1.
Object oriented simulation for six freedom degree reentry trajectory
再入弹道六自由度面向对象仿真研究
2.
maneuverable ballistic reentry vehicle
机动弹道式再入飞行器
3.
advance ballistic reentry system (ABRS)
高级弹道式再入系统
4.
Optimization Design of Reentry Trajectory for Maneuverable Warhead Based on Genetic Algorithms
基于遗传算法的机动弹头再入段弹道优化设计
5.
In this paper, the principles and methods of target recognition are discussed mainly, using infrared optical technical equipment through the measurement of the target′ s temperature, radiant intensity and infrared thermal image.
反导系统对于来袭弹道导弹弹道中段及再入段的识别可以用微波雷达技术，也可用光学技术。
6.
MIRV (multiple independently targeted reentry vehicle)
多弹头分导再入飞行器（多弹头导弹）
7.
multiple independent reentry vehicle
多弹头分导再入飞行器
8.
Analysis and Prediction of Reentry Error for Reentry Maneuvering Warhead With Integrated Navigation System
复合制导再入机动弹头再入误差分析
9.
Estimate, Discriminate, Modeling and Mathematics Simulation Research of Ballistic Coefficient for Reentry Object;
再入目标弹道系数的估计、辨识、建模及其数学仿真研究
10.
Research on application of virtual guidance to the trajectory optimization of reentry-glide flight
虚拟导引方法在再入滑翔弹道优化中的应用研究
11.
To place into an orbit, a trajectory, or a stream.
置于放入一个轨道、弹道或潮流中
12.
THE ECHO BEHAVIOR ANALYSIS OF THE NONEQUILIBRIUM WAKE
再入弹头非平衡尾迹的回波特性分析
13.
Research on Restriction of Initial Space Maneuver of Reentry Missile
弹头初始再入点空间约束范围的研究
14.
Study of Missile Reentry Dynamic Decoupling Control Based on Variable Structure Robustness Compensating
动态解耦和变结构鲁棒补偿的导弹再入控制
15.
An Optimal Guidance Law for Reentry Warhead Base on Angular Velocity
一种基于角速率的再入弹头最优制导律
16.
Study of Reentry Trajectory Optimization of Maneuverable Warhead Based on Spline Curve
基于样条曲线的机动弹头再入轨迹优化研究
17.
Interceptive Research of Missile with the Mobility of the End Zone at It’s Re-Entry Phase
带末端机动的导弹再入段拦截问题研究
18.
Variable structure guidance law of reentry maneuvering warhead with terminal angular constraint
带落角约束的再入机动弹头的变结构导引律