The search model of terminal guidance radar in anti - ship missile 反艦導(dǎo)彈末制導(dǎo)雷達(dá)搜索模型
System application of staring infrared imaging terminal guidance 凝視紅外成像末制導(dǎo)系統(tǒng)應(yīng)用研究
Semi - object experimental research on handing over midcourse to terminal guidance 中末制導(dǎo)交班半實(shí)物實(shí)驗(yàn)研究
Part , study the guidance law of the terminal guidance section 第三部分研究了攔截導(dǎo)彈末制導(dǎo)段的制導(dǎo)律。
A control algorithm for designing anti - ballistic missile terminal guidance law 一類不確定非線性系統(tǒng)變結(jié)構(gòu)自適應(yīng)魯棒控制
Study of handing over between midcourse guidance and terminal guidance for multi - purpose missiles 多用途導(dǎo)彈中末段交班研究
Modeling and simulation of terminal guidance mortar projectiles using impulse thruster control 末制導(dǎo)迫彈脈沖控制建模與仿真
Research on the vertical intercept terminal guidance system of tv - command - guidance air - to - ground missile 電視指令制導(dǎo)空地導(dǎo)彈垂直命中目標(biāo)的末制導(dǎo)系統(tǒng)研究
With such a geometry , the final approach for physical contact occurs under much higher rates of angular change , making terminal guidance much more difficult 幾何規(guī)律使這種攻擊最后的角度變大,從而更不容易導(dǎo)引。
The terminal guidance procedure is simulated , and the results validated the capability of the exoatmosphere kinetic - kill vehicle to hit the target directly 在此基礎(chǔ)上對(duì)動(dòng)能攔截器的攔截過(guò)程進(jìn)行仿真,驗(yàn)證了動(dòng)能攔截器對(duì)彈道導(dǎo)彈的直接命中能力。