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介绍采用压电晶体加速度传感器与信号分析仪进行导弹折叠翼实验的原理、方法，并以某导弹实例进行了测量，证明了本方法是可靠的，实用的。
This paper introduces the principle and method of missile folding wing experiment using piezoelectric accelerometer and signal analyzer, and takes a missile as an example. It proves that this method is reliable and practical.