研究了制导炮弹最优滑翔弹道与控制问题。
The optimal glide trajectory and control system of combined guidance munition were studied.
该武器系统由电视末制导炮弹和地面控制站二部分组成。
This weapon system consists of two parts, namely, the TV-guided projectile and the ground control station.
飞行弹体的姿态测量是制导炮弹设计中必须要解决的问题。
The attitude measurement of flying projectile is a very important problem which must be resolved when designing the guided projectile.
还有一部火炮侦校雷达和一部气象雷达(改良非制导炮弹准确性)。
There is also an artillery spotting radar and a weather radar (to improve the accuracy of unguided shells).
该系统能够向末制导炮弹控制舱提供模拟光电激励，并得到响应信号。
It can provide simulative optical and electronic stimulation to control cabin and obtain response signal.
在激光半主动末制导炮弹武器中，激光照射器的有效照射距离对武器系统的作战效能有着很大影响。
Available irradiation range of laser irradiator influences the efficiency of weapon system of laser half initiative end guilding shell.
最近，美陆军将神剑精确制导炮弹的生产数量从30000枚减少到了6264枚，违反了纳恩-麦克柯迪法案。
The U.S. Army recently reduced the production numbers of the Excalibur precision-guided projectile from 30,000 to 6,264 projectiles, which caused the program to enter a Nunn-McCurdy unit cost breach.
为了实现所设计的方案弹道，提出了制导控制系统的总体方案，建立了滑翔制导炮弹的控制系统数学模型。
In order to realize the designed project trajectory that the guidance and control overall scheme is proposed and control system mathematical model of guided projectile is established.
基于对激光制导武器系统激光编码及波门设置特点的分析，提出了激光末制导炮弹武器系统的新型激光编码方案。
Upon analyzing the characteristics of laser code and wave gate setting, a new kind scheme of laser code in the laser terminal guidance ammunition round is proposed.
仿真结果表明，设计的自动控制系统能够使滑翔制导炮弹在飞行过程中具有良好的响应特性，方法简单，易于实现。
The simulation results show that the automatic control system can make the guided projectile response perfectly and design method is simple and achieved easily.
通过模拟弹试验与分析计算，研究了滑动式塑料弹带的主要结构参数与弹带强度的关系，为某大口径制导炮弹设计提供了依据。
To study the relations between main structure parameters of sliding plastic belt and intensity of belt by experimented and analyzed on simulative projectile.
弹道模型由炮弹无控自由飞段、惯性制导滑翔段和末制导段按比例导引制导率建立。
The trajectory model consists of the uncontrolled free flight segment, the inertial guided glided segment and the final guidance segment, which accords with the proportional guided law.
弹道模型由炮弹无控自由飞段、惯性制导滑翔段和末制导段按比例导引制导率建立。
The trajectory model consists of the uncontrolled free flight segment, the inertial guided glided segment and the final guidance segment, which accords with the proportional guided law.
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