1) Supersonic missile
超声速导弹
1.
The design of jet vane system is investigated preliminarily,which is based upon a supersonic missile.
以超声速导弹为对象,初步研究了燃气舵系统的设计。
2) Hypersonic Missile
高超声速导弹
1.
Study on Robust Variable Structure Control for Hypersonic Missile in Reentry;
高超声速导弹再入的鲁棒变结构控制方法研究
3) Supersonic ground to air missile
超声速地空导弹
4) supersonic maneuverable missile
超声速飞航导弹
1.
A prediction method of liftdrag ratio of supersonic maneuverable missile was given.
参考飞机/发动机一体化设计的思路,建立了基于能量法的超声速飞航导弹/冲压发动机一体化设计的约束分析和任务分析模型。
5) hypersonic cruise missile
高超声速巡航导弹
1.
Method Research on Trajectory Design and Optimization of Hypersonic Cruise Missile;
高超声速巡航导弹弹道设计与优化方法研究
2.
Aimed at the complex dynamic course of combat engagement,a framework for hypersonic cruise missile combat engagement simulation is established.
针对攻防对抗这一复杂的动态过程,建立了高超声速巡航导弹攻防对抗仿真体系,并在此体系框架下,分别给出了作战环境模型、结果评判模型和进攻方与防御方的交战仿真模型。
3.
In the conceptual design of hypersonic cruise missiles,the evaluation of the missile combat effectiveness is necessary to avoid excessive index in the missile performance requirements.
在高超声速巡航导弹概念设计阶段,为了避免对某些性能指标要求过高,需要对其作战效能进行评估与分析。
6) hypersonic air-to-surface missile
高超声速空地导弹
1.
In order to study the terminal precision guidance of the hypersonic air-to-surface missile with constraints,the guidance law was designed respectively in the pitching plane and swerve plane.
针对高超声速空地导弹多约束高精度末制导的基本需求,在三维解耦的俯仰平面和转弯平面上分别设计制导律。
补充资料：V-1导弹