The vibration of flying missile head is a subject of random vibration mainly. Calculating the random response is a major work of missile head structure and environment analysis.
弹头在飞行过程中的振动主要是随机振动，计算随机激励下弹头的响应是弹头结构强度和环境分析的重要任务之一。
The Exoatmospheric Kill Vehicle (EKV) is a small flying device located in the tip of a Ground-Based Interceptor (GBI) missile.
外太空杀伤拦截器(EKV)是一种位于陆基拦截弹(GBI)顶部的小型飞行器。
Ukrainian officials denied the U. S. missile claim, saying they had launched only short-range missiles that couldn't reach the plane flying some 155 miles away.
乌克兰官员否认了美国有关导弹误射的说法，辩称他们只发射了短程导弹，不可能击中飞行在155英里以外的客机。
In the case of lacking remote signal of the missile at flying extremity, it is a credible method to recur the data of movement parameter at that time using grey forecast model.
在导弹飞行末段遥测信号缺失的情况下，采用灰色预测模型对导弹飞行末段的运动参数进行数据重现是一种较为可信的方法。
Flying simulated drone of skimming sea missile is one of the important drone to complete short range antimissile warship gun weapon system development test and equipment adopt.
掠海导弹飞行模拟靶标是完成近程反导舰炮武器系统研制试验及装备交验所必须的重要靶标之一。
It is a ubiquitous matter, for example, the photo shot at the plane or space aerocraft, the photo of object moving at high speed, missile flying at the battlefield.
运动模糊是成像过程中普遍存在的问题，在飞机或宇宙飞行器上拍下来的照片，用照相机拍摄高速运动物体的照片，以及战场上飞行中的导弹均可能存在这种现象。
The paper analyses the importance of measuring vibrating data of air-to-air missile in flying experiment, it introduces a multi-range acquisition method of air-to-air missile vibrating sensor signal.
分析了准确测量空空导弹在飞行试验中振动数据的重要性，介绍了一种空空导弹振动传感器信号多量程采集的方法。
U. S. intelligence officials believe the plane was accidentally hit by a Ukrainian S-200, or SA-5, missile - a large surface-to-air missile built to shoot down heavy bombers flying at high altitudes.
美国情报官员确信这架飞机是被一枚乌克兰发射的S-200，又名为SA-5导弹意外击落的，这是一种被用来击落高空重型轰炸机的大型地对空导弹。
It is a ubiquitous matter, for example, the photo shot at the plane or spacecraft, the photo of object moving at high speed, missile flying at the battlefield.
这种运动模糊现象是成像过程中普遍存在的，例如：在飞机或太空飞行器上拍摄的照片、战场上高速飞行的物体的运动照片。
But now the parameters of digital autopilot system can be easily designed, changed and loaded at real-time, at different flying states and at different Mach Numbers by missile-borne computer.
随着数字式弹载计算机的使用，自动驾驶仪能够很方便地实现系统变参数设计，在不同的马赫数及不同的飞行状态下，通过弹载计算机的解算来实时装订系统参数。
But now the parameters of digital autopilot system can be easily designed, changed and loaded at real-time, at different flying states and at different Mach Numbers by missile-borne computer.
随着数字式弹载计算机的使用，自动驾驶仪能够很方便地实现系统变参数设计，在不同的马赫数及不同的飞行状态下，通过弹载计算机的解算来实时装订系统参数。
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