变结构控制作为控制系统的一种综合方法，它的滑动模态具有不变性，这是变结构控制在导弹姿态控制中最突出的优点。
As a synthesis method in control system, the sliding mode of variable structure control is invariable, and which is its most excellent advantage in the missile attitude control system.
在小子样情况下，利用系统和分系统试验数据对导弹的飞行可靠性指标进行评定，从数学上说是系统可靠性综合问题。
In the situation of small samples, it belongs to systems reliability integration by math that we estimate the flight reliability of missile using systems and subsystems testing data.
根据海军导弹使用、维护情况以及技术保障要求，建立导弹武器系统综合保障管理信息系统。
According to the use, the maintenance and the technical support demand of navy missile equipment, this paper exploit mis of Integrated Logistics support for Guided missile Weapon System.
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