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本文设计了一种控制装置,用于控制飞控计算机中的特殊版本软件向作动系统发送扫频信号来测得飞机的伺服弹性稳定性。本成果已在某型号飞机全机结构模态耦合试验得到应用。
In this paper, a control device is designed to control the special version software in the flight control computer to send the sweep signal to the actuation system to measure the servo elasticity stability of the aircraft. This result has been applied in the modal coupling test of the whole aircraft structure of a certain type of aircraft.