颤振的增益调度控制实验研究

An Investigation on Flutter Semi-active Suppression of Wing/Store System by Wind Tunnel Test

本文对机翼外挂系统颤振的半主动抑制实验进行了研究分析 ,在引入电磁阻尼器对风振控制的同时 ,根据增益调度控制原理设计并制造了控制系统 ,在风洞实验中实现了电磁阻尼器对系统的颤振半主动抑制 ,为颤振抑制的实现又提供了一种实验的方法 .

The wind tunnel tests for wing/store system flutter semi active suppression are investigated. The test model with an electro magnetic damper and the circuit control system are specially designed. The results of wind tunnel tests show that the suppression of the wing/store flutter is achieved and the method of the test is reasonable.