1.
The Aerodynamic Simulation of External Flow Field of Terminal Segment of Terminal Homing Projectile
末制导炮弹末制导段外流场气动仿真
2.
Research on the Last-Stage Guidance Trajectory Simulation of the TV-guided Missile
电视制导导弹末制导段的弹道仿真研究
3.
End-Game Performance Analysis of Exo-Atmospheric Kinetic Vehicle;
大气层外动能拦截器末制导段性能研究
4.
Optimum Design of Variable Structure Guidance Law for Exoatmospheric Endgame Interception
大气层外末段拦截变结构制导律设计
5.
Fluent-Based Aerodynamic Simulation of Terminal Guided Projectile in Its Initial Stage
基于Fluent的末制导炮弹初始段气动仿真
6.
A terminal guidance law design applied to space-to-surface precision attack weapons
天对地精确攻击武器末段制导律设计
7.
Studies of Guidance and Combined Control in Terminal Phase When Intercepting Tactical Ballistic Missile;
拦截战术弹道导弹末段导引和复合控制研究
8.
The Terminal Area Energy Management Trajectory Designe and Guidance for a Reusable Launch Vehicle;
可重复使用飞行器末端能量管理段轨迹与制导
9.
Study on Terminal Guidance Laws and Control Methods for Kinetic-Kill Vehicle;
动能拦截器末段导引规律和控制方法研究
10.
Many missiles use a different type of guidance in the midcourse phase than in the terminal phase, as will be discussed later.
许多导弹在中段和末段使用不同的指导方式，我们随后将讨论这些制导方式。
11.
Analysis of the Divert Ability of Atmospheric Interceptors Controlled by Lateral Jet Thrusters
大气层内直接侧向力控制拦截导弹末段修正能力分析
12.
Approximative Computation of Zero Effort Miss and Energy Required by Terminal Guidance for Space Interception
空间拦截零控脱靶量与末段制导能量需求的近似计算
13.
The final phase is terminal guidance when the missile uses a highly accurate tracking system to make rapid maneuvers for intercepting the target.
最后的阶段是末端制导，此阶段导弹利用高精度的追踪系统，快速机动，截击目标。
14.
The idea and method in this paper can be taken as a reference for the design of terminal homing anti-tank missiles and accuracy allocation of weapon system.
文中结果可为末段寻的制导的反坦克导弹总体设计及武器系统精度分配提供参考。
15.
The Study of Terminal-Guided Radar Detectors in Anti-Ship Missile;
反舰导弹末制导雷达实用检测器研究
16.
A technology of tracking filtering in ARM terminal guidance phase
反辐射导弹末制导跟踪滤波技术研究
17.
Performance of proportional navigation law for terminal laserguided projectile
激光末制导炮弹比例导引律性能研究
18.
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