Terminal guidance of cruise missile based on electromagnetic fingerprint is presented according to the defense system of cruise missile .
根据巡航导弹防御系统的特点,提出了一种基于电磁指纹的巡航导弹 末 制导方式。
In basic framework of total system signal stage isomorphic simulation for centroid chaff countering anti-ship missile terminal guidance radar models of warship were researched .
在全系统的、信号级的、同构的仿真研究基本框架下,从研究针对反舰导弹 末 制导雷达的质心式箔条干扰的目的出发,对目标舰的有关模型进行了研究。
Missile Terminal Guidance and Control Against Evasive Targets ; Master 's thesis
导弹 终端 制导和控制用于对付企图逃避打击的目标/硕士论文
The final phase is terminal guidance when the missile uses a highly accurate tracking system to make rapid maneuvers for intercepting the target .
最后的阶段是 末端 制导,此阶段导弹利用高精度的追踪系统,快速机动,截击目标。
In this paper aperture synthesis theory is proposed to be used in passive millimeter-wave terminal guidance .
本文将综合孔径理论应用于被动毫米波 末 制导技术,并研究了天线阵列的排布方式。
During the course of the terminal guidance the interceptor may proceed a homing guidance with the help of the homing head and self power mechanism until the final direct collision with the target .
在 末段 制导中利用拦截器的导引头和自身动力机构进行自寻的制导并最终和目标的直接碰撞。
Study on Control and Estimation Model of a Strap-down Terminal Guidance System
捷联 末 制导系统的控制与滤波模型研究
Effect of instruction delay on handing over midcourse to terminal guidance of ship-to-air missile The formulae of optimal control overload commands are reckoned .
指令时延对舰空导弹中 末 制导交班误差影响分析推导了基于捷联惯导控制方案的导弹最优控制过载指令公式,并进行了仿真验证。
Design of Terminal Guidance Radar Signal Processor System
某 末 制导雷达信号处理机系统设计与实现
Simulation of Terminal Guidance System Based On Stateflow / Simulink
基于Stateflow/Simulink的 末 制导系统仿真
A New Approach to Target Tracking during Infrared Image Terminal Guidance
一种新的红外成像 末 制导目标跟踪方法
First a model of the minimal search angle in the azimuth of the terminal guidance radar ( TGR ) is deduced .
首先推导了 末 制导雷达(TGR)最小方位角搜索范围模型。
Echo Simulation and Algorithm Study on Signal Processing for Anti-ship Terminal Guidance Radar
反舰 末 制导雷达回波建模与信号处理算法研究
Simulation study on the terminal guidance radar of the antiship missile and the ECM system
反舰导弹 末 制导雷达电子对抗系统仿真研究
The matching problem of terminal maneuver and terminal guidance trajectory of anti-ship missile is analyzed .
以上模型及仿真结果为反舰 导弹 末端机动突防“密集阵”系统在实战中的应用 提供了 参考。
Estimation of Target Maneuver Acceleration and Guidance Law Implementation in Homing Terminal Guidance
目标机动加速度的估计与 导引律实现
Study on the Optimal Terminal Guidance Law with Interception and Impact Angle
带落点和落角约束的最优 末 制导律研究
First the velocity acquisition probability of seeker at the handover from intermediate to terminal guidance was analyzed .
首先,对中、 末 制导交接班时雷达导引头的速度截获概率进行了分析;
To improve the capture probability the hand-over point of anti-ship missiles between midcourse guidance and terminal guidance was analyzed .
为了提高对目标的捕捉概率,研究了反舰导弹中 末 制导交班点的选择问题。
A fuzzy terminal guidance law with robustness to measurement noise disturbances is presented .
提出一种对测量噪声干扰鲁棒的模糊 末 制导律。
Sampling of IF digital down-conversion and DSP are used to digitize terminal guidance seeker .
利用中频采样、数字下变频以及DSP技术,实现了 末 制导雷达的数字化。
An Optimal Space Terminal Guidance Law Based on Inverse System
一种基于逆系统方法的最优空间 末 制导律
Terminal Guidance Study of Exoatmospheric Spin Stabilized Interceptor
大气层外自旋稳定拦截器 末 制导 控制研究
Realization method of frequency micro adjustment in automatic detection system of missile terminal guidance radar
频率微调在导弹 末 制导雷达自动检测系统中的实现方法
The Application of Scene Matching Aided Navigation in Terminal Guidance of Ballistic Missile
景象匹配辅助导航在弹道导弹 末 制导中的应用
Research on the Influence of Storage Environment on Terminal Guidance Projectile and the Countermeasures
环境条件对 末 制导炮弹储存的影响及对策
Research on Terminal guidance law of missiles based on nonsingular terminal sliding mode
基于非奇异Terminal滑模的导弹 末 制导律研究
Monopulse Radar 3-D Imaging and Its Application in Terminal Guidance Radar
单脉冲三维成像及其在 末 制导雷达中的应用
An infrared seeker enables a missile in its terminal guidance time to track a target precisely .
红外导引头能够使导弹在 末段 制导中精确地跟踪目标。
SAR image matching using both edge and statistical characteristic for terminal guidance
结合边缘和统计特征的 末 制导SAR图像匹配
美[ˈtɚmənəl ˈɡaɪdns]英[ˈtə:minəl ˈɡaidəns]
末段制导末段引导终端导引最终瞄准