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本文论述飞航式导弹弹体结构和弹上设备振动控制的基本原理。根据这些原理,运用振动控制技术,解决飞航式导弹在飞行试验中出现的故障问题。
This article discusses the basic principles of missile-based missile projectile structure and on-board equipment vibration control. According to these principles, vibration control technology is used to solve the problem of flight-type missiles in flight test.