1) TGSM (terminally guided sub-missile)
终点制导子导弹
2) missile guidance
导弹制导
1.
Scene simulation system of missile guidance based on Vega;
基于Vega的导弹制导视景仿真系统
2.
This paper aims at deficiencies in the course of missile guidance hardware-in-the-loop simulation,puts forward engineering simulation idea,and sets up the engineering flow of missile guidance hardware-in-the-loop simulation and researches it particularly.
文中针对导弹制导半实物仿真中出现的诸多不足,从技术和管理两方面提出工程化仿真思想,建立了导弹制导半实物仿真的工程化流程并加以详细研究。
3.
Considering the characterization of missile guidance,the correcting method of distortion resulting from scanning ladar imaging moving target is deduced.
系统的分析了扫描成像激光制导雷达的原理,介绍了扫描成像激光制导雷达的特点,并结合导弹制导的特点,分析了扫描成像激光雷达对运动目标成像产生的畸变的原因,推导出了对成像畸变进行修正的数学方法,并对推导的结果进行了分析和讨论。
3) guided missile
制导导弹
1.
Simulation Method of IR Image Seeker for Guided Missile;
红外成像制导导弹导引头仿真方法研究
2.
Research on the Positioning Accuracy of the GPS/INS Guided Missile;
GPS/INS制导导弹运行模型变化定位精度分析
3.
The rapidly development of modern guiding technology and the renovation of new weapon bring forward rigorous demands for the training and employment of guided missile.
现代制导技术的迅速发展和武器装备的不断更新,对制导导弹的训练使用仿真提出了苛刻的要求。
5) scatter of terminal point of self-control phase of a missile
导弹自控终点纵向散布
1.
By a known longitudinal scatter of terminal point of self-control phase of a missile, how to find out its intervals of initial altitude that is necessary to definite tactical and technical index, launch mode, combat use, is an inevitable problem to weapon system of a missile based on moving launch plate.
在给定导弹自控终点纵向散布的情况下,如何界定导弹的发射初始姿态域?是动基座发射的导弹武器系统必须面对的问题,它对确定导弹武器系统战术技术指标、发射方式和战斗使用等至关重要。
6) point-type infrared missile
点源型红外制导导弹
1.
Secondly, how the airborne radar confront the point-type infrared missile is studied emphatically.
然后根据预警机自身的特点,着重研究了预警机如何与点源型红外制导导弹进行对抗的情况。
补充资料：终点
1.一段行程结束之处。 2.指径赛中规定的终止地点。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条