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Linear Quadratic Differential Games Guidance Law for Dual Controlled Missiles

机译:双控制导弹的线性二次微分博弈制导律

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摘要

A novel guidance law designed specifically for a missile having forward and aft control systems is presented. For the derivation a linear quadratic differential games formulation of the end-game interception scenario is used. Conditions for achieving perfect intercept are given and new game spaces are presented. It is also shown that increasing the direct lift associated with the canard control allows intercepting targets with higher maneuvering capability, while for the tail control the effect is opposite.
机译:提出了一种新颖的制导律,专门针对具有前,后控制系统的导弹而设计。对于推导,使用终端游戏拦截场景的线性二次差分博弈公式。给出了实现完美拦截的条件,并提出了新的游戏空间。还显示出增加与鸭翼控制相关的直接升力允许拦截具有更高机动能力的目标,而对于尾巴控制则效果相反。

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