1) overhead attack guidance
击顶制导
1.
In this paper, the law of overhead attack guidance for anti tank missiles is studied applying principles of flight mechanics and theory of optimum proceses.
运用飞行力学原理和最优过程理论 ,在考虑导弹击顶攻击坦克有弹道倾角要求的条件下 ,推导出了一种适用于反坦克导弹击顶制导的组合性能指标最优的导引律。
2) overhead-attack guidance law
击顶制导律
3) dive overhead attack anti tank missile
击顶反坦克导弹
4) hit on top of the tank
击顶
1.
According to the general program of a portable antitank missile steering to hit on top of the tank at terminal trajectory, this paper presented the closed-loop control stiffness ballistic model and simulation for the straight flight, the glancing flight and terminal steering trajectory under both the fixed and active targets.
在末端姿态弹体折转控制、掠飞击顶轻型反坦克导弹总体方案论证的基础上 ,利用某反坦克导弹的总体参数 ,建立了这种新型导弹的闭环控制刚体弹道模型 ,进行了固定目标平飞、固定和活动目标掠飞折转等三种闭环控制弹道的全数字仿真 ,仿真结果表明 ,末端姿态弹体折转控制击顶的总体方案技术可
5) terminal-guide mortar bomb
末制导迫击炮弹
1.
For controlling a terminal-guide mortar bomb,attitude angles of the mortar bomb are needed in real-time.
在末制导迫击炮弹控制时,需要知道迫击炮弹的实时姿态角。
6) pursuit-course guidance
追击航向制导
补充资料：波束制导(见遥控制导)
波束制导(见遥控制导)
beam-rider guidance
boshu zhidao波束制导(beam一rider guidanee)见遥控制导。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条