1) ship-to-air missile beyond visual range
超视距舰空导弹
1.
Towards the gaining altitude segment in the mid-course guidance of the ship-to-air missile beyond visual range,the procedure circinal arcs were applied to design the trajectory and the altitude and the pitch angle instructions were obtained.
针对超视距舰空导弹中制导的爬升段,采取两段程序圆弧相结合的方法设计弹道,给出了导弹爬升段的高度与倾角指令,并对于在圆弧间及弧与高空平飞段两转接点处出现的抖动现象,通过改变转接基准并做必需的导引指令修正,有效地解决了抖动问题。
2) over horizon guided missile
超视距导弹
3) ship-to-air missile
舰空导弹
1.
On service probability of ship-to-air missile based on improved queuing theory;
基于改进排队论的舰空导弹服务概率研究
2.
FTA of suddenness blast-off of the engine of the ship-to-air missile;
舰空导弹发动机意外点火故障树分析
3.
Effect of instruction delay on handing over midcourse to terminal guidance of ship-to-air missile
指令时延对舰空导弹中末制导交班误差影响分析
4) ship to air missile
舰空导弹
1.
In hypothesis condition,the firing time model of ship to air missile firing at group target is established.
在一定假设条件下,对舰空导弹对群目标的射击次数建立计算模型。
2.
Finally,launching time of ship to air missile and demand of cooperative air defence in ship formation.
最后 ,根据计算结果确定了舰空导弹的发射时机和编队协同防御要
3.
From character and construct of typical target for ship to air missile,target volnerability models have been built by using the kill tree theory and probability theory and reliability theory.
从舰空导弹典型目标的特征出发 ,利用杀伤树理论 ,结合目标功能系统的性质和构成 ,提出了以概率论和可靠性理论为基础的目标易损性分析模型 。
5) air-to-ship missile
空舰导弹
1.
According to the integral technical performances and the characteristic of air-to-ship missile,this paper makes clear the design principal,and divides the control system to several important parts,meanwhile analyzes the roles of each part,then gets the control equipment selective demands and its control diagram.
根据某型空舰导弹总体性能要求和特点,确定了控制系统的设计指导思想,将控制系统划分成制导分系统、姿态控制系统、飞行电气控制系统和机载测试发控系统几大部分,分析了各部分的作用,按照控制系统的原理构建了控制系统方框图。
2.
The range matching problem between air-to-ship missile and airborne radar, which is the key to the cooperation between air-to-ship missile and its carrier is studied in this paper.
机载雷达的作用距离与空舰导弹的射程之间的匹配是弹机协调中的关键问题之一。
3.
The problem of fire distribution for air-to-ship missiles is described and the optimal model of fire distribution is established at first.
描述了空舰导弹火力分配问题,建立了火力分配优化模型。
6) Air to ship missile
空对舰导弹
补充资料：英国“海鹰”空对舰导弹
这是一种亚音中程掠海飞行的反舰导弹，主要装载在“海鸥”、“海鹰”飞行及舰载直升机上。采用惯导和主动雷达末端制导体制，并具有多目标攻击能力。战斗部为半穿甲爆破型，采用触发和近炸引信，对小目标也有较高的命中概率。最大射程１１０千米，可以在敌舰防空火力外 进行攻击，巡航速度为０．９倍速，弹长４．１米，弹径０．４０米，全弹质量６００千克。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条