1.
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
2.
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
3.
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
4.
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
5.
maneuverable ballistic reentry vehicle
机动弹道式再入飞行器
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.
Guidance Law of Maneuvering Reentry Warhead Based on Stochastic Variable Structure Control Theory
基于随机变结构控制理论的再入弹头制导律
9.
The design of control system on attitude stability of maneuver re-entry missile head is studied.
对大机动弹头再入飞行段姿态稳定控制系统的设计问题进行了分析与研究。
10.
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
11.
THE ECHO BEHAVIOR ANALYSIS OF THE NONEQUILIBRIUM WAKE
再入弹头非平衡尾迹的回波特性分析
12.
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
13.
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
14.
Design of Trajectory of the Maneuver of Warhead in a Plane Based on Impulse Firing in the Passive Curve
基于脉冲点火弹头平面机动的被动段弹道设计
15.
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
16.
The Method of the Trajectory Design and Numerical Stimulation of the Missile Maneuvers in Space Based on the Impulse Firing in the Passive Curve
基于脉冲点火弹头空间机动的被动段弹道设计方法和数值仿真
17.
advance ballistic reentry system (ABRS)
高级弹道式再入系统
18.
Insert the hunting arrow from the front, and get the tail of the arrow pressed under the spring of the crossbow body.
将狩猎箭自弩身头部插入，弩机处弹簧片压在箭尾翼处。