导弹发射系统手持姿态，不太符合我的习惯，但是，操作简便，可靠性也是很不错。
The missile launching system is not in line with my habit, but its easy to operate, the reliability is very good.
它把主动雷达和一个被动参考单元以及微电脑系统结合在一起，可使得导弹更少的依靠飞机上的发射控制系统。
It incorporates active radar with an inertial reference unit and micro-computer system, which makes the missile less dependent upon the fire-control system of the aircraft.
当然不仅海上可以发射这些导弹，其他的超级精确制导系统，比如某些悬挂在F15E战鹰攻击机上的制导导弹（GBU），通过激光和尾翼制导。
Destruction doesn't only come from the sea, either. Other super accurate systems, like certain Guided Bomb Units (GBU) carried on F15E Strike Eagle planes, use lasers and fins for guidance.
宙斯盾弹道导弹防御系统利用远程传感器预先提供的实时信息，由舰载SPY-1雷达捕捉入侵弹道导弹，并发射了一枚标准导弹进行拦截。
The Aegis BMD system fired a Standard Missile using real-time information from a remote sensor prior to the shipboard SPY-1 radar acquiring the inbound ballistic missile.
今天，Artillery公司使用的是努里特雷达系统，这使他们能够发现向以色列发射的包括奇格勒、卡萨姆和卡秋莎等导弹。
Today, the Nurit Radar System is used by the Artillery Corps and it enables them to locate missiles including Grad, Qassam and Katyusha missiles that have been fired at Israel.
为满足防空系统抗击隐身目标的需求，提出了一种计算双基地制导雷达rcs和导弹发射距离的方法。
To meet the requirement of air defence system countering stealthy target, a method of calculating the RCS of bistatic guidance radars and distance of the launched missile was given.
还配备相当准确的武器系统，比方说它身处英吉利海峡，发射的巡洋导弹能丝毫不差击中远在北非的目标。
And its weapons systems are so accurate that were it positioned in the English Channel, its cruise missiles could pinpoint targets as far away as North Africa.
提出了航空发动机防喘控制系统设计和研制方法，分析了当战斗机发射导弹时热扰动参数对发动机的影响。
The design and development methods of aeroengine anti-surge control system are presented. Effects of heat disturbance parameters on the engine are analyzed during missile launch.
提出了一种确定目标进入角的原理和方法，这种原理和方法具有较高的计算精度和实时性，易于工程实现，可用于机载火力控制系统完成空对空导弹允许发射区计算。
This method are with a high accuracy and real time application, and can be applied in the calculation of allowable launching area of air to air missile in air borne fire control system.
为研究具有大离轴角及越肩发射能力的先进空空导弹初始段敏捷转弯方法，研究了装有反作用喷气控制系统的空空导弹的大角度姿态过失速机动控制律。
This paper investigates the large Angle attitude post stall maneuver control for the agile turn phase of an air-to-air missile that has high off-boresight capability and head reverse maneuverability.
激光引信光学组件作为导弹系统中的重要组成部分，担负着探测信号的发射与接收，其工作性能影响到整个武器系统的质量。
As a key component of a missile, the optical module in the laser fuze transmits and receives detecting signal, its performance affects the whole weapon system.
本文旨在通过对某类常规战术导弹发射控制系统射击模型的分析，探讨导弹打击目标的精确度。
Through the analysis to firing model of the launching control system for a certain type conventional tactical missile, the firing accuracy to the target is discussed.
导弹地面测发控系统可以对导弹进行发射控制、时序检测和火工品通路阻值测量，其整体构成采用分布式结构。
A low cost missile ground test and control system adopts distributed structure, which can carry out launch control, time sequence detection and pyrotechnics channel resistance measurement.
新的系统避免了由于发射大的波长阵列跨越整个红外光谱所引起的问题，保证能反制所有类型的导弹。
The new system avoids that problem by emitting a large array of wavelengths across the entire infrared spectrum, to ensure all missiles types are countered.
本文首先分析了一种先进的空空导弹系统，确定导弹对允许发射区边界敏感的主要性能特点，在此基础上提出了导弹允许发射区的算法。
In this paper, one advanced air-to-air missile system has been analyzed in order to determine the main characteristics which are sensitive to the boundary of the allowable launch envelope.
目的为解决战术导弹自力垂直发射中的燃气排导、防护及防意外点火等问题，提出了一种自力垂直发射系统的新方案；
Aim A new scheme of vertical launching system was presented to solve the problems of combustion gas exhaust and protection, guarding against unexpected firing and so on.
定向器束在发射状态下的振动特性能够反映发射系统动态性能和结构的合理性，并且会影响火箭、导弹武器系统的射击精度。
The vibration characteristic of launch tube in launching state can reflect the dynamic performance and the structural rationality of launch system, and it will influence the shooting precision.
其任务是突入苏联在中欧的严密的防空体系，对重要目标和防空系统(雷达、指挥中心和导弹发射架)实施攻击。
The mission it was designed for was to penetrate thick Soviet air defenses in central Europe and attack key targets and air defense systems (radars, command centers, and missile launchers).
根据发射系统内弹道计算模型 ，针对燃气发生器喷喉面积对导弹发射动力的影响进行导弹运动参数、内弹道性能的计算与分析。
During the ground test under different working conditions of the gas generator, the influences of the radial clearance and exhaust nozzle area were studied.
根据发射系统内弹道计算模型 ，针对燃气发生器喷喉面积对导弹发射动力的影响进行导弹运动参数、内弹道性能的计算与分析。
During the ground test under different working conditions of the gas generator, the influences of the radial clearance and exhaust nozzle area were studied.
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