Vibration Control System Design Using Active Devices for Large Space Structure During Attitude Maneuver

被引:0
作者
Shengyu Lin [1 ]
Yang Zhao [1 ]
Wenlai Ma [1 ]
机构
[1] Harbin Institute of Technology,Department of Aerospace Engineering
关键词
Large space structures; Actuator position optimization; Vibration control;
D O I
10.1007/s42417-025-01841-6
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