自适应主动机翼颤振抑制系统设计
The Design of an Adaptive Active Wing Flutter Control System
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摘要: 本文介绍一种用九模态描述的运输机机翼自适应颤振抑制系统的设计方法.通 过数字机模拟试验表明,本文所述方法使颤振速度提高40.6%.Abstract: A design method of an adaptive active wing flutter control system for a transport aircraft wing flutter model in 9 modes is described in this paper. The performance of the adaptive control law was evaluated in flight test simulation. The simulation result shows that the flutter velocity has been increased by 40.6%.
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