to - rest flexible spacecraft attitude maneuver with the active vibration suppression.

针对航天器三轴同时姿态机动时挠性附件的振动抑制问题,提出了基于动态输出反馈控制的主动振动抑制方法.

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In this design approach, attitude control and vibration suppression were designed separately using lower order model.

针对挠性卫星大角度姿态机动的振动抑制问题, 提出了一种双回路鲁棒主动振动控制方法.

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