自适应控制方法的直接命中目标本体的平行接近制导律

本文在最少量测条件下采用视线角速度ｑ趋于零的指标函数和低阶等效辨识模型与快速自适应控制方法实现了战术导弹的平行接近制导律。这种最优制导律可以实现直接命中目标本体，实现一弹多用，可以用于反导弹的控制。能使制导装置简化并使其尺寸和重量减小，算法简单易于工程使用。经过大量数学和半实物仿真试验表明，上述成果可应用于实际工程当中。

CONSTANT BEARING COURSE GUIDANCE LAW OF DIRECTLY HITTING TARGET USING ADAPTIVE CONTROL

In this paper,the constant bearing course guidance law of tactical missiles is realized by using an ideal function of the angular velocity of sight line tending to zero,and a lower order equivalent identification model and the fast adaptive control method with minimum measure numbers of state variable This optimal guidance law can realize directly hitting target and multi uses missiles,and can be used to antimissile guidance law,and can simplify the guidance device and reduce its size and weight,and the algorithm is simple and easy to apply A lot of mathematical and hardware in the loop simulations have shown that the above achievements can be used into practical engineering