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。
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。
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。
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。
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。
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。
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。
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。
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。
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。
Using" the method of analytical reconstruction the acceleration information of target is added into-the missile guidance law. The performance of the homing missile are improved."
在导弹上用解析重构的方法形成目标加速度信息并引入导引规律，提高了自动导引导弹的性能。
In order to enter into the ideal trajectory with minimal energy, the nonlinear thrust vector control and the prediction guidance are adopted in the missile guidance control system.
为使飞行器能在主动段很快地进入到理想弹道上，系统采用了非线性的推力向量控制及预测制导方法。
Engineering mechanics applies these principles to real-world design problems as diverse as nuclear reactors, hybrid automobiles, experimental aircraft, and missile guidance systems.
机械学工程将这些原理应用于现实生活来处理核反应堆，混合动力汽车，实验性飞机，导弹导航系统等各种问题。
The missile guidance law utilizing nonlinear variable structure control is proposed. The acceleration command input is determined considering the target acceleration as an uncertainty.
针对导弹拦截问题，在非线性系统滑模变结构控制理论的基础上，提计出一种新型滑模变结构导引律；
The method for consistency check of multisensor data by using the probability distance measuring is presented, and it used in CAN bus missile guidance and control system based on multi-IMU.
提出了应用概率距离测量对多传感器信息进行一致性检验的方法，并将此方法引入到基于多惯性测量组合的总线式导弹制导控制系统中。
It can be widely used in the system of radar, missile guidance, electronic countermeasures, test instrument. And the merits of communication system are often directly affected by its performance.
它被广泛的应用于雷达导航、导弹制导、电子对抗、测试仪表等系统中，其性能的优劣往往直接影响着整个通信系统的性能。
The damage mechanism and intensity of AntiRadar Missile(ARM) to the surfacetoair missile guidance radar were analyzed, and the relevant mathematical models and calculation methods were put forward.
针对反辐射导弹对地空导弹制导雷达的毁伤机理和强度进行分析和理论研究，提出求解破片式战斗部对制导雷达毁伤概率的数学模型和计算方法。
The guidance systems didn't work and the missile couldn't hit its target.
制导系统失灵了，所以导弹没能命中目标。
Lockheed Martin successfully conducted a test of the new upgraded guidance and control system for the Army Tactical Missile system (ATACMS) at White Sands Missile Range.
在白沙导弹试验场，洛克西德马丁公司对陆军战术导弹系统(ATACMS)新升级的导航和控制系统进行了一次成功的测试。
The general idea is that the Chinese DF-21 ballistic missile has been equipped with a high-explosive warhead and a guidance system that can find and hit a aircraft carrier at sea.
一般认为中国DF-21弹道导弹已经装备一枚高爆弹头和一套能在海上寻找并且击中一艘航空母舰的制导系统。
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.
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。
Based on the necessary modeling accuracy for radiating characteristics and movement characteristics of infrared targets, it can meet the design and debug demand for the guidance algorithm of missile.
在保证必要的红外目标辐射特性和运动特性建模精度基础上，采用这种方法可以满足导弹制导算法的研制和调试需要。
Among the guidance principles of the air-to-ground missile, the proportional guidance method and the direct guidance method have their respective advantages and disadvantages.
在空地导弹的导引律中，比例导引法与直接导引法各有优缺点。
It can be said that automatic detection of remote airplane and missile has been the key techniques for imaging guidance, warning system and photoelectricity resist.
可以说远距离的飞机、导弹等飞行物的自动检测已成为成像制导、告警系统和光电对抗的核心技术。
Combined with the research on ir imaging signature of target, the principle of ir imaging homing guidance technology of air defence missile in clutter background is described.
结合对目标红外特性的研究，阐述了在复杂背景条件下防空导弹对目标的红外成像寻的制导原理。
The airborne OTH target indication radar for ship born helicopter not only provides relay guidance and longer range, but also improves the missile attack accuracy.
舰载直升机机载超视距目标指示雷达不仅能为舰载导弹进行中继制导，延长导弹射程，而且能够提高导弹攻击精度。
The stability analysis of variable structure guidance system of an air-to-air missile was conducted based on the circle criterion nonlinear stability analysis theory.
文中在圆判据非线性稳定性理论基础上，进行空空导弹变结构制导系统的稳定性分析。
A mini digital Attitude and Heading Reference System (AHRS) based on DSP is designed, which can be used on air-to-air missile with Strapdown Inertial Navigation System (SINS) as mid-course guidance.
论文针对使用捷联惯导系统为中制导的近距空空导弹，设计了一种基于数字信号处理器(dsp)的小型数字式捷联航姿应用系统。
The guidance of closed-loop guidance in a missile is the guidance of optimization based on the significance of "fuel consumption is minimum", and it is only secondly-optimal in implementation process.
导弹闭路制导的导引是基于“燃料最省”意义下的最优导引，并且在实际应用中，实现过程只是准最优的。
The guidance error sources are analyzed and the hitting probabilities are calculated before the disturbance and after it by utilizing the formula about single missile shot percentage.
分析了制导误差的来源，根据建立的导弹命中概率计算公式，具体计算激光干扰前后导弹命中概率。
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