振动
航天器
形状记忆合金*
振动控制
模式(计算机接口)
滑模控制
工程类
控制(管理)
形状记忆合金
结构工程
控制理论(社会学)
计算机科学
航空航天工程
物理
非线性系统
声学
算法
操作系统
量子力学
人工智能
出处
期刊:Mechanical Engineering & Automation
日期:2010-01-01
被引量:1
摘要
Taking flexible spacecraft with solar panels as study object,this paper established the system's dynamics model.A sliding mode variable structure control law to control the vibration of solar panels was put forward.SMA wires were embedded into solar panels,and the classical linear optimal control was used to control the SMA drive.The simulation results show the control law suppresses the vibration of the panels effectively.
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