本文提出了寻的导弹的一种新型制导律。这个设计概念基于使寻的时间最短。业已表明,为了实现这种制导概念必须有预测拦截路线的算法和使导弹航向转到所预测的拦截路线方向上的制导命令产生器。本文推导了预测拦截路线的算法并且证明整个制导律是容易实现的。仿真结果证明了最短的寻的时间性能和加宽的发射包迹。 This paper presents a new type of guidance law for missiles. This design concept is based on minimizing seek time. It has been shown that in order to realize such a guidance concept there must be algorithms for predicting the route of interception and a guidance order generator that directs the course of the missile to the direction of the predicted interception route. In this paper, we deduce the algorithm to predict the interception route and prove that the whole guidance law is easy to implement. The simulation results show the shortest time-seeking performance and broadened transmission envelope.