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1·High PRF and inverse receiver are often used in radar missile guidance.

在雷达导引头中经常采用高prf倒置接收体制。

2·Finally, a design of the missile guidance control law is arrived at using proportional navigation method.

最后，设计了移动质心与直接力复合控制动能弹的制导控制规律。

3·This paper Outlines the current status and future development of TV tracking technology used in missile guidance.

本文综述了电视跟踪制导技术的现状和发展趋势。

4·The parts include fasteners used on aircraft, missile guidance electronics, materials used in body armor and engine mounts.

其中也包括了在飞机上使用的紧固器、飞弹导航电子设备。 防弹衣原材料和引擎装置。

5·In recent years, with various aircraft to en-hance the speed and maneuverability, the task of the missile guidance system has become increasingly complicated.

近年来，随着被拦截目标速度和机动性能力的增强，导弹导引系统的制导任务变得越来越复杂。

6·The mechanism of modern fighter guidance is discussed, referring to the theory of missile guidance. A kind of fighter guidance law based on optimal time is given.

借鉴导弹导引理论对现代战机的导引机理进行了探讨，推导出一种基于时间最优的飞机导引控制律。

7·The stability of a kind of missile guidance system is analyzed, and the effect of perturbation of radome boresight error slope a on the stability is investigated.

分析了某类导弹系统的稳定性，研究了天线罩瞄准线误差斜率A的摄动对寻的制导控制系统的影响。

8·In this study we have attempted to investigate the trajectory stability problems of head-on anti-tactical ballistic missile guidance by way of the Lawes Criterion.

针对一种拦截战术弹道导弹制导规律的特点，以经典的劳斯稳定判据为依据，对其制导控制回路的稳定性进行了分析。

9·However, the PLA would need to make substantial advances in missile guidance and countermeasures in order to achieve the very high precision required to attack a moving target.

然而，PLA将会需要去获得实质上的进步在导弹制导和反干扰上，为了实现攻击一个移动目标所必需的、非常高的精确度。

10·In this paper, the missile guidance with terminal impact Angle constraint and integrated guidance and control design for missile with terminal impact constraint were researched.

在这一背景下，本文研究了带末端攻击角度约束的制导方法设计和制导控制一体化方法设计问题。