1) overhead-attack guidance law
击顶制导律
2) 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。
3) dive overhead attack anti tank missile
击顶反坦克导弹
4) guidance law
制导律
1.
Three-dimensional guidance model and guidance law design for head pursuit interception;
前向拦截的三维制导模型及制导律设计
2.
Variable structure guidance law with terminal attack angle constraint;
带终端攻击角度约束的变结构制导律
5) Midcourse Guidance Law
中制导律
1.
Variable Structure Midcourse Guidance Law with Angle Constraint for Anti-Ship Missile;
带落角约束的反舰导弹变结构中制导律研究
2.
A Optimal Midcourse Guidance Law Using Neural Network;
基于RBF神经网络的一种最优中制导律
3.
Derivation and simulation of a suboptimal midcourse guidance law for air-launched cruise missile;
一种次优空射巡航导弹中制导律的推导与仿真
6) terminal guidance law
末制导律
1.
Robust terminal guidance law for maneuvering targets;
拦截机动目标的一种鲁棒末制导律设计
2.
Considering the attack process of the television guidance UCAV,taking a terminal guidance law of UCAV as a problem of tracking the target at meeting the impact attitude angle restriction,the law based on autopilot was designed,which eliminates the influences of dynamic factor of autopilot and gravity factor on hitting the target.
综合考虑电视指令制导无人攻击机的作战过程,将其末制导律设定为满足落角约束的目标跟踪问题,设计了一种基于自动驾驶仪末制导律,该方法消除了自动驾驶仪动态因素和重力等因素的影响;并通过以平行接近法作为辅助导引法来克服追踪法的缺陷;新的末制导律加自适应卡尔曼滤波,使得无人攻击机不仅可以对固定目标实施攻击也可以对低速移动目标实施攻击,且能保持无人攻击机垂直命中目标,提高作战效能。
3.
Selecting appropriate terminal guidance law is an important factor for the precise guidance of anti-ship missile.
选择合适的末制导律是实现反舰导弹精确制导的重要因素。
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