antiaircraft missile

Research on Variable Structure Control in Slide Attitude Control of Antiaircraft Missile

防空导弹侧向姿态变结构控制器研究舱壁扶强材的侧向稳定性

A Method of Trajectory Optimization for Homing Antiaircraft Missile

寻的防空导弹的一种弹道优化方法

Establishes the firepower plan models of surface-to-surface tactic missile army sallying the antiballistic-antiaircraft missile position under different campaign intentions based on the characteristics of antiballistic-antiaircraft missile position and the traits of surface-to-surface tactic missile.

根据地地战役战术导弹特性和反导防空导弹阵地自身特点，得出在不同作战意图下，某型地地战役战术导弹部队突击反导防空导弹阵地火力计划模型。

The targets type recognition is an important content of antiaircraft missile command and control model.

目标识别模型是防空导弹指控模型的重要组成部分.

A simulation method used to evaluate on antiaircraft missile damage effect was proposed.

研究了一种配有激光近炸引信的防空导弹毁伤效果评估仿真方法.

Firepower Plan Research on Surface-to-surface Tactic Missile Army Sallying Antiballistic-antiaircraft Missile Position

某型地地战役战术导弹部队突击反导防空导弹阵地火力计划模型研究

Terminal Sliding Mode Control for Attitude Control of Antiaircraft Missile

防空导弹姿态控制系统终态滑模变结构设计

The computation methods are given for the firing table of real-time trajectory optimization of antiaircraft missile.

文章给出防空导弹轨道 实时 优化射表的计算方法.